CN118129323A - Fixing device and related equipment and technology - Google Patents

Abstract

The invention provides a device capable of connecting, combining and fixing, in particular to equipment capable of connecting, combining and fixing in the air, a method and application thereof. The device or equipment comprises an ABA mechanism, a sucker, a remote control fixing device, an unmanned aerial vehicle system and the like. By adopting the technical scheme of the invention, the device or equipment can be connected, combined or fixed relatively quickly.

Description

Fixing device and related equipment and technology

Technical Field

The present invention relates to an aircraft, a building, and related equipment and methods used in the fire extinguishing process thereof, as well as to techniques, methods and related equipment for aerial operations, glass breaking, smoke evacuation, transportation, connection, bonding and securing of aerial objects, and the like.

Background

Fire suppression of buildings, particularly high-rise and super high-rise buildings, is a difficult problem. Smoke in a fire scene is harmful to trapped personnel and firefighters in the fire scene, and affects fire fighting. Smoke evacuation is an important task in fire fighting operations of buildings. At present, when a fire disaster occurs in a building, smoke is discharged mainly through a smoke discharging channel or a fixed smoke discharging machine arranged in the building, and the mobile smoke discharging equipment is mainly used on the ground or in a low-rise building. In addition, the conventional mobile smoke exhaust devices are generally placed on the ground or exposed surfaces, and cannot be directly fixed on the outer wall of a building to exhaust smoke. The valve is closed in the fire scene at present by adopting manual operation.

Disclosure of Invention

There is currently no portable smoke evacuation device that is useful in a variety of buildings, particularly high-rise buildings, in a fire, and in particular, devices that can evacuate smoke from the building directly to the outside through a window. The invention provides a series of technical schemes. Comprising the following steps: fire extinguishing apparatus or device, method of extinguishing fire, techniques, methods and related devices in aerial work, breaking glass, smoke evacuation, transportation, connection, bonding and securing of aerial objects, and the like. The invention also provides a pole setting system, a valve opening and closing method and the like which are convenient for combining equipment with the unmanned aerial vehicle. The building comprises a house and a structure. Such structures include, but are not limited to, water towers, chimneys, tanks. By adopting the technical scheme provided by the invention, the development of fire-fighting works and the like can be facilitated.

By way of illustration, in the present disclosure, the terms "comprises," "comprising," "has" and any variations thereof are intended to cover a non-exclusive inclusion. For example, a process, method, system, apparatus, or device that comprises a series of steps or elements is not limited to the listed steps or elements but may alternatively include other steps or elements not listed or inherent to such process, method, system, apparatus, or device. For convenience of description, in the present invention, the terms "connected," "fixed," "connected," "coupled," and any variant thereof are used in the sense of "coupled" and are included in the term. The term "couple" is intended to mean "couple" two objects together, either directly or through other objects. The terms "support," carry, "" move, "and any variation thereof, are intended to" support, "" carry, "and move" one object with respect to another object, without or with respect to other objects. The terms "mounted," "connected," or other variations thereof are to be construed broadly and may be, for example, fixedly connected or detachably connected.

In the present invention, when the same embodiment is described, the "preferable" and the "further preferable" are in parallel relation, not in an inclusive or progressive relation; all of these solutions can be combined as desired without conflict. Because the invention provides a plurality of devices and methods, a plurality of technical schemes are provided, and under the condition of no conflict, the different technical schemes and the contents or steps of the different technical schemes can be combined according to the needs. Such combinations are also within the scope of the present invention.

It should be noted that in the description of the present invention, the numerals "I", "II" … … or "1", "2" … … and the terms "first", "second" … … are merely used for convenience in describing the different components and are not to be construed as indicating or implying a sequential relationship, relative importance or implying that the number of technical features indicated is indicated. Thus, a feature defining "I", "II" … … or "1", "2" … … may include at least one such feature explicitly or implicitly.

The present application has been defined in terms of devices or terms in order to ascertain the concepts and scope of the devices. Where related devices or terms are referred to, they are defined in the present specification. The definitions in the prior application or patent application number 2022106156183 of the present application are referred to, not defined in the present specification.

The structure and use of the motor, steering engine and its control parts, distance detector, unmanned aerial vehicle body, camera, thermal imaging instrument, etc. and the sealing waterproof protection of some devices are known technology, so it will not be described in detail in the present invention.

In order to achieve the above object, embodiments of the present invention provide the following technical solutions.

In a first aspect, the invention defines a latch for locking two items together, or for snapping together, or for bonding two objects together so that they are not easily separated.

In a second aspect, the present invention defines a "AB style mechanism" in combination with "AB style". In the present invention, "a manner of bonding the object a and the object B together in order to enable the object a to provide support for the object B" is defined as an AB bonding manner; the apparatus used to implement the AB type bonding method is simply referred to as an AB type mechanism, that is, a mechanism capable of bonding the object a and the object B together so that the object a can provide support for the object B. The AB type mechanism includes, but is not limited to, an electromagnet, a sucker, a magnet, a clamping mechanism, and the lock catch. If the AB type mechanism is combined with other objects and can be separated from the objects, the AB type mechanism is called an ABA type mechanism. The invention provides an ABA mechanism I, which comprises a sucker, an air pipe and a pump; the pump is used for pumping air. The sucking disc is connected with one end of the trachea, and the other end of the trachea is connected with the pump. Thus, after the pump is started, the suction cup can be attached to an external object. Preferably, the surface of the suction cup contains a compressible porous object, including but not limited to a sponge, so that the suction cup can be attached to a roughened object.

In a third aspect, the present invention provides a support system for supporting objects from outside a building, including but not limited to fire extinguishing devices, glass breaking devices, transportation equipment, aircraft, objects onboard an aircraft. The support system includes, but is not limited to, one or more of the following: rods, rings, plates. The support system is mounted on an exterior wall or surface of a building or an appendage of an exterior wall or surface of a building. The exterior wall, exterior surface appendages include, but are not limited to, windows, window frames, balconies.

Preferably, the support system satisfies: after the support system is installed on a building, the entity formed by connecting the points on the support system projects to the plane where the surface of the window glass of the building adjacent to the support system is located, and the projection has a superposition part with the surface of the glass. As a further preference, the portion of the support system for supporting is located outside the plane of the window pane.

Preferably, the support system satisfies: when an external bracket or device (including but not limited to the bracket, bracket system, fire fighting related device of the present invention) is coupled to the support system, all or a portion of the bracket or device is positioned outside the window of the building. As a further preference, the window pane is moved in the direction of its surface normal towards the outside of the building, and then the bracket or the device can be hit. As a further preference, the glass breaking device, or the glass breaking device mounted on the bracket system, may contact the glass of the building, and may also perform a glass breaking operation; the nozzles or water guns mounted on the bracket system can spray water into the building, and the nozzles or water guns can also enter the building.

Preferably, the support system satisfies: when external brackets or equipment (including but not limited to brackets, bracket systems, fire fighting equipment, and the like of the present invention) are coupled to the support system, the entity connecting the points of the brackets or equipment projects into the plane of the surface of the architectural window glass adjacent the support system where there is a coincidence with the surface of the glass. As a further preference, the portion of the support system for supporting is located outside the plane of the window pane.

Preferably, the support system is used for supporting equipment or devices; as a further preference, the support system is for supporting a fire extinguishing apparatus or device. Preferably, the support system is for use in conjunction with a device or apparatus; as a further preference, the support system is for use in conjunction with a fire extinguishing apparatus or device. Preferably, when the support system supports a device or apparatus, the support site of the support system is more than 10 cm from the exterior surface of the building; or the distance between the supporting position of the supporting system and the outer elevation of the building is more than 10 cm.

Preferably, the support system can be incorporated by means from outside the building using an AB type mechanism. Preferably, the support system is used for supporting objects conveyed by the aircraft or for supporting objects conveyed outside the building. Preferably, the support system is located outside the outer surface of the window glass of the building. Preferably, the portion of the support system for supporting is located outside the outer surface of the glass. Preferably, the support system comprises a limiting component. The limiting component is used for limiting the movement or rotation of an object, such as a limiting rod, a groove and a boss. Preferably, the support system has one or more of the following features: the device is only used for supporting the fire extinguishing device, is not used for supporting objects in a flat state, is only limited to fire-fighting use, is only used for supporting objects from an aircraft, is not used for preventing people outside a building from entering the interior of the building, is not used for preventing the supported device or equipment from moving, and is not used for supporting daily use devices of the building. The daily use devices of the building comprise, but are not limited to, air conditioners, clothes hangers and flowerpots.

Preferably, the support system is configured and dimensioned to cooperate with the AB mechanism of the object to be supported and not impede movement of the supported object. For example, when the bracket system described below includes two AB-type mechanisms on the left and right for engagement with two vertical posts, then the support system includes two vertical posts and the distance between the two vertical posts is equal to the distance between the two AB-type mechanisms on the bracket system, while the two vertical posts are sized to meet the requirements for their ability to enter the two AB-type mechanisms.

Preferably, the support system is mounted on an exterior facade of a building and the shortest distance to the window frame is less than 1 meter. Preferably, the support system is a stand comprising a plurality of rods. Preferably, the support system is composed of a material having a melting point of 500 degrees celsius or a softening point of 300 degrees celsius or more, including but not limited to steel, aluminum alloy.

In a fourth aspect, the present invention defines an electric primer-shooter, which is a shooter that fires, ignites a propellant charge by means of a current or voltage, and shoots a nail. The invention provides an electric primer nail shooting bullet I, which comprises a nail shooting, a bullet sleeve, a propellant powder, an electric igniter and an electrode. The propellant powder is filled in the bullet sleeve, the shooting nail comprises a protruding head (short for nail head), the nail head is buried in the propellant powder, and the electric igniter is a component capable of igniting and igniting the propellant powder after being electrified so that the propellant powder starts to work and comprises but not limited to a resistance wire, an arc generator and an electronic igniter. The electric igniter is connected between two electrodes.

In a fifth aspect, the present invention provides a barrel for use with an electric primer cartridge, the barrel comprising a securing means for securing the barrel to an object to be secured (simply referred to as object G), which may be a plate, rod, bracket or device, and a nail shot from the barrel securing the object G to another object. Preferably, the barrel further comprises an electric igniter. Preferably, the barrel contains a battery for powering the electric primer projectile. Preferably, the outlet of the gun barrel comprises a gasket, such as a rubber gasket, a silica gel gasket and an asbestos gasket, for enhancing the stability of the contact position; or the side of the object G to which the barrel is coupled, which is in contact with an external object, contains a spacer. Preferably, the design of the barrel satisfies: when a nail is loaded into the barrel, a portion of the shank of the nail extends out of the barrel. The protruding portion may be used for insertion into a hole of the object G.

In a sixth aspect, the invention provides an electric primer shooting device, which comprises a gun barrel and a remote control part, wherein the remote control part is used for controlling the on and off of a circuit. Preferably, the electric primer shooting nail bullet is also included. When the electric primer nail-shooting bullet is put into the gun barrel, and the electrode of the electric primer nail-shooting bullet is communicated with the electrode of the gun barrel, the electrode of the gun barrel is connected with the anode and the cathode of the battery, and when a remote control part is used for communicating a circuit, the electric igniter ignites the propellant powder, and the nail is shot out of the gun barrel. Preferably, the electric primer nail shooting device comprises a battery.

In a seventh aspect, the present invention provides an electric nailer comprising a barrel I, a firing pin, and a power component. The firing pin is used for striking the shooting nail, so that the primer can be fired, and then the shooting medicine works to shoot out the shooting nail. The power component is used for pushing the firing pin to strike the nail shooting bullet. Preferably, the electric nail gun comprises a remote control part IV, wherein the remote control part IV is used for switching on and off a remote control circuit so as to control the action of the power part. Preferably, the electric nail gun comprises a fixing part, wherein the fixing part is used for combining the remote control nail gun with an object to be fixed; preferably, the outlet of the gun barrel I comprises a gasket, such as a rubber gasket, a silica gel gasket and an asbestos gasket, for enhancing the stability of the contact position. Preferably, the design of barrel I satisfies: when a nail is loaded into the barrel I, a portion of the nail extends out of the barrel I. The protruding portion may be used for insertion into a hole of the object G.

In an eighth aspect, the present invention defines a remote controlled nailer, which is a device capable of remotely emitting nails. Including but not limited to the electric nailer, the electric primer nailer, which are remotely controlled. Preferably, the remote control nailer includes the fixing member.

In a ninth aspect, the present invention defines a device for fixing an object by remote control (simply referred to as a remote control fixing device) which can fix one object to another object by remote control. Such means of fixation include, but are not limited to, fixation with pins, rods (e.g., expansion bolts), or binding fixation. Such as driving nails into walls, metal sheets, timber weights. The structure of which includes but is not limited to any of the following: (1) remotely controlling a nail shooting device; (2) Means for driving the spike into an external object by remote control; (3) Means for inserting a sleeve of an expansion bolt into said hole by remote-control punching, and tightening the expansion screw; (4) strapping machine.

A remote controlled stapling apparatus is an apparatus capable of ejecting staples by remote control, including but not limited to: an electric primer nail gun capable of being controlled by a remote control, an electric nail gun capable of being controlled by a remote control, or a nail gun capable of being controlled by a remote control. The electric primer nail shooting bullet is a bullet which is ignited by current or voltage and can shoot nail-shaped objects; the electric primer nail shooting device is a device capable of igniting and shooting nails by voltage or current; the electric nail gun is a device capable of emitting nails in an electric control mode; the remote control nail gun refers to a device capable of emitting nails in a remote control mode.

Preferably, the remote control fixing device comprises an object to be fixed (simply referred to as an object G), which is used for fixing the object G to other objects by means of an object capable of ejecting a nail. As a further preferred feature, the object G comprises a hole (including a blind hole) having a diameter smaller than the diameter of the nail head of the nail or the spike, such that the nail or the spike shank passes through the blind hole but the nail head does not. In this way, the object G can then be fixed by the nail or the spike. As a further preference, the cartridge or cartridge containing the spike is mounted in the barrel by an interference fit prior to firing to prevent falling. As a further preference, the cartridge or cartridge containing the spike is mounted in the barrel by a magnet attraction force prior to firing to prevent falling. The object G is an object to be fixed, including but not limited to a device for extinguishing fire in the present invention, such as a glass breaking device, a spraying device, a smoke discharging device, a rack system. As a further preference, the object G has a pressure sensor on a side for contact for detecting a pressure with an external object before the fixing operation. And after the pressure reaches a certain value, performing operations such as nail shooting and the like. The object G includes, but is not limited to, a device for fire protection in the present invention. The pressure sensor includes, but is not limited to, a diaphragm pressure sensor.

In a tenth aspect, the present invention provides a suction cup, which refers to a disk capable of being combined with a foreign object through mechanical force or electromagnetic force, including but not limited to a vacuum suction cup and an electromagnet. The vacuum sucker comprises a sucker main body and an air pipe, and the air pipe is used for exhausting air; preferably, the vacuum chuck comprises a compressible porous (through-hole) material, such as a sponge, which is secured to the suction side of the vacuum chuck.

Preferably, the suction cup contains or has attached thereto one or more of the following: the electric primer nail shooting bullet, the gun barrel, the remote control nail shooting gun and the remote control fixing device. Such suction cups are simply referred to as suction cups with fixtures. Thus, the sucker with the fixing device can be primarily combined with an external object through components such as a vacuum sucker, an electromagnet and the like, and then the electric primer nail shooting bullet, the gun barrel, the remote control nail shooting gun or the remote control fixing device is further fixed, so that the combining capacity and the loading capacity are enhanced. As a further preferred aspect, the sucker comprising the fixing device sucker is combined with the electric primer nail gun, the gun barrel, the remote control nail gun or the remote control fixing device by an ABA mechanism, so that the sucker can be conveniently separated from the electric primer nail gun, the gun barrel, the remote control nail gun or the remote control fixing device.

In an eleventh aspect, the present invention defines a joint pipe comprising a tubular body having on its inner or outer wall a structure for connecting to the plug, pipe, hose or other water pipe joint, including but not limited to grooves, recesses, annular protrusions, snaps, threads. In a twelfth aspect, the present invention defines a spray system. The spraying system is a system capable of spraying water and cooling. In a thirteenth aspect, the invention defines a pipe holding system comprising a pipe holding mechanism, which means a mechanism capable of clamping, unclamping, fixing, moving, tilting or rotating a tubular. In a fourteenth aspect, the present invention defines a positioning/orientation system, which refers to a system that can be used to position, or orient, or change the position of an object, or change the orientation of an object. Including but not limited to: a linear motion part and a rotary motion part. The linear motion component is a component with a movable block capable of performing linear motion and comprises a sliding table, a push rod and an electric lifting table. The rotary motion component comprises, but is not limited to, a motor and a steering engine.

In a fifteenth aspect, the invention provides an electric gripper, which comprises a gripper head, a connecting rod, a power mechanism and a pull rope. The electric gripper comprises a gripper head, a connecting rod and a power mechanism, wherein the gripper head is arranged at one end of the connecting rod, and the power mechanism is used for controlling the opening and closing actions of the gripper head. Preferably, the electric gripper comprises a gripper head, a connecting rod, a power mechanism and a pull rope; the grabbing head is arranged at one end of the connecting rod, and the power mechanism is connected to the other end of the connecting rod; the power mechanism pulls the pull rope, and the pull rope pulls the grabbing head to achieve grabbing and releasing functions. The power mechanism comprises, but is not limited to, a winding mechanism, and the winding mechanism is adopted to realize the winding and unwinding of the pull rope, so as to control the grasping and loosening of the grasping head. With this structure, the mass of the gripper is reduced as much as possible, and the gripper is suitable for the situation that a light gripper is required, such as the situation that an unmanned aerial vehicle carries an electric gripper. Preferably, the surface of the connecting rod is smooth, so that the movable block can be sleeved on the connecting rod to slide, and the movable block comprises, but is not limited to, a sleeve, a linear bearing and a sliding block.

In a sixteenth aspect, the present invention provides a connection system for connecting or joining together an aircraft body or an aircraft system with an external object.

The invention provides a connection system I, which is characterized in that the connection system I comprises: one or more shafts. By shaft is meant an object having a ratio of length to square root of cross-sectional area greater than 10. The shaft may be used to provide support for moving solid objects.

Preferably, the shaft is not used to provide support for the unmanned aerial vehicle rotor or the drug delivery device, and is not used as a passage for powder or fluid. Preferably, the shaft includes a through hole. Preferably, the shaft comprises or functions as a guide rod or rail for transporting objects, including but not limited to prismatic slide rails, cylindrical slide rails, ball rails, roller rails, L-shaped rails, U-shaped rails. Preferably, the cross-section of the shaft includes, but is not limited to, circular, square, L-shaped, irregular, or U-shaped. Preferably, the connection system contains one or more of the following components: the AB type mechanism or the ABA type mechanism.

The invention provides a connection system II, which is characterized in that the connection system II comprises: ABA mechanism.

Preferably, the connection system I contains one or more of the following components: the AB type mechanism, the guiding and positioning component, the distance detector, the camera, the infrared detector, the thermal imaging detector and the electric gripper. The AB type mechanism is fixed at one end of the rod-shaped object and is used for combining the connecting system I to an object outside the aircraft system in an AB type combination mode; as a further preference, the linking system I contains the ABA type mechanism.

The connection system may be used to connect or join together an aircraft body or an aircraft system with an external object.

In a seventeenth aspect, the present invention provides a transportation system. The transport system is for moving an object. Preferably, the transport system transports the object from the aircraft or the aircraft system to the outside. Preferably, the transport system includes a transport unit and a transport power mechanism. The transport component includes, but is not limited to, one or more of a crane, the linear motion component, a movable block of the linear motion component, a linear bearing, a crane. The transport power mechanism can provide power for the transport component and drive the transport component to move. The transport power mechanism includes, but is not limited to, an electric motor, the winding mechanism. The winding mechanism moves the transport component through a pull rope.

Preferably, the transport system contains one or more of the shaft, the ABA mechanism, the connection system, and the motorized gripper. The transport member may be movable from one end of the shaft to the other.

Preferably, the transport system comprises a rail (or guide bar) over which the transport member is nested, forming a pair including but not limited to a mobile pair or a rolling linear rail pair. As a further preferred aspect, the transport component contains or is connected to the ABA mechanism.

Preferably, the transportation system further comprises a winding mechanism with double grooved wheels and a fixed pulley. The fixed pulley is assembled at one end of the rod-shaped object, the winding mechanism comprising the double grooved wheels is assembled at the other end of the rod-shaped object, and winding directions of two grooves on the double grooved wheels are opposite, so that when the double grooved wheels rotate, one groove is used for winding up, and the other groove is used for paying off. The stay cord in one groove is directly connected with one end of the transportation component, and the stay cord in the other groove is connected with the other end of the transportation component after bypassing the fixed pulley, so that the movement of the transportation component can be controlled through the double grooved wheels.

Preferably, the transportation system comprises a spring and the winding mechanism, one end of the spring is connected to the base of the winding mechanism, the other end of the spring is connected to the rod-shaped object, and the spring is used for tightening a pull rope of the winding mechanism, so that the pull rope keeps tension and avoids loosening.

Preferably, the transportation system adopts a motor with a self-locking function.

The transport system may be used to: transporting objects from the aircraft or aircraft system to the outside of the aircraft system through a shaft or from one end of the shaft to the other, the transport route of the objects being outside the shaft.

Preferably, the transport system may be coupled to the support system using the AB-type coupling or the ABA-type coupling. Preferably, the transport system is for transporting solids. Preferably, the transport system transports devices, including but not limited to fire fighting related devices or equipment.

Preferably, the transport system transports the transported object from the aircraft or aircraft system to a precise location outside the aircraft or aircraft system. Preferably, the transporting method of the transporting system does not include transporting the object by throwing. Preferably, the objects transported by the transport system do not include liquid objects and powder objects. Preferably, the transportation system can reciprocate the object, namely, can transport the object in a direction away from the aircraft body, and can also transport the object to be close to the aircraft body. Preferably, the transport system is used for transporting equipment, and more preferably, the transport system is used for transporting fire extinguishing equipment or fire extinguishing devices. Preferably, the objects conveyed by the transport system comprise solids. Preferably, the transport system comprises a shaft for transporting objects from one end of the shaft to the other end of the shaft of the mechanical device. As a further preference, the mechanical device is an aircraft system or other carrying device.

In an eighteenth aspect, the present invention defines a blocking device that can be used to block glass fragments from falling out of a glass plane or building facade, or/and to block a window frame, or window, from air circulation when breaking glass.

The invention provides a blocking device I, which comprises (1) a blocking component and (2) one or two of the linear motion component and the rotary driving piece. The blocking member includes, but is not limited to, a baffle, a curtain. The use of the blocking member can prevent glass from falling outdoors when the glass is broken. The linear motion component is used for moving the blocking component, and when the glass is broken, the broken glass can be pushed into the room by moving the blocking component. The rotary driving piece is used for adjusting the included angle between the blocking part and the glass. Preferably, the blocking member comprises a high temperature resistant material, which is a material capable of withstanding temperatures of 100 degrees celsius, including, but not limited to, asbestos cloth, metal plates, silica gel, ceramics, glass wool, rock wool, perlite, rubber, metal plates or plastic plates coated with a high temperature resistant coating, plates covered with a high temperature resistant material, metal mesh, and hollowed-out metal plates. The baffle may be a composite plate, such as a two-layer plate of rubber and aluminum plate secured by bolts. For example, a metal mesh with a maximum pore size of less than 2 mm. Preferably, the baffle comprises one or more of the following plates of material: a plate of rigid material (abbreviated as rigid plate), a plate of elastic material (abbreviated as elastic plate), a plate of plastic material (abbreviated as plastic plate). By using an elastic or plastic plate, the glass can be pushed into the window frame to push the glass into the room even if the plate area is larger than the window frame. Preferably, the elastic plate or the plastic plate is arranged around the rigid plate, so that the baffle plate with the structure can be pushed into the window frame more conveniently, broken glass can be pushed off better, and air circulation is prevented.

The invention provides a blocking device II, which comprises a flowering water nozzle and can spray flowering water flow to prevent broken glass from falling out of a glass installation plane or a building outer elevation.

Preferably, the blocking means I comprise means for discarding the blocking member. Preferably, the curtain can be rolled up or unrolled, and the blocking device I comprises a device capable of supporting, rolling up and unrolling the curtain, including but not limited to a return gear structure, a motor, and a spiral spring.

Preferably, the blocking device I, II contains one or more of the AB-type mechanism, the bracket body, the positioning/orientation device.

At present, the breaking and disassembling of glass of high-rise buildings, particularly super high-rise buildings, is very careful, because falling glass fragments can cause injury to people and objects on the ground and water bands laid in the air during fire extinguishment. By adopting the blocking device, glass fragments can be reduced or even completely prevented from falling outside a building when the glass in the air is damaged; after damaging window frame glass and extinguishing fire, the fire-extinguishing device can be used for blocking air circulation and reducing the re-burning risk, and no means similar to the method for blocking air circulation exists at present.

In a nineteenth aspect, the present invention defines a glass breaking device, which is a device capable of breaking glass. Comprising the following steps: (1) Broken glass body, broken glass body can directly act on glass, destroy glass. The broken glass body comprises, but is not limited to, a hammer head, a metal bead, a metal rod, a bullet and a sharp object. Preferably, the broken glass body contains a sharp part, and is made of a hard material with hardness higher than that of glass, wherein the hard material comprises, but is not limited to, diamond, artificial diamond, tungsten steel, high-carbon steel and alloy steel, and the hammer head is used for generating interaction with the glass and breaking the glass; (2) The glass breaking power device is used for enabling the glass breaking body to move, act on glass and break the glass. The glass breaking power device comprises but is not limited to the following devices: the linear motion part and the impact device. For example, the tungsten steel tip is fixed on a sliding block of the sliding table, and the sliding table can drive the tungsten steel tip to act on glass to damage the glass. The impact device refers to a device capable of enabling an object to accelerate suddenly, and comprises, but is not limited to, an ejection device, a rotation device, a gun-type spring device, an explosion device and a gunpowder device. The ejection device is a device capable of ejecting the broken glass body and enabling the broken glass body to generate linear motion in the air. The rotating device is a device capable of rotating the broken glass body. The explosion device refers to a device which can explode and generate an object which can impact and break glass after explosion. The gun-type spring device is a device capable of enabling an object to accelerate suddenly after spring energy storage and spring release.

The invention provides a glass breaking device I, which comprises a motor, a cam, a spring, a glass breaking body and a push rod. The principle is as follows: the motor is adopted to drive the push rod to rotate, so that the cam compression spring with limited rotation is pushed, and after the push rod rotates to pass through the high position of the cam profile, the spring ejects the cam out to drive the broken glass body to impact and break glass.

The invention provides a glass breaking device II, which comprises a motor, a connecting rod and a hammer head. The hammer head is installed at two ends of the connecting rod, the motor is adopted to drive the hammer head to rotate, and glass is broken through the hammer head.

Preferably, the glass breaking device includes the linear motion member, and the glass breaking body is moved by the linear motion member. Preferably, the glass breaking device comprises one or more of the following objects: the AB-type mechanism, the blocking member, the blocking device, the spraying system, the positioning/orientation system, the holder body described below, the smoke evacuation device described below. The spraying system is used for cooling the glass breaking device. The blocking component is used for blocking the window frame of broken glass and blocking air circulation. The blocking device can prevent broken glass from falling outside the building when the glass is broken. For example, when breaking glass, the baffle or the curtain of the blocking device can be used to close to the outer surface of the glass, and when the glass is broken, the linear motion component is used to push the baffle or the curtain into the room, so that glass fragments can be pushed into the room. Or the water for blowing flowers is sprayed from outside to the glass when the glass is broken, so that the glass is flushed into the room by water flow after the glass is broken. As a further preferred feature, the linear motion member is used to control the blocking member, or the blocking device.

In a twentieth aspect, the present invention defines a spray device comprising a nozzle from which water (or other fluid) can be sprayed after a source of water (or other fluid) under pressure is communicated.

The present invention provides an injection device I comprising: a nozzle and one or more of the following: the glass breaking device is characterized in that the glass breaking device is provided with the AB type mechanism, the support body is provided with the blocking component. The AB type mechanism is used for combining the spraying device I to other objects; the bracket body is used for supporting the spraying device I; the blocking component is used for blocking the window frame to avoid or reduce air circulation after water spraying and fire extinguishing; the glass breaking device is used for breaking glass before spraying water. As a further preference, one or more of the following means are also included: the blocking device, the spraying system, the positioning/orientation system. The blocking device is used for blocking glass from falling to the outer side of a building when the glass is broken; the spraying system is used for spraying water for cooling; the positioning/orientation system is used to move the spraying device I or change the spraying direction.

The invention provides a spraying device II which comprises a flowering water nozzle, so that the flowering water flow can be sprayed to prevent broken glass from falling out of a glass installation plane or a building outer elevation.

Preferably, the spraying device comprises one or more of the following components: a remote control switch, a multifunctional water gun, a smoke exhausting device, a bracket system, a glass breaking device and a blocking device; the remote control switch can be used for controlling the on/off of the waterway; the multifunctional water gun is used for controlling the type of sprayed water spray, for example: straight water, flowering water and spray water.

In a twenty-first aspect, the present invention defines a smoke evacuation device that is operable to evacuate smoke and that may be used to evacuate smoke from a room. The invention provides a smoke exhaust device I, which is preferable to be provided with a motor, blades and a base, wherein the blades can be driven to rotate by the motor, so that the smoke exhaust function is realized; the base is used for supporting the motor. Preferably, the smoke exhaust device I is composed of a fan and an accessory structure, and the fan comprises a motor and blades. Preferably, the smoke device I comprises a direct current motor, and the direct current motor is adopted to drive the blades to rotate; preferably, the smoke device I comprises an alternating current motor, and the blade is driven to rotate by the alternating current motor. Preferably, the smoke exhaust device I comprises an outer cover, an air inlet and an air outlet, so as to enhance smoke exhaust efficiency. Preferably, the blade is made of a material with a melting point or a softening point of 200 ℃ or more; as a further preference, the blade is made of a material having a melting or softening point above 600 degrees celsius, including but not limited to steel, iron, titanium, and alloys containing titanium. Preferably, the smoke exhaust device I is an axial flow type fire-fighting smoke exhaust fan. Preferably, the air inlet of the smoke exhaust device I comprises a mesh enclosure, and the mesh enclosure can be used for placing larger objects into the air inlet of the smoke exhaust device I. Preferably, the smoke evacuation device I is provided with or fixed to a filter element for blocking particulate matter in smoke from being expelled into the atmosphere. Preferably, the smoke exhaust device I comprises a supporting seat, a sleeve, a connecting sleeve, a motor, a blade and a connecting tail sleeve; the supporting seat is used for being fixed with other objects, supporting the sleeve and the motor, and the motor is used for driving the blades to rotate; the inner cavity of the connecting tail sleeve is an air outlet. As a further preference, the connector sleeve is movable relative to the support sleeve. Preferably, the row performance device I comprises a supporting seat, a sleeve, a motor and blades; the sleeve or the supporting seat is fixedly connected with a guide cover, the motor is arranged in the guide cover, a gap is reserved between the motor and the inner wall of the guide cover, and the guide cover is supported by adopting a heat insulation material. For a specific structure and a specific setting mode of the air guide sleeve refer to patent CN 218971501U. Preferably, the air guide sleeve is made of a material with a melting point or a softening point higher than 600 ℃.

The smoke exhaust device can be used for exhausting smoke and can be used for exhausting the smoke from a specific space; for example, smoke from a room is drawn out of the room or out of a building. The fume extractor can be integrated with the transport system, or can be carried by an aircraft or aircraft system, or can be integrated to the support system, or contains the AB mechanism. The AB mechanism may couple the fume extractor to the transport system, the support system, or the like. Preferably, the smoke evacuation device I includes the ABA type mechanism.

Preferably, the smoke exhaust device I comprises a mounting seat or a mounting bracket for fixing or supporting the fan.

Preferably, the fume extractor I includes a glass breaking device. The glass breaking device is used for breaking glass before smoke is discharged. As a further preferable aspect, the smoke exhaust device I further includes the linear motion member, and the glass breaking device is controlled to move by the linear motion member.

Preferably, the fume extractor I comprises a spraying system. The spraying system is used for spraying water or spraying liquid for cooling. The spraying system can spray water or cooling liquid for cooling, can cool high-temperature flue gas, and avoids the influence of the too high temperature on the normal operation of the fan; and can also be used for cooling fans. The water or coolant may be stored on the fume extractor I or may be transported from the outside through a pipe. For example, water or coolant may be transported from the building or the ground through pipes.

Preferably, the fume extractor I comprises a blocking device. The blocking device may be used to block glass fragments and/or to block air circulation. Preferably, the smoke exhaust device I further comprises a linear motion part, and the blocking device is controlled to move by the linear motion part.

Preferably, the fume extractor I comprises an ejector. Fire can be extinguished by spraying water through the water spraying device or glass fragments can be prevented from falling out of the building. Preferably, the device further comprises the linear motion component, and the ejector device is controlled to move through the linear motion component.

Preferably, the smoke evacuation device I includes an atomizer. The atomizing nozzle is used for cooling high-temperature air or cooling a motor and blades.

Preferably, the air inlet side of the smoke exhaust device I can be attached to a window frame.

Preferably, the air inlet side of the smoke exhaust device I contains an elastic object, such as sponge and rubber, for tightly fitting with a window frame and glass, so as to enhance the air exhausting effect.

Preferably, the smoke channel of the smoke discharging device I comprises a telescopic component, and the smoke discharging device I comprises the linear motion component; the telescopic part is driven by the linear motion part so as to control the distance between the air inlet of the smoke exhaust device I and the window frame, and the air inlet of the smoke exhaust device I can be attached to the window frame.

Preferably, the fume extractor I includes a drain hole through which liquid such as water can flow to avoid water accumulation.

Preferably, the smoke evacuation device I comprises a battery for powering a motor or other control device;

preferably, the smoke evacuation device I includes a wire for connecting to an external power source.

Preferably, the smoke exhaust device comprises one or more of a water pipe connector, a water pipe or a water hose, and the water pipe connector, the water pipe or the water hose is used for being connected with an external water source and supplying water to the spray head.

Preferably, the fume extractor I comprises a water tank for supplying water or other liquid, such as cooling liquid, extinguishing medium, to the spraying device or the spraying system, or comprises the pipe holding system, or is connected with a water pipe, or comprises a water pipe connection. The holding pipe system is used for being connected with an external valve and used for conveying water or other fire extinguishing media; the water pipe or the water pipe connector is used for communicating with an external water source or a fire extinguishing medium source.

In a twenty-second aspect, the present invention provides a stent system. The bracket system comprises the bracket body and an object supported by the bracket body and carried by the bracket body.

Preferably, the rack system contains one or more of the following: the system comprises an AB type mechanism, a glass breaking device, a positioning/orientation system, a pipe holding mechanism, a joint pipe, an electric valve, a rotary ball valve, a passive component, a spraying device, a spraying system, a blocking component, a blocking device and a smoke exhausting device. Preferably, the linear motion member is used to move one or more of the following: the glass breaking device, the spraying device, the joint pipe, the pipe holding system, the pipe holding mechanism, the spraying system, the passive component, the blocking component and the blocking device. The support body is used for supporting the device or the component, and the structure and the function of the device or the component are described in detail above and are not repeated here. The bracket system may be coupled to a building or building attachment by the AB style mechanism.

Preferably, the stent system further comprises one or more of the following: the system comprises an ABA mechanism, a control box, a thermal imaging instrument and a camera. The control box is used for placing objects such as motor control parts, batteries and the like.

Preferably, the stent body is made of a lightweight, high strength or heat resistant material including, but not limited to, aluminum alloy, steel, titanium alloy, carbon fiber or other composite material coated with a fire retardant coating.

Preferably, the electric grab, the connection system, the transportation system, the blocking device, the glass breaking device, the spraying device, the smoke discharging device, the bracket system comprise one or more of the following components: an electric primer nail gun, a gun barrel, a remote control nail gun, a remote control fixing device and a sucker; these components are used to secure the device or system to other objects. As a further preferred aspect, the electric gripper, the connection system, the transportation system, the blocking device, the glass breaking device, the spraying device, the smoke discharging device, and the support system are provided with any one or two of a pressure sensor and an elastic object, wherein the pressure sensor is used for detecting the pressure of the contact part of the fixing part and an external object, and the elastic object comprises, but is not limited to, a gasket made of a sponge, rubber or other substances and is used for being placed between two objects to be fixed.

In a twenty-third aspect, the present invention provides an aircraft system. Comprising the following steps: (1) Aircraft bodies, hoverable aircraft bodies, including but not limited to rotary wing aircraft, tilting wing aircraft, are employed in the present invention. (2) J parts. The J-section is used to contact, connect, couple, clamp, secure or join the aircraft system in the air with a target object. The target object is an object, such as a building, the support system, a person, other than the aircraft system, with which the aircraft system is intended to contact, connect, couple, clamp, secure or join. The J-piece includes, but is not limited to, the AB mechanism, the shaft.

Preferably, the unmanned aerial vehicle system contains one or more of the following objects: the device comprises a support body, a support system, a connecting system, a transportation system, a glass breaking device, a positioning/orientation system, a spraying device, a joint pipe, an accurate structure, an electric valve, a rotary ball valve, a winding mechanism, a cross-platform pipe connecting structure, a transportation system, a pipe holding mechanism, an electric grabbing device, an ABA type mechanism, a spraying system, a blocking part, a passive part, a blocking device and a smoke exhausting device. As a further preference, the linear motion member is employed to move one or more of the following: the device comprises a blocking component, a glass breaking device, a spraying device, a joint pipe, a pipe holding system, a pipe holding mechanism, a spraying system, a blocking device, a passive component and a smoke exhausting device. The structure and function of these devices or components are described in detail above and are not described in detail herein. Preferably, the object on which the aircraft system is mounted includes one or more of the following components: the electric primer nail gun comprises an electric primer nail gun body, a gun barrel, a remote control nail gun, a remote control fixing device and a sucker, and is used for being combined with an external object.

Preferably, the aircraft is an unmanned aircraft, i.e. an unmanned aircraft.

Preferably, the aircraft system comprises the shaft of the connection system, the length of the shaft being greater than 2 times the wheelbase of the aircraft body when the aircraft body is of the rotary wing type.

Preferably, the aircraft system comprises a water hose or a water pipe, the rod-shaped object and the spraying device, one end of the rod-shaped object is fixed on the aircraft body, one end of the water hose or the water pipe is communicated with a nozzle of the spraying device, the other end of the water hose or the water pipe is combined to one end, far away from the aircraft body, of the rod-shaped object by adopting the ABA type mechanism, or the other end of the water hose or the water hose is connected with the joint pipe, and the joint pipe is combined to the rod-shaped object by adopting an AB type combination mode.

Preferably, the aircraft system comprises the connection system, the transport system and the support system. The rack system is coupled to the transport component of the transport system with the ABA mechanism, transported from the aircraft system by the transport system, and coupled to an external object with the AB mechanism.

Preferably, the aircraft system includes the transport system and the smoke evacuation device. The fume extractor is mounted on the transport system or coupled to the transport system by an ABA mechanism, and the fume extractor can be moved by the transport system or moved by the transport system and coupled to an object external to the aircraft system. As a further preference, the aircraft system also contains the connection system.

Preferably, the unmanned aerial vehicle system comprises one or more of the following components: an electric primer nail gun, a gun barrel, a remote control nail gun, a remote control fixing device and a sucker; these components are used to secure the object to be secured (object G) on the drone system to an object outside the drone system. As a further preferred feature, the aircraft contains components that are capable of bonding to external objects, including but not limited to bonding by mechanical or electromagnetic forces, including but not limited to bonding by mechanical, electromagnetic means, such as clamping, gripping, suction, clamping, and the like. Preferably, the aircraft comprises an AB or ABA type mechanism. Preferably, the aircraft comprises a suction cup or suction system, an electromagnet. The adsorption system comprises a sucker, a vacuum pump and an air pipe, and the sucker and an object outside the aircraft are adsorbed together in a mode of exhausting air through the vacuum pump. The sucking disc is used for adsorbing to the outside object of unmanned aerial vehicle system, the trachea is connected the vacuum pump with the sucking disc. The aircraft system may be coupled to ferromagnetic objects outside the aircraft by the AB-type mechanism or the ABA-type mechanism. As a further preferred aspect, the suction cup is fixed at the end of the connection system or shaft (the end far away from the aircraft), the vacuum pump is fixed at the end near the aircraft body or fixed on the aircraft body, and the suction cup is communicated with the vacuum pump through the air pipe. As a still further preferred aspect, the suction cup comprises a compressible porous object (e.g. a sponge) on the side for suction. Thus, when the vacuum pump is used for pumping, the sucker can be adsorbed on not only smooth objects, but also rough objects such as walls; when the suction is stopped, the suction cup can be separated from the adsorbed object. Such an aircraft system may be used as a means for airborne object fixation. As a further preference, the aircraft system further comprises one or both of said connection system, said transport system. The fixation device may be transported by the transport system. As a further preferred feature, the aircraft system comprises the positioning and orientation system by which the electric primer cartridge, barrel, remote nailer, remote fixture, suction cup or the object G can be moved or turned. Preferably, the side of the object G facing the object W contains a spacer, which is elastic or compressible, which helps to enhance the stability between the two when the object G is pressed onto the object W. As a further preferred feature, the object G contains a blind hole in which a portion of the nail or spike is placed and which has a smaller diameter than the head of the nail or spike so that when the nail or spike is fired, a shank passes through the blind hole to secure the object G to the object W. The blind holes are used for placing the shooting nails or nails to fall out.

Preferably, the aircraft system comprises the sucker with the fixing device, wherein the sucker with the fixing device is combined with the electric primer nail gun, the gun barrel, the remote control nail gun or the remote control fixing device by adopting an ABA mechanism, or the sucker with the fixing device is combined with the aircraft system by adopting an ABA mechanism. In this way, the aircraft system can be disengaged from the electric primer cartridge, the barrel, the remote nailer, or the remote fixture, or the aircraft system can be disengaged from the fixture-containing suction cup. The aircraft system can perform fixing operation in the air, fix objects in the air, be used for replacing manual air operation, and also can enter places which are difficult to reach or cannot reach by people to perform fixing operation.

Preferably, the aircraft system comprises an aircraft body and the object G, wherein the unmanned aerial vehicle body and the object G are combined by adopting an ABA mechanism; the object G contains AB-type bonding means for bonding to the object W. The aircraft system contains ABA-type mechanisms for coupling to, decoupling from, or for coupling to, or decoupling from the object W or an object in the vicinity of the object W. As a further preference, the means for fixing the object G comprises a pressure sensor. As a further preferred aspect, the means for fixing the object G includes a pressure sensor for detecting a pressure at which the means for fixing contacts an external object, and a remote control nail shooting device.

Preferably, the aircraft system comprises one or more of the following components (hereafter replaced by component X): the device comprises a bracket system, a spraying device, a glass breaking device, a smoke exhausting device and a blocking device. The component X is combined on the body of the aircraft system through the ABA type mechanism, and the combination and the separation of the aircraft body and the component X can be controlled by controlling the ABA type mechanism. The ABA type mechanism III is contained on the component X, and the combination and the separation of the component X and an external object can be controlled by controlling the ABA type mechanism III.

Uses for the aircraft system include, but are not limited to: (1) For moving the mounted object out of the aircraft system through a shaft; (2) For connecting the water connection carried on to a water connection outside the aircraft system, for transporting and coupling the fire extinguishing device carried on or the spraying device to a building or an accessory of a building; (3) Transporting and coupling any one or more of the following mounted devices to an object (e.g., a building) external to the aircraft system: the fire extinguishing device, the spraying device, the support body, the support system, the pipe connection structure, the water pipe connector, the pipe holding system, the spraying system, the blocking component and the blocking device.

With the aircraft system according to the invention, objects on the aircraft system can be transported outside the aircraft. Preferably, the aircraft system can be connected to external objects, objects on the aircraft system can be transported precisely to external locations, and the devices listed above in the aircraft can be carried on and transported. Preferably, the aircraft system also allows the above-described devices to be combined with external objects and perform related tasks including, but not limited to, breaking glass, spraying liquids, blocking glass debris from falling, blocking air flow, water spray cooling, water piping, opening water valves, object positioning or orientation, and the like. The aircraft system can be applied to fire fighting, fire extinguishing, air transportation, air operation and the like. Preferably, the object on the aircraft system that can be transported outside the aircraft comprises a solid.

In a twenty-fourth aspect, the present invention provides a pole setting system comprising a pole setting for supporting an object. Preferably, the pole setting system further comprises one or more of the following: rods, rings, plates. Preferably, the pole setting system further comprises a valve. Preferably, the pole setting system is used to support or incorporate fire extinguishing apparatus, or other apparatus transported by an aircraft. Preferably, the pole system can be combined by means from outside the building using an AB-type mechanism. Preferably, the pole setting system is used to support objects conveyed by the aircraft, including but not limited to the various devices or systems of the present invention. Preferably, the pole system is used to support an aircraft or an object on an aircraft, including but not limited to the various devices or systems hereinafter. Preferably, the upright rod system comprises a limiting component or a guiding and positioning component. The limiting component is used for limiting the movement or rotation of an object, such as a limiting rod, a groove and a boss. The guiding and positioning component refers to a component which can guide an external object from a larger space into a smaller space or can guide and position a rod-shaped object and a ring-shaped object or limit the position, and comprises, but is not limited to, a rod, a V-shaped groove, a flaring groove, an object with a conical surface, a needle-shaped object, a rod-shaped object, a ball-shaped object and a ring-shaped object. The guiding and positioning means facilitate positioning of objects associated with the pole setting system. Preferably, the pole setting system has one or more of the following features: only for supporting fire extinguishing devices, not for supporting objects at rest on average, only for fire-fighting use, only for supporting objects from the aircraft, without impeding the operation of the supported devices or equipment. Preferably, the arrangement and size of the pole system is compatible with the arrangement of the AB mechanism of the object to be supported and does not hinder the operation of the object being supported. Preferably, the pole setting system is a stand comprising a plurality of poles. Preferably, the pole setting system is constructed of a material having a melting point of 500 degrees celsius, or a softening point of 300 degrees celsius or more, including but not limited to steel, aluminum alloys. The upper part of the upright rod system comprises a frame which can be used for combining a three-dimensional frame transmitted by an aircraft. Preferably, the upper surface of the pole system comprises a planar frame which may be used in conjunction with a top-down drop down stereoscopic frame delivered by an aircraft.

The invention provides a vertical rod system I, which comprises a vertical rod and a three-dimensional frame, wherein the three-dimensional frame is fixed on the vertical rod. The pole setting system I may be arranged on the ground or on a building. Preferably, the stereoscopic frame can be used to support or incorporate an aircraft system, or an object transported from an aircraft system; as a further preference, the space frame can be used to support or incorporate an aircraft system, or fire extinguishing equipment transported from an aircraft system, for fire fighting and extinguishment. Preferably, the stereoscopic frame can be used to support or incorporate the connection system, or the transport system. Preferably, the upright system I further comprises a pipe, a water pipe joint or a valve; the water pipe connector or the valve is used for being connected with a water pipe connector transported by an aircraft. Preferably, the water pipe connector or the valve comprises a male connector or a female connector in the quick connector for connecting with a water pipe connector carried by an aircraft.

The invention provides a pole setting system II, which comprises a plurality of pole setting systems I. Preferably, the upright systems I comprise valves or water pipe joints, and the valves or the water pipe joints between the upright systems I are communicated through pipelines. As a further preference, the upright system I comprises a valve or water connection connected with a water source, a fire extinguishing medium source or a water pump by a pipeline. In this way, fire extinguishing medium can be supplied to the valve or water connection, if desired. The pole setting system II can be used for extinguishing fire of houses, structures and other objects, such as petroleum storage tanks, old communities, thousand-family villages and forests. The current fire truck in the latter three places is difficult to enter and fire is difficult to extinguish. The vertical rod system II is arranged in a forest, so that the upper surface of the water forest can be poured downwards, the water quantity is sufficient, the response is rapid, fire can be extinguished in places which cannot be reached or are difficult to reach when a fire is on, and the fire extinguishing effect is better than that of currently commonly adopted manual fire extinguishing.

In a twenty-fifth aspect, the present invention provides a building comprising a house and a structure, the structure comprising: (1) a building body; (2) any one or more of the following components or structures: the fire-fighting system comprises a supporting system, a valve, a window frame I, a fire-fighting system, a guiding and positioning component, a building curtain wall and a vertical rod system. The support system or the upright rod system is fixed on the outer surface, the outer wall, a window, a balcony and a roof of the building or on the appendages of the outer surface, the outer wall, the window, the balcony and the roof. The water outlet of the valve is arranged on the outer surface of the building or the outer side of the outer elevation or in the area where the window and the balcony of the building are positioned. So that the water connection can be coupled with the water outlet of the valve from the outside of the building facade. And the water inlet of the valve is communicated with the fire-fighting vertical pipe. Preferably, the valve is an electric valve, and the electric valve is electrically connected with a fire-fighting power supply. As a further preference, the operating voltage of the electrically operated valve does not exceed 36V. Preferably, the valve is the pull valve. Preferably, the opening of the pipe section where the water outlet of the valve is located is downward. As a further preference, the axis of the outlet pipe of the valve is vertically downward. Preferably, the valve is used to couple a water connection transported from an aircraft.

Preferably, the building comprises one or more of (a) a building curtain wall, (b) a valve, the support system, and the pole setting system; the valve and the support system are fixed on the building body, and the outermost end of the support system is arranged outside the building curtain wall. Preferably, the shortest distance between the valve and the window frame is less than 20 meters; as still further preferred, the shortest distance between the valve and the window frame is less than 5 meters; as a still further preferred aspect, the shortest distance between the valve and the window frame is less than 1 meter.

Preferably, the building contains the support system and the shortest distance between the support system and the window frame is less than 3 meters; as a further preference, the shortest distance between the support system and the window frame is less than 1 meter. As a still further preference, the shortest distance between the support system and the window frame is less than 0.3 meters.

Preferably, the building comprises the pole setting system. The device that can be used to combine unmanned aerial vehicle system to convey is used for operations such as fire control, especially can be used to the outer wall extinguishment. Preferably, the building roof is provided with said pole setting system or said support system.

The use of the building may be advantageous for extinguishing fires with the aircraft system or for transporting objects from the aircraft system to the building.

In a twenty-sixth aspect, the present invention provides an apparatus or device comprising one or more of the following: an electric primer nail gun, a gun barrel, a remote control nail gun, a remote control fixing device and a sucker; as a further preferred feature, the spraying device comprises a mounting plate or bracket for supporting the spraying device, the mounting plate or bracket comprising thereon one or more of the following: an electric primer nail gun, a gun barrel, a remote control nail gun, a remote control fixing device and a sucker. Preferably, the injection device comprises a pressure sensor on the part for fastening. As a further preference, the means for securing of the device or apparatus comprises a pressure sensor for detecting the pressure at which the means for securing is in contact with an external object. The apparatus or device may be transported by the aircraft system and combined with other objects.

In a twenty-seventh aspect, the present invention provides a fixing method, which is based on the principle that: one or more of the electric primer-firing cartridge, the gun barrel, the remote-control-firing gun, or the remote-control-fixing device is mounted or fixed on an object (object G) to be fixed, the object G is abutted against or combined with an external object (object W), and then a firing pin of the electric primer-firing cartridge, the gun barrel, the remote-control-firing gun, or the remote-control-fixing device, or other pins, or other objects for fixing are controlled to enter the object W, so that the object G is fixed with the object W by the firing pin, the pins, or other objects for fixing.

Preferably, the electric primer shooting device, the gun barrel, the remote control shooting gun or the remote control fixing device is controlled in a remote control mode. Further preferably, the object G has a blind hole, the diameter of which is smaller than the diameter of the head of the nail, and the part of the remote control nail gun exposed when the remote control nail gun is fixed to the object G is inserted into the blind hole of the object G. Thus, when the nail is fired, the object G is fixed to an external object through the hole; more preferably, the nail shooting body is in clearance fit with the blind hole. It is further preferred that the cartridge or cartridge containing the spike is mounted in the barrel by an interference fit or by magnetic attraction.

Preferably, the AB type mechanism, the suction cup, the ABA type mechanism, or other combination means are used to combine the object G with the object W or an object adjacent to the object W before the nail or other nail is emitted, and then the remote control setting device or the remote control fixing device is used for fixing.

Preferably, the fixing method adopts the sucker with the fixing device, firstly performs preliminary combination with an external object through the sucker with the fixing device, and then adopts the electric primer nail shooting bullet, the gun barrel, the remote control nail shooting gun or the remote control fixing device to perform further fixation so as to enhance combination capacity and loading capacity.

Preferably, the fixing method further includes: before fixing, the pressure value between two objects to be fixed is measured by a pressure sensor, and after the pressure value reaches a certain value, the two objects to be fixed are fixed by a remote control nail shooting device.

Preferably, the fixing method includes: punching by a punching device, plugging an expansion bolt sleeve into the hole, and tightening the bolt.

In a twenty-eighth aspect, the present invention provides a method for fixing an aircraft, which is based on the following principle: and (3) adopting an aircraft system carrying one or more of the electric primer nail shooting bullet, the gun barrel, the remote control nail shooting gun, the remote control fixing device or the sucker, and adopting the aircraft transportation method to fly to a destination for fixing operation. For example, the firing pin or other object for securing may be fired by the electric primer firing pin, the barrel, the remote control nailer, the remote control securing device, or the suction cup. Preferably, the aircraft fixing method includes: the electric primer gun, the gun barrel, the remote control nail gun, the remote control fixing device or the sucker is fixed on an object (object G) to be fixed, then the object G is abutted against an external object (object W) or combined with the object W, and then the nail, the nail-shaped object or other fixed objects are used for fixing the object G and the object W together through remote control.

Preferably, the aircraft system is provided with the object G to be fixed, and one or more of the electric primer gun, the gun barrel, the remote control nail gun, the remote control fixing device, and the suction cup is mounted or fixed to the object (object G) to be fixed, so that the object G is abutted or combined with an external object, and then the fixing operation is performed. Further preferably, the object G has a blind hole, the outer diameter of which is smaller than the diameter of the head of the nail, and the nail exposed from the remote control nail gun is inserted into the blind hole of the object G when the remote control nail gun is fixed to the object G. Thus, when the nail is fired, the cord object G is secured to an external object through the hole. As a further preference, the cartridge or cartridge containing the spike is mounted within the barrel using an interference fit or a magnet.

Preferably, the aircraft system used in the aircraft fixing method includes the AB time mechanism or the ABA time mechanism, and the aircraft fixing method further includes: the AB or ABA type mechanism is used to join the aircraft system or object G to the object W or an object adjacent to the object W and to press the object G against the object W prior to the firing pin or other pin.

Preferably, the aircraft system used in the aircraft fixing method includes one or both of the connection system and the transport system, and the aircraft fixing method further includes: transporting an electric primer nail gun, a gun barrel, a remote control nail gun, a remote control fixing device, a sucker or the sucker with the fixing device through the transport system; the aircraft system may be coupled or contacted with an external object by the connection system.

Preferably, the aircraft system used in the aircraft fixing method includes the positioning and orientation system, and the aircraft fixing method further includes: and moving or rotating the object G, the electric primer nail gun, the gun barrel, the remote control nail gun, the remote control fixing device, the sucker or the sucker with the fixing device through the positioning and orientation system.

Preferably, the aircraft fixing method includes: (1) Carrying out object transportation by adopting the aircraft transportation method, and abutting the object G with an external object; (2) And controlling the remote control fixing device or the remote control nail gun to fix the object G on an external object.

Preferably, the aircraft fixing method further includes: the sucking disc is adopted for adsorption operation, and then the remote control fixing device or the remote control nail gun is adopted for fixing operation.

Preferably, the aircraft fixing method further includes: the pressure sensor is used for detecting the direct pressure of the object G and the object W, and the remote control nail shooting device is controlled to fix the object G and the object W after the pressure reaches a certain value (for example, 100 newtons).

Preferably, the aircraft fixing method further includes: the ABA type mechanism is adopted to combine an aircraft with the object W, then the object G containing the remote control fixing device is transported to the position of the object W and is abutted against the object W, the object G is fixed to the object W or an object near the object W through the remote control fixing device, other devices are transported to the position of the object W and are fixed with the object W through the remote control fixing device, then the remote control fixing device is separated from the aircraft body, and the aircraft body is controlled to be separated from the object G.

The aircraft fixing method can fix the object in a remote control mode, particularly can fix the object in the air, is particularly suitable for places which are difficult to be reached or cannot be reached by some people, and can be fixed on the object on the ground. Such as on buildings, on exterior walls of buildings on fire, on trees, on piers. By adopting the aircraft fixing method, the fire extinguishing equipment can be fixed on an object in the air in the fire extinguishing process.

The invention provides a transportation combination mode, which comprises the following steps: with the aircraft system comprising the component X, the component X is coupled to the body of the aircraft system by means of the ABA mechanism and then a target object X is flown, which contains components that can be coupled to the component X, for example the support system, the pole setting system, which are dimensioned and structured. The ABA mechanism III on the part X is controlled to bind to the target object X and then the ABA mechanism is controlled to disengage the aircraft body from the part X. This bonds the component to the target object X.

In a twenty-ninth aspect, the present invention provides a smoke evacuation method, the smoke evacuation method comprising: the smoke exhaust device is combined, fixed or supported on a building or other objects needing smoke exhaust through the transportation and the movement of the aircraft, and then smoke is exhausted through the smoke exhaust device.

Preferably, the fume extractor is coupled to, fixed to or supported by a window or window frame of a building or the periphery of the window or window frame, so that the fume extractor can extract fume through the window frame or window in which glass is broken.

Preferably, the smoke evacuation method further comprises one or more of the following operations: (1) breaking glass by the glass breaking device; (2) The blocking device is used for blocking glass fragments from falling outside the building; (3) Spraying water or other cooling liquid through the spraying system for cooling; (4) spraying fire extinguishing medium by the spraying device to extinguish fire; (5) Blocking indoor and outdoor air circulation through the blocking device; and (6) moving the air inlet to enable the air inlet to be attached to the window frame. Therefore, the air exhausting efficiency of the fan can be furthest exerted; (7) And fixing the smoke discharging device on a target position or a target object by adopting the aircraft fixing method. (8) The water inlet pipe of the injection device of the smoke exhaust device is communicated with an external valve through the pipe holding system; (9) Manually communicating a water pipe of the smoke exhaust device with an external water source; (10) The lead of the smoke exhaust device is communicated with an external power supply by adopting a manual mode; (10) The water pipe of the smoke exhaust device is communicated with an external fire extinguishing medium source by adopting a manual mode; (11) Manually communicating a water pipe of the smoke exhaust device with an external cooling liquid source; (12) Manually communicating a water pipe of the smoke exhaust device with an external pipeline; (13) The motor power line of the smoke exhaust device is communicated with an external lead by adopting a manual mode and is used for providing electric energy; (14) The wires and the water pipes of the smoke exhaust device are connected with the wires and the pipes outside the smoke exhaust device by adopting the manual work in the adjacent fireproof partition of the smoke exhaust room so as to provide electric energy, water, fire extinguishing medium, cooling medium and the like.

The smoke exhaust device or the smoke exhaust method can be used for directly exhausting smoke to the space in the building very flexibly. For example, the fume extractor may be mounted and transported by the aircraft system, and coupled to a support system on a building such that the air inlet of the fume extractor faces the window, and the fume extraction may be performed. The flue gas circulation path of the fixed type smoke discharging device in the existing building is long, and the smoke discharging efficiency is low. The smoke exhausting device can form negative pressure to exhaust smoke outside the building, and is safer than a positive pressure smoke exhausting device. The smoke exhaust device is very flexible to use, and the smoke exhaust device can be directly combined, fixed or supported to the outer wall of a room to be exhausted by adopting the technical scheme of the invention, and can directly exhaust smoke to the outside through a window with broken glass, so that the smoke exhaust path is short and the efficiency is high.

And if glass exists on the window, the glass can be broken by the glass breaking device, and the blocking device can be used for blocking the glass from falling outside the building when the glass is broken. In the smoke discharging process, the high-temperature smoke can be cooled by spraying water or cooling through the spraying system, so that the smoke is prevented from damaging a fan; the fan may also be cooled by a spraying system. At the end of smoke discharge or other needs, the blocking device can be used for blocking air circulation caused by the broken glass window frame, so that the re-burning risk is reduced. The smoke exhausting device can exhaust smoke at one side so as to spray water or other fire extinguishing media through the spraying device for fire extinguishing operation.

In the prior art, the glass is not easily damaged because the risk exists that the glass falls when the glass is damaged in a high-rise building. Even if the glass is damaged, smoke can be discharged naturally, and the damage to the glass can cause wind to blow into the room, damage the flow of smoke in the room and introduce fresh air to support combustion. However, the smoke evacuation device of the present invention not only can evacuate smoke, but also has no such drawbacks. In the prior art, a positive pressure fan can be adopted to discharge smoke, and the mode can influence the indoor smoke circulation and has certain danger for personnel entering the inner tap. The smoke exhaust device provided by the invention is used for forming negative pressure indoors, and smoke flows outwards towards a window, so that the smoke exhaust device is beneficial to the operation of inner attack personnel.

In a thirty-first aspect, the present invention provides a vehicle comprising a vehicle body containing the ABA mechanism for securing the aircraft system. Preferably, the vehicle comprises a water pump or means for securing a water pump. The water pump is used for supplying water for the aircraft system.

In a thirty-first aspect, the present invention provides a trailer comprising a trailer body containing the ABA-type mechanism for securing the aircraft system. Preferably, the trailer comprises a water pump or means for securing a water pump. The water pump is used for supplying water for the aircraft system.

By adopting the technical scheme of the invention, when one or more rooms of a building catch fire, if the temperature of a certain window is higher or a flame exists, the fire extinguishing device such as a nozzle and the like can be arranged in a nearby safe place, water is sprayed to the window for cooling, the fire extinguishing device such as other nozzles and the like is arranged at the position of the cooled window and the like, and then the indoor, the outer vertical surface or the outdoor object is cooled at the position. In particular, the technical solution of the present invention benefits from factors including, but not limited to: (1) The support system and the pole setting system can be installed in advance, (2) the aircraft fixing method can be adopted; therefore, the fire extinguishing device such as a nozzle and the like can be combined to a place which is not ignited in the middle of a fire scene and has proper temperature through an aircraft, the fire extinguishing medium is sprayed from the place to extinguish fire, and the fire extinguishing force combined with the fire extinguishing force outside the fire scene can be combined to extinguish fire. Of course, other fire extinguishing operations may be performed using other devices or equipment. However, fire extinguishment is generally only performed at the periphery of a fire scene, and the fire extinguishment personnel or ground equipment can not easily pass through the fire scene by gradually advancing from the periphery to the middle of the fire scene.

In a thirty-second aspect, the present invention provides a method for accurately positioning/orienting an aircraft (hereinafter simply referred to as the aircraft X method). The method comprises the following steps: the unmanned aerial vehicle system comprising the transport system is adopted, an object to be transported (simply referred to as an object X) is combined to the transport system of the unmanned aerial vehicle system in the ABA type combination mode, one end of the transport system is combined to the object to be combined (simply referred to as an object M) by adopting the ABA type mechanism, and then the object X is transported to one end close to the object M by adopting the transport system. Preferably, the X method further comprises one or more of the following steps: (1) bonding the object X to the object M using an AB structure; (2) The object X is moved or rotated using the positioning/orientation system. (3) disengaging the object X from the transport system.

Preferably, the object X is mounted on the positioning/orientation system. Preferably, the object X is mounted on a sub-platform, the sub-platform is moved by the transport system, and then the sub-platform is bonded to the object M using the AB bonding method. Preferably, the X method includes the fixing method or the aircraft fixing method, and the fixing operation is performed by using the fixing method or the aircraft fixing method.

In a thirty-third aspect, the present invention provides a method of screwing a nut (bolt, screw), in which a tool for screwing a nut (bolt, screw) is coupled to a position near the nut (bolt, screw) to be screwed, and the tool is coupled to the nut (bolt, screw) by the positioning and orientation system, and then the tool is controlled to rotate, so that the nut (bolt, screw) is rotated, thereby completing the screwing of the nut (bolt, screw). By the method for screwing the nuts (bolts and screws), the operation of screwing the nuts (bolts and screws) can be performed by using an aircraft in the air or in places inconvenient for people to reach.

In a thirty-fourth aspect, the present invention provides a nut (bolt, screw) twisting device for rotating a nut (bolt, screw). The nut (bolt and screw) screwing device comprises an AB mechanism, a motor and a nut (bolt and screw) screwing tool. The AB mechanism is used in conjunction with a nut (bolt, screw) to be screwed either directly or indirectly (i.e., the AB mechanism is not directly coupled to the nut, bolt, or screw, with other objects in between). Preferably, the screwing device comprises a support (to distinguish it from the support above, this support is called support B) on which the AB-type mechanism, screwing (bolting, screwing) tool is included. Further preferably, the bracket B includes the positioning and orientation system described above. Such nut (bolt, screw) screwing tools include, but are not limited to: screw driver, electric screw driver. The nut screwing (bolt and screw) tool is mounted on the positioning and orienting system, and the AB mechanism and the positioning and orienting system are mounted on the bracket B. The AB mechanism may be used to couple the bracket B to an external object. The device for screwing the nuts (bolts and screws) can be carried and transported by the aircraft system and can be used for screwing the nuts (bolts and screws) in the air or in places inconvenient for people to reach.

In a thirty-fifth aspect, the present invention provides a valve opening (closing) mechanism for opening or closing a valve. The valve opening mechanism comprises an AB mechanism, a motor and a rotary valve component (simply referred to as a rotary valve component). Preferably, the valve opening mechanism includes a bracket (for the purpose of distinguishing from other brackets of the present invention, the bracket is referred to as a bracket C). The support C comprises an AB type mechanism and a rotary valve component. The rotary valve assembly is used to drive the opening and closing rotation of the valve to open or close the valve, including but not limited to the rotary drive. As a further preference, the carriage C contains thereon the positioning and orientation system described above, the rotary drive being mounted on the positioning and orientation system. The AB mechanism may be used to couple the bracket C to an external object. The valve opening mechanism can be carried and transported by the aircraft system and can be used for opening (closing) valves in the air or in places inconvenient for people to reach.

In a thirty-sixth aspect, the present invention provides a can comprising a can body having a support thereon for supporting, connecting or incorporating one or more of the following: nozzle, squirt, support system, aircraft, connected system. Preferably, the distance between the position of the support for supporting and the tank body is greater than 1 meter. As a further preference, the location of the support for support is more than 2 meters from the tank. As a further preference, the location of the support for support is more than 5 meters from the tank.

In a thirty-seventh aspect, the present invention provides a valve opening method. The valve opening (closing) mechanism is combined on a valve supporting system through the AB type mechanism, and then the valve opening and closing mechanism is driven to rotate through the rotary valve component, so that the valve opening or closing function is achieved.

In a thirty-eighth aspect, the present invention provides a method of suppressing a fire. The fire extinguishing method comprises the following steps:

(1) Controlling the flight of the aircraft system comprising the fire suppression device to a destination location. The destination locations include, but are not limited to, the location of the connection hose, water pipe or fitting pipe, the location of the injection device or the bracket system to be incorporated, the location of the valve, the location of fire fighters, the location of the support system, other architectural appurtenances.

(2) The nozzle or the spraying device is in communication with a fire water source or other fire extinguishing medium source. The connection method includes, but is not limited to, the pipe holding system making connection, the aircraft take over method, or manual connection. The location of the source of extinguishing medium includes, but is not limited to, on-building, ground. Preferably, the source of extinguishing medium to which the spraying device is connected is on the building.

(3) The aircraft system, a portion of the aircraft system, or a fire suppression device is coupled to a target object using an AB coupling. The fire extinguishing device is a device for extinguishing fire, including but not limited to a glass breaking device, a spraying system, a smoke discharging device, a blocking device, a bracket system and a pipe holding system. The target object comprises the support system, a valve, an attachment of an outer building elevation or other objects which can be combined with the support system, the valve, the attachment of the outer building elevation in an AB type combination mode. In a specific operation, the steps (2) and (3) may be exchanged according to the actual situation. Preferably, the nozzle or the spraying device is bonded to the target object in an AB bond. Preferably, the stent system comprising a nozzle or the spraying device is used, and the stent system is bonded to the target object by an AB bonding method. Preferably, the connection system is used for binding the target object in an AB binding mode. Preferably, the attachment system is coupled to the target object using an ABA type mechanism.

(4) And opening a valve for controlling water or other fire extinguishing medium, so that the water or other fire extinguishing medium is sprayed out of the nozzle or the spraying device and is used for extinguishing fire, or other fire extinguishing devices are operated to perform work. Target locations for fire suppression include, but are not limited to, building interiors, building surfaces, building facades, attachments to building facades, objects outside of facades. Methods of opening the valve include, but are not limited to, the valve opening method, manual opening of the valve.

Preferably, the fire extinguishing method further comprises one or more of the following steps:

1. And separating the plug from the valve. The methods used include, but are not limited to, the plug pulling method or the plug opening method. 2. Breaking the glass. The apparatus used includes but is not limited to the glass breaking device and the method used includes but is not limited to the glass breaking method. 3. Moving one or more of the following devices with the transport system: the device comprises a spraying device, a glass breaking device, a tube holding system, a blocking device, a spraying system and a bracket system. 4. The positioning/orienting system is used for positioning or orienting the water pipe joint or the spraying device. 5. The nozzle or the spraying device is communicated with a valve on a building by adopting the aircraft connecting pipe method. 6. The blocking member or the blocking means is employed to block the ventilation caused by the window frame. 7. And searching a high-temperature area by adopting the thermal imager. 8. The water spray is cooled, and the equipment used includes but is not limited to the spraying system. 9. When the glass is broken, the blocking device is adopted to block glass fragments from falling outside the building. 10. And combining the ABA mechanism with the water hose or the water hose connector at one end of the aircraft system or the connecting system of the aircraft system, and releasing the water hose or the water hose connector after reaching a destination. 11. The fire extinguishing personnel communicate the fire extinguishing medium source with the nozzle or the spraying device in the fireproof subarea adjacent to the fire place, and then control the nozzle or the spraying device to spray the fire extinguishing medium to extinguish the fire. 12. And carrying out smoke discharging operation through the smoke discharging device. 13. The equipment or device required for fire suppression is secured to a target object B located outside the aircraft system by the securing method or aircraft securing method described below, including but not limited to a building, a building facade, a building exterior, an attachment to a building facade or exterior, an object in the air, an object on the ground. 14. And transporting by adopting the aircraft transportation method.

Preferably, the aircraft is an unmanned aircraft.

Preferably, the fire extinguishing method comprises the following steps: firstly, controlling the unmanned aerial vehicle system to fly to a position to be extinguished. 2. An ABA type mechanism is employed to bond the connection system to the support system or building attachment. 3. The bracket system is transported to the supporting system through a transport system and is combined with the supporting system through an AB combination mode. 4. The connector tube on the bracket system is connected with the valve mounted on the outer wall of the building through the pipe holding system. 5. The connection system of the unmanned aerial vehicle system is controlled to be disconnected from the bracket system. 6. And opening the valve, and spraying water to extinguish fire. Wherein steps 4,5 may be exchanged in order.

Preferably, the fire extinguishing method comprises the following steps: 1. the unmanned aerial vehicle system is controlled to fly to the position of fire extinguishing personnel, and the tail end of the connecting system of the unmanned aerial vehicle system adopts the ABA mechanism to combine with a water pipe connector. 2. The fire fighter removes the water connection from the connection system of the unmanned aerial vehicle system and communicates with a fire water source. 3. And controlling the unmanned aerial vehicle system to fly to the position to be extinguished. 4. The unmanned aerial vehicle system or fire extinguishing apparatus transported from the unmanned aerial vehicle system is integrated with a building attachment or the support system at the location to be extinguished. 5. The fire extinguishing personnel opens the valve and sprays water to extinguish fire. Preferably, one or more of the following steps are also included: 1. controlling the separation of the unmanned aerial vehicle system from the building attachment or the support system. 2. The bracket system or the spraying device is coupled to an accessory of a building by an AB-type mechanism. Preferably, the fire fighter opens a valve adjacent to the fire zone in the fire location.

Preferably, the fire extinguishing method comprises the following steps: 1. and controlling the unmanned aerial vehicle system to fly to the building attachment at the position to be extinguished. 2. An ABA type mechanism is employed to bond the connection system to the building attachment. 3. The bracket system is transported to the supporting system through a transport system and is combined with the supporting system through an AB combination mode. 4. The connection system of the unmanned aerial vehicle system is controlled to be disconnected from the bracket system. 5. And controlling the ABA type mechanism to release the folded water bands. 6. And opening the valve, and spraying water to extinguish fire. Wherein the order of steps 4, 5 is exchangeable.

Preferably, the fire extinguishing method comprises the following steps: (1) Controlling the flight of the aircraft system comprising the fire suppression device to a destination location. The destination locations include, but are not limited to, the location of the connection hose, water pipe or fitting pipe, the location of the injection device or the bracket system to be incorporated, the location of the valve, the location of fire fighters, the location of the support system, other architectural appurtenances. (2) The nozzle or the spraying device is in communication with a fire water source or other fire extinguishing medium source. The connection method includes, but is not limited to, the pipe holding system making connection, the aircraft take over method, or manual connection. The location of the source of extinguishing medium includes, but is not limited to, on-building, ground. Preferably, the source of extinguishing medium to which the spraying device is connected is on the building. (3) The fire suppression apparatus is secured to a target object B that is external to the aircraft system using the aircraft securing methods described below, including but not limited to a building, a building facade, a building exterior surface, an attachment to a building facade or exterior surface, an object in the air, an object on the ground. Preferably, the aircraft securing method includes using the AB mode to bond the aircraft system, a portion of the aircraft system, or a fire extinguishing device to the target object B or an object adjacent to the target object B that may be bonded thereto using the AB mode. In a specific operation, the steps (2) and (3) may be exchanged according to the actual situation. Preferably, the nozzle or the spraying device is bonded to the target object in an AB bond. Preferably, the stent system comprising a nozzle or the spraying device is used, and the stent system is bonded to the target object by an AB bonding method. Preferably, the connection system is used for binding the target object in an AB binding mode. Preferably, the attachment system is coupled to the target object using an ABA type mechanism. Preferably, the fire extinguishing apparatus is fixed to the target object using the aircraft fixing method. (4) And opening a valve for controlling water or other fire extinguishing medium, so that the water or other fire extinguishing medium is sprayed out of the nozzle or the spraying device and is used for extinguishing fire, or other fire extinguishing devices are operated to perform work. Target locations for fire suppression include, but are not limited to, building interiors, building surfaces, building facades, attachments to building facades, objects outside of facades. Methods of opening the valve include, but are not limited to, the valve opening method, manual opening of the valve.

By adopting the technical scheme of the invention, the fire extinguishing height can be greatly improved relative to the fire truck, and in fact, the fire extinguishing operation according to the technical scheme of the invention is not limited by the building height. Meanwhile, the fire can be sprayed in a short distance to extinguish the fire, which is beneficial to reducing air entrainment; the method is favorable for smoke discharge, can use the thermal imaging instrument to find an indoor high-temperature area, and is favorable for directly attacking a fire point. Therefore, the technical scheme of the invention can be beneficial to extinguishing fire of buildings, especially high-rise buildings. The spraying device can enter a room to extinguish fire, so that fires in all directions can be extinguished by adjusting the angle of the nozzle. This is not done by current fire engines. Glass fragments can be prevented from falling from the control when the glass is broken and detached. After fire extinguishment, the window frame of broken glass can be shielded to block air circulation, so that the re-combustion probability is reduced. Firefighters can extinguish fire to the bulkhead unit of the firing room or adjacent fire-resistant zones without directly accessing the fire scene, thus greatly reducing security risks. The spraying device can be combined with the attachment of the building outer elevation or the supporting system in an AB type combination mode, so that high-pressure large-caliber water columns can be sprayed, and the problem of backseat force generated when water is directly sprayed from an aerial vehicle at present is avoided. Compared with the aircraft spraying water directly in the air, the aircraft adopted by the invention has small carrying capacity and low manufacturing cost. Besides a fire-fighting water source, the fire-fighting water source can be used for manually receiving tap water from a higher floor adjacent to a fireproof partition to extinguish the fire, and the problem of insufficient water pressure can be avoided because water flows from a high place to a low place; meanwhile, tap water can be in normal condition, and the problems that similar fire hydrants find no water and the water pressure is low when water is needed are avoided; firefighters can use the passenger elevator of the unfired building unit without having to climb the building with heavy firefighting equipment.

By adopting the technical scheme of the invention, the air transportation objects can be transported, transferred and combined by using the aircraft, the air is connected with the water pipe, the glass is broken, the glass fragments are prevented from falling outdoors, the window frame is shielded after the glass is broken to prevent fresh air from entering, the back seat force problem when the unmanned aerial vehicle sprays water can be realized, the smoke can be rapidly and flexibly discharged, and the problem that the sprayed fire extinguishing agent dosage is too small when the unmanned aerial vehicle extinguishes the fire can be solved. By adopting the technical scheme of the invention, one part of the aircraft (such as a connecting system) can be combined or fixed on other objects, so that the object transmission in the air can be conveniently carried out, for example, objects can be transmitted to a building; the device can utilize the aircraft to carry objects and fix the objects on other objects, for example, the spraying device and the smoke discharging device can be directly fixed on the outer wall of a building for operation, so that quick response of fire extinguishment and rescue can be realized; by adopting the aircraft transportation combination method, equipment or devices can be combined on an object in the air very conveniently for operation. By adopting the method and the device for screwing the bolt, the nut, opening the valve and the like provided by the invention, related operation can be carried out by using the unmanned aerial vehicle without personnel; this may avoid personnel entering dangerous (e.g., fire, explosion) environments. The technical schemes not only can be applied to the fire-fighting field, but also can be applied to other technical fields. Such applications are also within the scope of the present invention. For example, it can be applied to aerial work, transportation of aerial objects, connection, bonding and fixing, and so on.

Drawings

In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, a brief description will be given below of the drawings required for the embodiments or the prior art descriptions, and it is obvious that the drawings in the following description are some embodiments of the present invention, and that other drawings may be obtained according to these drawings without the need for inventive effort for a person skilled in the art.

Fig. 1 is a schematic view of a smoke exhaust 46.

Fig. 2 is a schematic view of the smoke exhaust 46 at another angle.

Fig. 3 is a schematic view of the smoke evacuation device 46 shown with the baffle of the glass breaking device 72 removed.

Fig. 4 is a schematic structural diagram of a blower 460.

Fig. 5 is a schematic view of a fan 460 at another angle.

FIG. 6 shows a glass breaking device

Fig. 7 is a schematic view of the structure of the rack and other accessories of the smoke evacuation device 46.

Fig. 8 shows a schematic view of the structure of the blocking device 462.

Fig. 9 is a schematic diagram of the smoke evacuation device 47.

Fig. 10 is a schematic structural view of an aircraft system 469.

Fig. 11 is a schematic view of the support system 68 and its positional relationship in the building 25.

Fig. 12 is a schematic diagram of the combination of the fume extractor 46 and the support system 68.

Fig. 13 is a schematic view of the structure of the electric primer shooting apparatus 12.

Fig. 14 is a schematic structural view of the electric primer shooting pot 121.

Fig. 15 is a schematic sectional view of the J-J plane in fig. 13.

Fig. 16 is a schematic view of the structure of the suction cup 141 with the fixing device.

Fig. 17 is a schematic view of another angular configuration including a fixture suction cup 141.

Fig. 18 is an enlarged schematic view of the structure within the dashed box in fig. 17.

Fig. 19 is a schematic structural view of the shaped connection plate 1414.

Fig. 20 is a schematic structural view of the electric nail gun 13.

Fig. 21 is another angular structural schematic view of the electric nailing device 13.

Fig. 22 is an exploded view of the electric nail gun 13.

Fig. 23 is an enlarged schematic view of the structure within the dashed box in fig. 20.

Fig. 24 is a schematic structural view of the rotary hook 138.

Fig. 25 is a schematic structural view of the main body 132.

Fig. 26 is a schematic sectional structure of the gun head 131.

Fig. 27 is a schematic structural view of the smoke evacuation device 47.

Fig. 28 is a schematic structural view of a holder 471 of the fume extractor 47.

Fig. 29 is a schematic structural view of an aircraft system 479.

Fig. 30 is a schematic structural view of a support system 691 on building 26.

Fig. 31 is a schematic diagram of a transport system 158.

Fig. 32 is an enlarged schematic view of the structure in the left-end dashed box in fig. 31.

Fig. 33 is an enlarged schematic view of the structure in the dashed box at the right end of fig. 31.

Fig. 34 is a schematic structural view of the suction cup 1581.

Fig. 35 is a schematic structural diagram of an aircraft system 589.

Fig. 36 is a schematic structural view of the bracket system 85.

Fig. 37 is another angular schematic view of the bracket system 85.

Fig. 38 is a schematic structural view of an aircraft system 850.

Fig. 39 is a schematic structural view of the connection member 859.

Fig. 40 is a schematic diagram of a pole setting system 858.

Fig. 41 is a schematic view of the structure of the pole system 858 in combination with the bracket system 85.

Fig. 42 is a schematic structural view of the valve 66.

Fig. 43 is a schematic view of the structure of the tank 9.

Fig. 44 is a schematic structural view of the valve opening mechanism 67.

FIG. 45 is a schematic view of a positioning system, motor, and lever.

Fig. 46 is a schematic structural view of the tank.

Detailed Description

In order to enable those skilled in the art to better understand the present invention, the following description will make clear and complete descriptions of the technical solutions according to the embodiments of the present invention with reference to the accompanying drawings. It will be apparent that the described embodiments are some, but not all, embodiments of the invention. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention. It is noted that reference herein to "an embodiment" means that a particular feature, structure, or characteristic described in connection with the embodiment may be included in at least one embodiment of the invention. The appearances of such phrases in various places in the specification are not necessarily all referring to the same embodiment, nor are separate or alternative embodiments mutually exclusive of other embodiments. Those skilled in the art will explicitly and implicitly appreciate that embodiments of the invention and features in the embodiments may be combined with each other without conflict. These combinations are also within the scope of the present invention. Unless defined otherwise herein, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. The terminology used in the description of the invention herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention.

In one embodiment of the present invention, a smoke evacuation device 46 is provided, as shown in fig. 1 and 2. After the baffle of the glass breaking device 72 is removed, the internal structure of the smoke exhaust device 46 can be displayed. As shown in fig. 3.

For ease of description, the fume extractor 46 is divided into three sections: blower 460 (fig. 4, 5), glass breaking device 72 (fig. 6), brackets, and other accessories (fig. 7).

The glass breaking device 72 includes an electric push rod 721, a glass breaking device 53 fixed to the electric push rod 721, a baffle 723, and an electric push rod 727, and the angle of the baffle 723 can be adjusted by the electric push rod 727. The more detailed structure of the glass breaking device 72 is shown in fig. 37 of the patent application 2022106156183 and related description. The electric push rod 721 of the glass breaking device 72 is fixed to the bracket 461 by a clip.

Fan 460 includes motor 4600, blades 4601, housing 4602, bezel 4603, 4 support bars 4604, louvers 4605. The motor 4600 drives the blades 4601 to rotate, and the left smoke can be pumped to the right to be discharged. The left end of the shutter 4605 is fixed to the frame 4603, and the right end is fixed to the housing 4602. 4 supporting rods 4604 are fixed on the frame, and the supporting rods 4604 are fixed on the mounting plate 7213 of the glass breaking device 72. Thus, the mounting plate 7213 of the electric putter 721 is controlled to move, so that the frame 4603 is moved, and the shutter 4605 is lengthened or shortened, so that the frame 4603 can be attached to the window frame of the building; when the smoke evacuation device 46 is actuated, the air evacuation effect is enhanced.

4 Lock catches 42, a lock tongue 4611, a lock tongue 4612, a camera 4613 and a control box 4614 are fixed on the bracket 461. The control box is used for placing control equipment and batteries. The structure of the shackle and tongue is shown in figures 8 and 25 of the patent application number 2022106156183.

The spraying system 463 includes a spray head 4631, a conduit 4632, a water connection 4633. The water connection 4633 is fixed to the bracket 461, and the nozzle 4631 is fixed to the housing 4602 of the blower 460. The nozzle is opened in the housing 4602 cavity to spray water to cool the flue gas passing therethrough.

The blocking device 462 is shown in fig. 8. Comprising a motor 4620, the motor 4620 may drive a bearing 4621 to rotate, a baffle 4622 is fixed to the bearing 4621, and the other end of the bearing 4621 is supported by a mounting 4623. The motor 4620 and the mount 4623 are fixed to the bracket 461. Thus, the shutter 4622 may be controlled to rotate by the motor 4620 to control the blocking or opening of the air outlet of the blower 460. The fire extinguishing device can be used for preventing air from entering a room after fire extinguishment, and reducing the risk of re-combustion.

The blower 460 is fixed to the bracket 461.

The smoke exhaust device 46 can be combined with the supporting system through the lock catch 42, the smoke can be cooled through the spraying system 463, the glass can be broken through the glass breaking device 72, and broken glass can be prevented from falling out of the building through the baffle 723 when broken glass is broken; the baffles 723 and 4622 of the blocking device 462 may be used to block the flow of air inside and outside the building as desired.

In one embodiment of the present invention, a smoke evacuation device 47 is provided, and a spraying device 95 (see 2022106156183 for a detailed structure) is mounted on a mounting plate 7213 of a glass breaking device 72 of the smoke evacuation device 47, as compared with the smoke evacuation device 46, as shown in fig. 9. In this way, the smoke discharging device 47 can spray the fire extinguishing medium through the spraying device 95 to extinguish the fire.

In one embodiment of the present invention, a smoke evacuation device 48 is provided that differs from smoke evacuation device 46 in that: an air filter screen is arranged at the air outlet of the flue gas and is used for preventing pollutants from entering the atmosphere.

In one embodiment of the invention, an aircraft system 469 is provided, as shown in FIG. 10. The manner of assembly between the drone body 222, the transport system 57, and the carrier 461 is the same as the manner of assembly between the drone body 222, the transport system 57, and the carrier system 82 in the aircraft system 71 (see fig. 26 and related description of the patent application number 2022106156183). The power cord 4692 of the motor 4600 is terminated with a waterproof connector 4693 to facilitate quick wire connection and waterproof. The waterproof connector 4693 is clamped to the end of the transport system 57 with a clamp. The water tube 4691 is connected at one end to the water connection 4633 of the sprinkler system 463 and at the other end to the quick connect 4694 and clamps the quick connect 4694 to the end of the transport system 57.

In this way, the aircraft system 469 may transport the fume extractor 46 and may transport the fume extractor 46 via the transport system 57, which may be coupled to an object in the air, such as a support system. The smoke discharging device 46 can be combined outside the window to perform the operations of breaking glass, discharging smoke, spraying fire extinguishing medium, spraying cooling, blocking broken glass, blocking air circulation, and the like.

In one embodiment of the present invention, a building 25 is provided with a support system 68 fixedly mounted to the exterior wall below the window frame of the building 25, the support system 68 and its location in the building 25 being shown in fig. 11. The support system 68 comprises 4 poles perpendicular to the wall surface, 2 poles parallel to the wall surface, a vertical pole 6801 containing spheres. The support system 68 is sized and positioned to ensure that when the vehicle system 469 is hovering, the mechanical catch of its transport system 57 grabs the ball of the vertical rod 6801, the smoke extractor 46 is transported, the 4 catches 42 on the smoke extractor 46 are able to engage the support system 58, and the box 4603 of the smoke extractor 46 is facing the upper right hand sub-frame of the window frame (the area enclosed by the rod 2511 and the window frame) in fig. 11.

In one embodiment of the present invention, a method of exhausting smoke is provided. With the aircraft system 469, the latch 42 is opened and the firefighter E controls the aircraft system 469 to fly to the window of room a (which is the next door unit room to the fire room, where room a is safe). Meanwhile, the fire fighter D carries the water pipe and the connector, the electric wire and the waterproof connector to the room A, the quick connector 4694 is taken off from the aircraft system 469, and the quick connector 4694 is connected with the carried water pipe and the connector; and simultaneously connects the electric wire and the waterproof connector 4693. Firefighter E controls aircraft system 469 to fly out of the support system 68 of the fire room window, and firefighter D cooperates with the release water lines, wires. Firefighter E controls the grip 561 to grip the sphere of vertical rod 6801, hovers, moves smoke extractor 46 through transport system 57 until it contacts support system 68, secures the bracket 461 of smoke extractor 46 with support system 68 by 4 latches 42. Optionally, the transport system 57 of the aircraft system 469 is then controlled to disengage the fume extractor 46, the support system 68 (see patent application number 2022106156183 for a specific operation). The combination of the smoke evacuation device 46 and the support system 68 is shown in fig. 12.

At this time, the fire fighter E can control the glass breaking device 72 to break the glass, and can control the blocking device 462 to block or open the smoke outlet of the smoke discharging device 46; when the firefighter D communicates the water pipe with the tap water outlet, the spraying system 463 can be operated to spray water to cool the smoke; when the fire fighter D turns on the electric wire, the fan 460 can be controlled to exhaust air and smoke.

In one embodiment of the present invention, an electric primer nailing device 12 is provided as shown in fig. 13. Including an electric primer cartridge 121 (fig. 14) and a mating barrel 122. Fig. 15 is a schematic cross-sectional view of the electric primer nail apparatus 12 taken along the plane J-J in fig. 13.

The electric primer firing pin cartridge 121 includes a pin 1211, a cartridge case 1212, an electrode 12133, and an electrode 12134. The electrodes 12133 and 12134 are electrodes of an electric igniter. The cartridge case 1212 is filled with the propellant powder 1214, and the left end metal of the electrode 12133 and the electrode 12134 is exposed and buried in the propellant powder. Cartridge case 1212 is a clearance fit with barrel 122, electrodes 12133, 12134 are insulated from barrel 122, and motors 12133, 12134 are an interference fit with barrel 122. When the electric igniter is powered on, the ignition between the electrodes 12133, 12134 ignites the propellant powder to eject the nail 1211. The on/off of the circuit is controlled by a remote controller. Electric igniters and methods of use thereof are well known and commercially available and the construction thereof is not described in detail herein.

In one embodiment of the present invention, a suction cup 141 is provided that includes a fixture, as shown in FIGS. 16 and 17. Fig. 18 is an enlarged schematic view of the structure within the dashed box in fig. 17. Comprises a sucker main body 1411, a sponge ring 1412, an air pipe 1413, a special-shaped connecting plate 1414, an L plate 1415, an electric primer nail shooting device 12 and a motor lock 446 (the specific structure is referred to as patent application number 2022106156183 in figure 18). Fig. 19 is a schematic structural view of the shaped connection plate 1414. The sponge ring 1412 is fixed on the sucker body 1411, the air pipe 1413 is connected with the sucker body 1411 by screw threads, and the special-shaped connecting plate 1414 is fixed on the sucker body 1411. The L-plate 1415 is in a clearance fit with the shaped connection plate 1414 (fig. 16) and the long nut 4461 of the motor lock 446 secured to the shaped connection plate 1414 can be moved into and out of the hole of the L-plate 1415 to lock or unlock the L-plate 1415 to or from the shaped connection plate 1414. The electric primer nail shooting device 12 is fixed on the L plate 1415, and the projecting parts of the nails of the electric primer nail shooting device 12 are placed in the through holes of the L plate 1415 by adopting clearance fit. Thus, when the sucker 141 is used for sucking an external object, the electric primer nail shooting device 12 can be used for shooting nails into the external object for further fixing. Thereafter, the long nut 4461 of the motor lock 446 can also be controlled to exit the hole of the L-plate 1415, which can disengage the suction cup body 1411 from the stapling apparatus 12.

In one embodiment of the present invention, an electric stapling device 13 is provided, as shown in fig. 20, 21, and an exploded view is shown in fig. 22. Fig. 23 is an enlarged schematic view of the structure within the dashed box in fig. 20. Comprising the following steps: gun head 131, main body 132, firing pin 133, bolt 137, bumper 134, electromagnet 135, spring 136, rotary hook 138, connecting rod 139, and connecting rod 130. The body 132 includes a barrel 1321 thereon, and the barrel 1321 is threadably coupled to the gun head 131. The gun tube 1321 is fixed with a mounting plate 1322, the mounting plate 1322 is provided with a hole 13221, and the mounting plate 1322 is fixed with a limiting plate 1323 and a round rod 1324.

Fig. 24 is a schematic structural view of the rotary hook 138, fig. 25 is a schematic structural view of the main body 132, and fig. 26 is a schematic sectional structural view of the gun head 131. The rotating hook 138 includes a hole 1383, a hole 1382, and a stub 1381. The hole 1383 is in clearance fit with the round bar 1324 and is restrained from movement along the axis of the round bar by the nut 1325, the rotating hook 138 is rotatable about the round bar 1324, and the stop plate 1323 restrains the angle of rotation of the rotating hook 138. The bumper 134 can pass through the hole 1382 on the rotating hook 138 and the hole 13221 on the main body 132, so that the rotating hook 138 can not rotate, and the functions of preventing the buckle from rotating and protecting can be achieved.

A short rod 1381 of the rotary hook 138 passes through a hole at the tail end of the iron core 1351 of the electromagnet 135, when the electromagnet is not electrified, a spring 1352 sleeved on the iron core 1351 is in a compressed state, and the iron core 1351 is pushed to extend out, so that the rotary hook 138 in fig. 23 is pushed to rotate clockwise and abut against the limiting plate 1323; when a nail cartridge needs to be loaded, the bolt 137 is pulled rightward in fig. 23, the bolt 137 contacts the rotary hook 138 to push the rotary hook 138 to rotate counterclockwise, and after the bolt 137 passes over the hook part at the left end of the rotary hook 138, the rotary hook 138 rotates clockwise under the thrust of the spring 1352 to hook the bolt 137; at this time, the bumper 134 may be inserted into the hole 1382 of the swivel hook 138 and the hole 13221 of the main body 132; then the nail shooting bullet is put into the gun head 131; and the gun head 131 is fixed on the object G to be fixed by adopting a screw, and the part of the gun head 131 exposed by the shooting nail is inserted into a hole (including a blind hole) of the object G. When the nail is required to be shot, the object G is abutted against an external object W, the safety rod 134 is pulled out, the remote control electromagnet is used for communicating with a power supply, the iron core is retracted into the electromagnet 135, the rotary hook 138 rotates anticlockwise, the bolt 137 is released, the bolt 137 pushes the firing pin 133 to eject towards the left end under the action of the spring 136, the nail shooting bullet is impacted, and the nail is ejected, so that the object G and the object W are fixed together through the nail shooting.

The firing pin 133 is threadably coupled to the connector rod 130, the connector rod 139 is threadably coupled to the connector rod 130, and the bolt 137 is secured in the bore of the connector rod 130 with an interference fit. The cavity of the spring 136 snaps onto the connecting rod 139 and the spring 136 is in clearance fit with the cavity of the barrel 1321. The firing pin 133 is in clearance fit with the small hole in the gun head 131; the connector rod 130 is a clearance fit with the bore of the barrel 1321.

In one embodiment of the present invention, an electric nail shooting device 14 is provided, the electric nail shooting device 14 comprises an electric nail shooting device 13, and the anode and the cathode of an electromagnet of the electric nail shooting device 13 are connected with a wireless remote control switch and a battery, so that the electric nail shooting device 14 can be controlled by a remote controller. The remote controller is used for controlling the on-off of the electromagnet, which belongs to the known technology and is not described in detail herein.

In one embodiment of the present invention, a smoke evacuation device 47 is provided, as shown in fig. 27. The holder 471 of the fume extractor 47 is shown in fig. 28. The fume extractor 47 has no lock catch 42, the support 471 has more rods 4711, 4712, 4713 and mounting plates 4714, 4715 than the support 461 of the fume extractor 46, the mounting plates 4714, 4715 have holes, 7 electric primer shooting devices 12 are fixed on the mounting plates 4714, 4715 (the structure is shown in fig. 13), and the protruding shooting nail bodies of the electric primer shooting devices 12 are inserted into the holes of the mounting plates 4714, 4715 by adopting clearance fit. The other structure of the smoke evacuation device 47 is the same as that of the smoke evacuation device 46. When the smoke discharging device 47 is pressed against an object such as a wall surface by an external force, the smoke discharging device 47 can be fixed to the object such as the wall surface by the electric primer nail shooting device 12. The embodiment is also an embodiment of a bracket system, a blocking device and a glass breaking device.

In one embodiment of the present invention, a building 26 is provided. The building 26 differs from the building 25 in that the support system is different and the others are identical. The support system 691 mounted on the building 26 includes spheres and support rods as shown in fig. 29.

In one embodiment of the present invention, an aircraft system 479 is provided, as shown in FIG. 30. The differences between the aircraft system 479 and the aircraft system 469 are: the fume extractor 46 is replaced by a fume extractor 47. The other structures are the same.

The embodiment also provides an aircraft fixing method, which comprises the following steps: with the aircraft system 479, the aircraft 479 is controlled to fly toward the support system 691 of the building 26, after the mechanical gripper of the transport system 57 is used to grip the sphere of the support system 691 of the building 26, hover, transport the fume extractor 47 by the transport system and against the wall of the building 26, then the nail shooting device 12 of the fume extractor 47 is controlled to shoot out the nail, and the fume extractor 47 is fixed on the building 26 by the nail shooting. The operation of the transport system 57 is described in connection with patent application number 2022106156183.

In one embodiment of the present invention, a transport system 158 is provided. As shown in fig. 31. An enlarged view of the left end of the dashed box in fig. 31 is shown in fig. 32, and an enlarged view of the right end of the dashed box is shown in fig. 33. The fixed pulley 5713, the base 5711, the transport member 93, the linear bearing slider 572, the winding mechanism 573, the spring 574, the retainer 575, and the wire ropes 576, 577 in fig. 31 to 33. The structure and assembly relationship of the round tube 3101, the T-bar 3102, the slide bar 31, the L-plate 5633, the retainer 575, the wire rope 576, and the wire rope 577 are the same as those of the corresponding components of the transport system 57 (see fig. 28 and related description of patent application number 2022106156183).

Suction cup 1581 (fig. 34) includes suction cup body 15811, sponge ring 15812, air tube 15813. The suction cup 1581 is coupled with the circular tube 3101 through threads, the long air tube 1582 penetrates through the circular tube 3101, an air tube 15813 with one end connected with the suction cup 1581, and the other end is coupled to an air inlet tube of the vacuum pump 1583. A vacuum pump 1583 is secured to the L plate 5633. Thus, when the suction cup 1581 is abutted against an object such as glass, a wall surface and the like, the suction cup 1581 can be adsorbed on the object such as glass, the wall surface and the like by the vacuum pump 1583, and after the suction is stopped, the suction cup 1581 can be separated from the object such as glass, the wall surface and the like.

In one embodiment of the present invention, an aircraft system 589 is provided, as shown in FIG. 35. The differences between aircraft system 589 and aircraft system 479 are: transport system 158 is used in place of transport system 57. The other structures are the same. With the aircraft system 589, the fume extractor 47 is transported to the wall after the suction cups 1581 of the transport system 158 are used to suck the wall, and then the fume extractor 47 is fixed to the wall.

In one embodiment of the present invention, an aircraft system 5899 is provided that employs a suction cup 141 (FIG. 16) containing a fixture in place of suction cup 1581 in aircraft system 589, otherwise configured identically to aircraft system 589. The smoke evacuation device 47 can be secured to the wall surface using the aircraft system 5899 as follows: the aircraft system 5899 is controlled to fly, the sucker with the fixing device sucker 141 is controlled to be attached to a wall surface and adsorbed on the wall surface, the electric primer nail shooting device 12 with the fixing device sucker 141 is controlled to shoot nails into an external object for reinforcement, then the transportation system can be controlled to transport the smoke discharging device 47 and lean against the wall surface, and then the electric primer nail shooting device 12 on the smoke discharging device 47 is controlled to shoot nails into the wall surface, so that the smoke discharging device 47 is fixed on the wall surface. The technical proposal has the advantages that: the external objects such as the wall body and the like do not need to be provided with a supporting object (such as a supporting system) in advance, and the external objects can be directly adsorbed by adopting the sucking disc and further fixed by a remote control fixing device such as a remote control nail shooting device and the like. When disengagement is desired, the long nut 4461 of the motor lock 446 in fig. 18 can be controlled to move downward and disengage from the L plate 1415, the vacuum pump can be controlled to stop, and the aircraft system 5899 can be controlled to fly to the right and then leave the wall.

In one embodiment of the present invention, a stent system 85 is provided, as shown in FIGS. 36, 37. 4 catches 42, a lock tongue 8508, a lock tongue 8509, 4 cameras, a spraying device 95, a control box 858 and a sliding table 852 are arranged below the bracket body 851. The base plate of the slide 444 of the holding tube system 44 (refer to fig. 18 and related description of patent application number 2022106156183) is fixed to the slide of the slide 852. The axes of the screw rods of the slide table 444 and the slide table 852 are mutually perpendicular. When needed, a hose is used to connect the spraying device 95 to the holding pipe system 44 so that water can flow from the holding pipe system 44 into the spraying device 95 and be sprayed out.

In one embodiment of the present invention, an aircraft system 850 is provided, as shown in FIG. 38. Including the drone body 222, the cradle system 85, and the connection members 859. The structure of the connection member 859 is shown in fig. 39. The structure in the left and right dashed boxes in fig. 39 is the same as the structure of the corresponding position of the transport member 93 (refer to fig. 27 of patent application number 2022106156183) for fitting with the bolts 8508, 8509 of the bracket system 85; the structure within the middle dashed box of fig. 39 is for securing to the bottom of the drone body 222. A water hose 853 is connected between the spraying device 95 and the hose system 44.

In one embodiment of the present invention, a pole setting system 858 is provided, as shown in FIG. 40. Valve 8543 communicates with tube 8581. The valve 8543 differs from the union 43 (see figures and description of patent application number 2022106156183) in that: the junction tube 43 contains a T-shaped support bar 4351, while the valve 8543 has no similar structure. The valve 8543 is the same as the other structure of the joint pipe 43. The 4 rods 8583, 8584, 8585, 8586 form a box, and the rods 8583, 8584 are sized the same as the ribs 8513, 8514, respectively, of the bracket system 85.

In one embodiment of the present invention, a transport combination is provided. With the aircraft system 850, the aircraft system 850 is controlled to fly toward the pole system 858, the bottom surface of the cradle system 85 is aligned with and brought into contact with the square frame of the rods 8583, 8584, 8585, 8586, the rods 8583, 8584, 8585, 8586 are locked into the 4 catches of the cradle system 85, and then the connecting members 859 are controlled to disengage from the catches 8508, 8509 of the cradle system 85, and the unmanned aerial vehicle body 222 is controlled to fly away. The control of the motor lock and the lock catch can be referred to in patent application number 2022106156183. In this way, the bracket system 85 is integrated with the pole system 858. A schematic of the structure of the pole system 858 in combination with the bracket system 85 is shown in fig. 41. The water pipe connector can be connected with the valve 8543 through the remote control operation pipe holding system 44, and then the water spraying fire extinguishing operation can be performed.

In one embodiment of the present invention, a fume extractor 48 is provided, fume extractor 48 comprising fume extractor 47, and a film pressure sensor affixed to the outer surface of mounting plates 4714, 4715 for detecting the pressure of fume extractor 48 against a wall or the like.

In one embodiment of the present invention, a valve 66 is provided, as shown in FIG. 42. The valve 66 includes a support that can be used to support external objects. The valve 66 includes a circular handle that can be turned to open or close the valve.

In one embodiment of the invention, a canister 9 is provided, as shown in fig. 43. The tank 9 contains a support system which can be used to provide support for the connection system of the aircraft, as well as for the bracket system or the spraying device according to the invention.

In one embodiment of the present invention, a bracket system, or a valve opening mechanism 67, is provided, as shown in FIG. 44. Comprises a bracket body 400, on which a lock catch 42 and a positioning system 401 are fixed. The dimensions were such that the 4 catches 42 could just engage with the 3 ribs on the upper surface of the bracket of the valve 66 of fig. 42, while allowing the two brackets to fit together. The positioning system comprises two crisscross sliding tables and a lifting table, a motor 402 is fixed on the lifting table, and a deflector rod 403 is fixed on an output shaft of the motor, as shown in fig. 45. Thus, when the valve 66 and the valve opening mechanism 67 are combined together through the lock catch 42, the axis of the output shaft of the motor is overlapped with the central axis of the circular handle of the valve through the control positioning system 401, the deflector rod 403 is inserted into the circular handle of the valve 66, and the motor 402 is controlled to drive the circular handle to rotate, so that the valve 66 can be controlled to be opened and closed.

In one embodiment of the present invention, a tank is provided, as shown in FIG. 46. The tank comprises a tank body, a valve is arranged on a pipeline on the tank body, and a supporting system is arranged near the valve. The support system is sized to match the support of the valve opening mechanism 67 shown in fig. 44 so that the two can be brought together by the catch 42 when the valve opening mechanism is transferred to the support system by the unmanned aerial vehicle system. In this way, the unmanned aerial vehicle system can be equipped with the valve opening mechanism to perform the valve opening and closing operations.

It will be apparent to those skilled in the art that the foregoing embodiments are merely some of the embodiments of the invention for convenience and brevity of description. The above embodiments are only for illustrating the technical solution of the present invention, and are not limiting. The technical scheme of the invention also comprises any combination of the embodiment modes.

Although the invention has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical scheme described in the foregoing embodiments can be modified, or the described technical schemes can be combined, or some technical features in the technical scheme can be replaced equivalently; such modifications and substitutions do not depart from the spirit and scope of the technical solutions of the embodiments of the present invention, and therefore, they are still within the scope of the present invention.

Claims (10)

1. The sucker is characterized by comprising a sucker main body and an air pipe, wherein the air pipe is used for exhausting air; the sucker comprises or is connected with a remote control fixing device, and the remote control fixing device adopts a remote control mode and can fix one object to another object.

2. The suction cup as set forth in claim 1 wherein said suction cup is connected to said remote control fixture using an ABA mechanism.

3. The suction cup as set forth in claim 1 wherein said remote control fixture of said suction cup is a remote control nailer.

4. An aircraft system, characterized in that it comprises a suction cup according to any one of claims 1-3.

5. The aircraft system according to claim 4, characterized in that it comprises a connection system, the end of which contains a suction cup according to any one of claims 1-3.

6. The aircraft system according to claim 4, characterized in that it comprises a transport system containing a suction cup according to any one of claims 1-3.

7. An aircraft system according to claim 4, characterized in that it comprises a transport system on which the device to be transported is carried, which contains a suction cup according to any one of claims 1-3.

8. The aircraft system according to claim 7, wherein the means of the aircraft system comprises one or more of the following means or devices: fire extinguishing device, fire control device, injection device, broken glass device, blocking device, bracket system and fume extractor.

9. The aircraft system according to any one of claims 4-8, characterized in that the aircraft system comprises an AB-type mechanism or an ABA-type mechanism.

10. Use of a suction cup according to any of claims 1-3 and an aircraft system according to any of claims 4-9 in aerial work, in the transportation, connection, joining and fixing of aerial objects, and in the field of fire protection.