CN111959752A - Unmanned aerial vehicle for fire scene exploration - Google Patents
Unmanned aerial vehicle for fire scene exploration Download PDFInfo
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- CN111959752A CN111959752A CN202010891561.0A CN202010891561A CN111959752A CN 111959752 A CN111959752 A CN 111959752A CN 202010891561 A CN202010891561 A CN 202010891561A CN 111959752 A CN111959752 A CN 111959752A
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- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 29
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62B—DEVICES, APPARATUS OR METHODS FOR LIFE-SAVING
- A62B3/00—Devices or single parts for facilitating escape from buildings or the like, e.g. protection shields, protection screens; Portable devices for preventing smoke penetrating into distinct parts of buildings
- A62B3/005—Rescue tools with forcing action
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B08—CLEANING
- B08B—CLEANING IN GENERAL; PREVENTION OF FOULING IN GENERAL
- B08B1/00—Cleaning by methods involving the use of tools
- B08B1/10—Cleaning by methods involving the use of tools characterised by the type of cleaning tool
- B08B1/14—Wipes; Absorbent members, e.g. swabs or sponges
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B08—CLEANING
- B08B—CLEANING IN GENERAL; PREVENTION OF FOULING IN GENERAL
- B08B1/00—Cleaning by methods involving the use of tools
- B08B1/30—Cleaning by methods involving the use of tools by movement of cleaning members over a surface
- B08B1/32—Cleaning by methods involving the use of tools by movement of cleaning members over a surface using rotary cleaning members
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B64C—AEROPLANES; HELICOPTERS
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- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/16—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting
- B64D1/18—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting by spraying, e.g. insecticides
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/02—Arrangements or adaptations of signal or lighting devices
- B64D47/06—Arrangements or adaptations of signal or lighting devices for indicating aircraft presence
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B64C2025/325—Alighting gear characterised by elements which contact the ground or similar surface specially adapted for helicopters
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
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- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Life Sciences & Earth Sciences (AREA)
- Pest Control & Pesticides (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The invention discloses an unmanned aerial vehicle for fire scene exploration, and relates to the technical field of unmanned aerial vehicles for exploration; in order to reduce the influence of smoke on a fire scene on a exploration camera in the exploration process; the fixed base comprises a fixed base, fixing base bottom outer wall has the fore-set through the bolt fastening, fore-set bottom outer wall rotates through the bearing and is connected with anti-shake cloud platform subassembly, anti-shake cloud platform subassembly one side outer wall rotates through the bearing and is connected with the exploration camera, fixing base bottom outer wall has transparent cylindricality shell through the bolt fastening, transparent cylindricality shell one side outer wall has the mounting bracket through the bolt fastening, mounting bracket one side outer wall has driving motor through the bolt fastening, transparent cylindricality shell both sides outer wall all rotates through the pivot and is connected with the swing arm. According to the invention, the anti-shake cradle head assembly is arranged, so that the angle of the exploration camera in the horizontal direction can be adjusted by the remote operation terminal, and the exploration range of the exploration camera in the horizontal direction can be enlarged.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles for exploration, in particular to an unmanned aerial vehicle for fire scene exploration.
Background
At present unmanned aerial vehicle uses very generally at the scene of a fire, but these unmanned aerial vehicles can only be used for surveying, instruct, though there is the unmanned aerial vehicle of putting out a fire, but it is comparatively single in its function, can only carry out some simple work, and because the scene of a fire condition is comparatively complicated, the temperature is higher, make unmanned aerial vehicle very easily bump, cause the damage, and the scene of a fire temperature is higher, can't protect unmanned aerial vehicle effectively, consequently need design an unmanned aerial vehicle for the scene of a fire exploration, can realize the exploration at the in-process of protecting itself.
Through the retrieval, chinese patent application number is CN201720647233. X's patent discloses a survey unmanned aerial vehicle for scene of fire, including an unmanned aerial vehicle that has independently cruising ability, this unmanned aerial vehicle carries on the life detection instrument and is used for the scene to shoot the camera that has, still including setting up the speaker that is used for shouting usefulness in camera one side, unmanned aerial vehicle's bottom is provided with two fixed bolsters, all is provided with a lifting rope on the fixed bolster, and a pivot is connected to the bottom of lifting rope, and one of the externally mounted of pivot puts the rolling element of thing usefulness, is provided with wet towel in the rolling element, and unmanned aerial vehicle drives the rolling element and rolls on the ground and advance.
One of the above-mentioned patents of surveying unmanned aerial vehicle for fire scene has the following disadvantages: the camera is at the in-process of carrying out the exploration, and the smog at the scene of fire very easily causes the hindrance to the shooting sight of camera to cause very big influence to the exploration effect of camera.
Disclosure of Invention
The invention aims to solve the defect that smoke in a fire scene easily obstructs the shooting sight of a camera in the process of exploring the camera in the prior art, so that the exploration effect of the camera is greatly influenced, and provides an unmanned aerial vehicle for exploring the fire scene.
In order to achieve the purpose, the invention adopts the following technical scheme:
the utility model provides an unmanned aerial vehicle is used in scene of fire exploration, includes the fixing base, fixing base bottom outer wall has the fore-set through the bolt fastening, fore-set bottom outer wall rotates through the bearing and is connected with anti-shake cloud platform subassembly, anti-shake cloud platform subassembly one side outer wall rotates through the bearing and is connected with the exploration camera, fixing base bottom outer wall has transparent cylindricality shell through the bolt fastening, transparent cylindricality shell one side outer wall has the mounting bracket through the bolt fastening, mounting bracket one side outer wall has driving motor through the bolt fastening, transparent cylindricality shell both sides outer wall all rotates through the pivot and is connected with the swing arm, just the driving motor output passes through coupling joint in one of them swing arm pivot input, two swing arm one side inner wall rotates and is connected with same adhesion roller.
As a further scheme of the invention: the fixing base outer wall is fixed with four supporting seats through the bolt, four supporting seat one side outer wall all rotates through the pivot and is connected with the telescopic link, and four telescopic link one side outer walls respectively through buckle joint in four supporting seat one side outer wall, four the flexible end circumference outer wall of telescopic link all is provided with the second elastic pin, and second elastic pin circumference outer wall joint in support circumference outer wall.
Further: four the telescopic end of telescopic link all welds and has an installation section of thick bamboo, four installation section of thick bamboo circumference inner wall all welds has two column plates, and two column plates one side inner walls that are located same installation section of thick bamboo have same double-shaft motor through the bolt fastening.
As a further scheme of the invention: four the biax motor output all is fixed with the rotating turret through the bolt, eight the outer wall of rotating turret both sides all rotates and is connected with two paddles, four installation section of thick bamboo circumference outer wall all is provided with two above louvres.
Further: the fixing base top inner wall has the battery through the bolt fastening, fixing base one side inner wall welding has the heat dissipation copper sheet, fixing base top inner wall is provided with the control unit, fixing base outer wall sliding connection has the protection apron, and the protection apron passes through the bolt fastening in fixing base top outer wall.
As a further scheme of the invention: and the outer wall of the bottom of the fixed seat is respectively fixed with a temperature sensor and a laser radar probe through bolts.
As a further scheme of the invention: the fixing base both sides outer wall all is fixed with the warning light through the bolt, fixing base bottom outer wall has the support through the bolt fastening, support circumference outer wall sliding connection has two above couples.
On the basis of the scheme: the outer wall of the bottom of the fixing seat is fixedly provided with four lifting columns and four circumferential outer walls of the lifting columns are fixedly provided with containing frames and four containing frames through bolts, the outer walls of two sides of the lifting columns are rotatably connected with an L-shaped frame and four rotating shafts, the inner wall of the L-shaped frame is rotatably connected with a damping assembly and four damping assemblies, and one ends, away from the L-shaped frame, of the damping assemblies are rotatably connected with four inner walls and four connecting rods respectively, the outer wall of the bottom of the L-shaped frame is welded with two connecting rods, the two connecting rods are located at the same side, the circumferential inner wall of each connecting rod is slidably connected with the same supporting rod and the circumferential outer wall.
As a further scheme of the invention: the fixing base bottom outer wall has the dead lever through the bolt fastening, dead lever circumference inner wall sliding connection has the regulation post, it is provided with the first elastic pin more than two to adjust post circumference outer wall, it has the spring more than two to adjust post one side outer wall welding, more than two the spring is kept away from the one end welding of adjusting the post and is had same impact head, impact head one side outer wall welding has spacing post, and spacing post circumference outer wall sliding connection in regulation post one side outer wall.
As a further scheme of the invention: fixing base bottom outer wall has water tank and roof through the bolt fastening, roof top outer wall has the force (forcing) pump through the bolt fastening, the force (forcing) pump output all has the steel water pipe, one of them steel water pipe one end is passed through flange joint in water tank one side outer wall, the other steel water pipe one end welding has the water storage dish, the welding of water storage dish circumference outer wall has the spraying dish more than two.
The invention has the beneficial effects that:
1. the remote operation terminal can be improved by arranging the anti-shake pan-tilt assembly to adjust the angle of the exploration camera in the horizontal direction, so that the exploration range of the exploration camera in the horizontal direction can be improved, meanwhile, the exploration camera is rotatably connected to the inner wall of one side of the anti-shake pan-tilt assembly, so that the exploration range of the exploration camera in the vertical direction can be adjusted, the exploration range and the exploration efficiency can be enlarged, the exploration camera can be protected by arranging the transparent cylindrical shell, meanwhile, the transparent cylindrical shell is of a transparent structure, so that the exploration of the exploration camera cannot be influenced, substances such as dust and the like contained in smoke can be attached to the outer surface of the transparent cylindrical shell, the driving motor can drive the swing arm to do circular motion, the adhesion roller can be used for adhering and wiping the substances such as dust and the like on the outer surface of the transparent cylindrical shell, and therefore, the exploration of the exploration camera cannot be influenced, meanwhile, the transparent cylindrical shell is of a cylindrical structure, so that the circumferential outer wall of the adhesion roller can be better attached to the outer wall of the transparent cylindrical shell, and the wiping efficiency can be improved.
2. Connect in supporting seat one side outer wall through rotating the telescopic link and can fold the telescopic link and accomodate, reduce the occupation space of telescopic link, simultaneously can control the elongation of telescopic link through the second elastic pin, thereby can reduce whole unmanned aerial vehicle's occupation space according to the on-the-spot particular case of conflagration, so that unmanned aerial vehicle can move to relatively narrow and small corner and carry out the exploration, utilize the biax motor to drive four paddles simultaneously, can not lead to the fact to show the influence to unmanned aerial vehicle holistic flight when one of them or a plurality of paddle take place to damage, thereby unmanned aerial vehicle's safety has been guaranteed, unmanned aerial vehicle's bearing capacity has been improved, utilize the louvre can spread the heat that the biax motor produced at the operation in-process.
3. The outer wall of the circumference of the bracket is connected with more than two hooks in a sliding way; can improve the speed of stranded personnel to unmanned aerial vehicle discernment at the scene of fire through being provided with the warning light, utilize the warning light can be used for hanging gas mask, rescue equipment such as wet towel, can improve the ability that stranded personnel saved oneself, thereby improve stranded personnel's survival probability, can play the effect of supporting the fixing base through being provided with four posts of falling, utilize two bracing pieces to bear the weight of the unmanned aerial vehicle main part simultaneously, be convenient for unmanned aerial vehicle rise and fall, can improve and the horizontal plane between frictional force through being provided with the non slipping spur, utilize shock attenuation subassembly can effectually alleviate the whole impact force that receives of unmanned aerial vehicle when descending, because unmanned aerial vehicle holistic weight is heavier, can effectually protect unmanned aerial vehicle.
4. Can adjust the length of adjusting column between for the dead lever through being provided with first elastic pin, thereby can adjust the elongation of impact head, need face the phenomenon of broken window usually at the scene of fire, the utilization is strikeed the head and can be strikeed the glass surface, set up impact head into the effect that the toper structure can improve the impact force, utilize the spring to cause the damage to unmanned aerial vehicle by the reaction force when can reducing the impact simultaneously, utilize spacing post can effectually lead to impact the head and strike the route, avoid the impact process to take place to skid.
5. Can utilize the force (forcing) pump to follow the spraying dish blowout with rivers with atomizing mode through being provided with the water tank, can form one cascade all around unmanned aerial vehicle, thereby can be to whole unmanned aerial vehicle when cooling down, avoid the high temperature to cause the unmanned aerial vehicle surface to burn, utilize the spraying to carry out moist to adhesion roller circumference outer wall simultaneously, thereby can improve the adhesion roller to the absorptive efficiency of dust, improve the efficiency of exploration when carrying out the protection to unmanned aerial vehicle.
Drawings
Fig. 1 is a schematic overall structure diagram of an unmanned aerial vehicle for fire scene exploration according to the present invention;
fig. 2 is a schematic view of a main view structure of an unmanned aerial vehicle for fire site exploration according to the present invention;
fig. 3 is a schematic diagram of an explosion structure of an unmanned aerial vehicle for fire scene exploration according to the present invention;
fig. 4 is a schematic structural view of a cross section of a protection mechanism of a prospecting component of an unmanned aerial vehicle for fire scene prospecting according to the invention;
fig. 5 is a schematic structural view of a collision assembly of an unmanned aerial vehicle for fire site exploration according to the present invention;
fig. 6 is a schematic structural view of a landing gear damping assembly of an unmanned aerial vehicle for fire site exploration, which is provided by the invention;
fig. 7 is a schematic top view of a blade assembly of an unmanned aerial vehicle for fire site exploration according to the present invention;
fig. 8 is a schematic side view of a blade assembly of an unmanned aerial vehicle for fire site exploration according to the present invention;
fig. 9 is a schematic side view of an unmanned aerial vehicle for fire site exploration according to the present invention;
fig. 10 is a schematic flow chart of a control circuit of the unmanned aerial vehicle for fire scene exploration according to the present invention.
In the figure: 1-a fixed seat, 2-a telescopic rod, 3-a bracket, 4-a protective cover plate, 5-a temperature sensor, 6-a laser radar probe, 7-an adjusting column, 8-a transparent cylindrical shell, 9-a supporting rod, 10-an antiskid column, 11-a hook, 12-a connecting rod, 13-a control unit, 14-a warning lamp, 15-a battery, 16-a radiating copper sheet, 17-an anti-shaking pan-tilt assembly, 18-an adhesive roller, 19-a swing arm, 20-a driving motor, 21-an installation rack, 22-a exploration camera, 23-a top column, 24-a fixed rod, 25-a spring, 26-an impact head, 27-a limiting column, 28-a first elastic pin, 29-L-shaped rack, 30-a containing rack, 31-a lifting and falling column, 32-damping component, 33-double-shaft motor, 34-mounting cylinder, 35-cylindrical plate, 36-rotating frame, 37-supporting seat, 38-second elastic pin, 39-heat dissipation hole, 40-paddle, 41-pressure pump, 42-water tank, 43-spray disk, 44-water storage disk, 45-steel water pipe and 46-top plate.
Detailed Description
The technical solution of the present patent will be described in further detail with reference to the following embodiments.
Reference will now be made in detail to embodiments of the present patent, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are exemplary only for the purpose of explaining the present patent and are not to be construed as limiting the present patent.
In the description of this patent, it is to be understood that the terms "center," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like are used in the orientations and positional relationships indicated in the drawings for the convenience of describing the patent and for the simplicity of description, and are not intended to indicate or imply that the referenced devices or elements must have a particular orientation, be constructed and operated in a particular orientation, and are not to be considered limiting of the patent.
In the description of this patent, it is noted that unless otherwise specifically stated or limited, the terms "mounted," "connected," and "disposed" are to be construed broadly and can include, for example, fixedly connected, disposed, detachably connected, disposed, or integrally connected and disposed. The specific meaning of the above terms in this patent may be understood by those of ordinary skill in the art as appropriate.
Example 1:
an unmanned aerial vehicle for fire scene exploration, as shown in figure 1, comprises a fixed seat 1, a top column 23 is fixed on the outer wall of the bottom of the fixed seat 1 through a bolt, the outer wall of the bottom of the top column 23 is rotationally connected with an anti-shake pan-tilt assembly 17 through a bearing, the outer wall of one side of the anti-shake pan-tilt assembly 17 is rotationally connected with an exploration camera 22 through a bearing, the outer wall of the bottom of the fixed seat 1 is fixed with a transparent cylindrical shell 8 through a bolt, the outer wall of one side of the transparent cylindrical shell 8 is fixed with a mounting rack 21 through a bolt, a driving motor 20 is fixed on the outer wall of one side of the mounting rack 21 through bolts, the outer walls of the two sides of the transparent cylindrical shell 8 are both rotationally connected with a swing arm 19 through a rotating shaft, the output end of the driving motor 20 is connected to the input end of the rotating shaft of one of the swing arms 19 through a coupler, and the inner wall of one side of each of the two swing arms 19 is rotatably connected with the same adhesive roller 18; the remote operation terminal can be improved by arranging the anti-shake pan-tilt assembly 17 to adjust the angle of the exploration camera 22 in the horizontal direction, so that the exploration range of the exploration camera 22 in the horizontal direction can be improved, meanwhile, the exploration camera 22 is rotatably connected to the inner wall of one side of the anti-shake pan-tilt assembly 17, so that the exploration range of the exploration camera 22 in the vertical direction can be adjusted, thereby expanding the exploration range and efficiency, as a large amount of smoke is generated in the process of exploring a fire scene by the unmanned aerial vehicle, the exploration range and the definition of the exploration camera 22 can be greatly influenced, the exploration camera 22 can be protected by arranging the transparent cylindrical shell 8, meanwhile, as the transparent cylindrical shell 8 is of a transparent structure, the exploration of the exploration camera 22 cannot be influenced, substances such as dust and the like contained in the smoke can be attached to the outer surface of the transparent cylindrical shell 8, utilize driving motor 20 can drive swing arm 19 and be circular motion, can utilize adhesion roller 18 to carry out the adhesion and clean to substances such as the dust of transparent cylindric shell 8's surface to can guarantee that exploration camera 22's exploration can not receive the influence, simultaneously because transparent cylindric shell 8 is the cylindricality structure, consequently can make the better laminating of adhesion roller 18 circumference outer wall and transparent cylindric shell 8 outer wall, thereby can improve the efficiency of cleaning.
In order to make the drone flyable; as shown in fig. 1, 7 and 8, the outer wall of the fixing seat 1 is fixed with four supporting seats 37 through bolts, the outer wall of one side of each of the four supporting seats 37 is rotatably connected with a telescopic rod 2 through a rotating shaft, the outer wall of one side of each of the four telescopic rods 2 is respectively connected with the outer wall of one side of each of the four supporting seats 37 through a buckle, the circumferential outer wall of the telescopic end of each of the four telescopic rods 2 is provided with a second elastic pin 38, the circumferential outer wall of the telescopic end of each of the four telescopic rods 38 is connected with the circumferential outer wall of the support 3 in a clamping manner, the telescopic end of each of the four telescopic rods 2 is welded with a mounting cylinder 34, the circumferential inner wall of each of the four mounting cylinders 34 is welded with two cylindrical plates 35, the inner wall of one side of each of the two cylindrical plates 35 in the same mounting cylinder 34 is fixed with the same double-, the peripheral outer walls of the four mounting cylinders 34 are provided with more than two heat dissipation holes 39; the telescopic rod 2 can be folded and stored by rotating the telescopic rod 2 and connecting the telescopic rod to the outer wall of one side of the supporting seat 37, the occupied space of the telescopic rod 2 is reduced, meanwhile, the elongation of the telescopic rod 2 can be controlled by the second elastic pin 38, so that the occupied space of the whole unmanned aerial vehicle can be reduced according to the specific situation of a fire scene, so that the unmanned aerial vehicle can move to a relatively narrow corner for exploration, the four blades 40 can be driven simultaneously by utilizing the double-shaft motor 33, damage to one or more of the blades 40 may not significantly affect the overall flight of the drone, thereby guaranteed unmanned aerial vehicle's safety, improved unmanned aerial vehicle's bearing capacity, paddle 40 can fold simultaneously, has further reduced unmanned aerial vehicle's occupation space, utilizes louvre 39 can spread the heat that biax motor 33 produced at the operation in-process.
To drive the drone; as shown in fig. 3, a battery 15 is fixed on the inner wall of the top of the fixed seat 1 through a bolt, a heat dissipation copper sheet 16 is welded on the inner wall of one side of the fixed seat 1, a control unit 13 is arranged on the inner wall of the top of the fixed seat 1, a protective cover plate 4 is connected to the outer wall of the fixed seat 1 in a sliding manner, and the protective cover plate 4 is fixed on the outer wall of the top of the fixed seat 1 through; can supply power for unmanned aerial vehicle through being provided with battery 15, utilize the control unit 13 can control unmanned aerial vehicle's each electronic components when receiving the instruction that remote control terminal sent, utilize heat dissipation copper sheet 16 can improve the thermal diffusion rate that battery 15 produced, simultaneously protective cover plate 4 has waterproof, dustproof and dampproofing effect, can effectually protect unmanned aerial vehicle's the control unit.
In order to ensure the safety of the unmanned aerial vehicle; as shown in fig. 1, a temperature sensor 5 and a laser radar probe 6 are respectively fixed on the outer wall of the bottom of the fixed seat 1 through bolts; can monitor the temperature at the scene of the conflagration through being provided with temperature sensor 5, when the high temperature, can feed back relevant data to remote operation terminal through temperature sensor 5 to the interruption is to the exploration at the scene of the conflagration, avoids causing the damage to unmanned aerial vehicle, the temperature sensor model is BM100, can carry out long distance laser ranging through being provided with laser radar probe 6, can effectually discern the barrier, avoids unmanned aerial vehicle to cause the collision because the scene of the conflagration is complicated environment, utilizes laser radar probe 6 to need not with the help of external light source simultaneously, can avoid the barrier at the scene of the conflagration under dim regulation, has improved unmanned aerial vehicle's security.
The self-rescue materials are convenient to convey; as shown in fig. 1 and 3, warning lights 14 are fixed on the outer walls of two sides of the fixed seat 1 through bolts, a support 3 is fixed on the outer wall of the bottom of the fixed seat 1 through bolts, and more than two hooks 11 are connected to the outer wall of the circumference of the support 3 in a sliding manner; can improve the speed that stranded personnel discerned unmanned aerial vehicle at the scene of fire through being provided with warning light 14, utilize warning light 14 can be used for hanging rescue equipment such as gas mask, wet towel, can improve the ability that stranded personnel saved oneself to improve stranded personnel's survival probability.
In order to improve the damping performance of the unmanned aerial vehicle; as shown in fig. 1, 2 and 6, four rising and falling columns 31 are fixed on the outer wall of the bottom of the fixed seat 1 through bolts, accommodating frames 30 are fixed on the circumferential outer walls of the four rising and falling columns 31 through bolts, the outer walls of the two sides of the four rising and falling columns 31 are rotatably connected with L-shaped frames 29 through rotating shafts, the inner walls of the four L-shaped frames 29 are rotatably connected with damping assemblies 32, one ends, far away from the L-shaped frames 29, of the four damping assemblies 32 are rotatably connected with the inner walls of the four accommodating frames 30 respectively, connecting rods 12 are welded on the outer walls of the bottoms of the four L-shaped frames 29, the circumferential inner walls of the two connecting rods 12 on the same side are slidably connected with the same supporting rod 9, and the circumferential outer walls of the two supporting rods 9; can play the effect of supporting fixing base 1 through being provided with four post 31 that fall, utilize two bracing pieces 9 to be used for bearing the unmanned aerial vehicle main part simultaneously, unmanned aerial vehicle's of being convenient for rise and fall, can improve and the horizontal plane between frictional force through being provided with non slipping spur 10, utilize damper 32 can effectually alleviate the whole impact force that receives of unmanned aerial vehicle when descending, because the holistic weight of unmanned aerial vehicle is heavier, can effectually protect unmanned aerial vehicle.
In order to break the window in the fire scene; as shown in fig. 1 and 5, a fixing rod 24 is fixed on the outer wall of the bottom of the fixing seat 1 through a bolt, the inner wall of the circumference of the fixing rod 24 is connected with an adjusting column 7 in a sliding manner, the outer wall of the circumference of the adjusting column 7 is provided with more than two first elastic pins 28, the outer wall of one side of the adjusting column 7 is welded with more than two springs 25, one end of each of the more than two springs 25, which is far away from the adjusting column 7, is welded with the same impact head 26, the outer wall of one side of the impact head 26 is welded with a limit column 27, and the outer wall of; can adjust the length of adjusting column 7 between for dead lever 24 through being provided with first elastic pin 28, thereby can adjust impact head 26's elongation, generally need face the phenomenon of broken window at the scene of a fire, utilize impact head 26 to strike the glass surface, set up impact head 26 to the effect that the toper structure can improve impact force, utilize the reaction force when spring 25 can reduce the impact to cause the damage to unmanned aerial vehicle simultaneously, utilize spacing post 27 can effectually to strike first 26 impact paths and lead, avoid the impact process to take place to skid.
This embodiment is used: firstly, an unmanned aerial vehicle is placed on a horizontal plane through a support rod 9 and an anti-skid column 10, then a paddle 40 and a telescopic rod 2 are respectively unfolded, meanwhile, the length of the telescopic rod 2 is adjusted according to the specific situation of a fire scene, then the unmanned aerial vehicle is controlled to take off through a controller, the unmanned aerial vehicle can crush glass on the fire scene by using an impact head 26 in the process of approaching the fire scene, the damage to the unmanned aerial vehicle is avoided, meanwhile, an anti-shaking pan-tilt assembly 17 and a exploration camera 22 are controlled through the controller, the exploration camera 22 carries out shooting exploration on the fire scene, relevant information of exploration is fed back to the controller, in the exploration process, a driving motor 20 is controlled to drive a swing arm 19 to rotate, so that the outer surface of a transparent columnar shell 8 is cleaned by using an adhesive roller 18, and the cleanness of the outer surface of the transparent columnar shell 8 is ensured, avoid materials such as dust to cause the influence to the exploration of exploration camera 22, can monitor the temperature at the scene of a fire through passing through temperature sensor 5 and laser radar probe 6, simultaneously can effectually avoid unmanned aerial vehicle to bump, can hang equipment of saving oneself in advance on couple 11 so that stranded personnel can save oneself in this moment, warning light 14 can carry out strong warning to stranded personnel simultaneously to can be quick carry stranded personnel department of saving oneself equipment.
Example 2:
an unmanned aerial vehicle for fire scene exploration is shown in fig. 9, and aims at avoiding the temperature of the unmanned aerial vehicle during exploration; the present embodiment is modified from embodiment 1 as follows: a water tank 42 and a top plate 46 are fixed on the outer wall of the bottom of the fixed seat 1 through bolts, a pressure pump 41 is fixed on the outer wall of the top plate 46 through bolts, steel water pipes 45 are fixed on the output ends of the pressure pumps 41 through flanges, one end of one steel water pipe 45 is connected to the outer wall of one side of the water tank 42 through a flange, a water storage disc 44 is welded at one end of the other steel water pipe 45, and more than two spraying discs 43 are welded on the outer wall of the circumference of the water storage disc 44; can utilize force (forcing) pump 41 to follow the blowout in the atomizing mode with rivers from spraying dish 43 through being provided with water tank 42, can form one cascade all around unmanned aerial vehicle, thereby can be to whole unmanned aerial vehicle when cooling down, avoid the high temperature to cause the unmanned aerial vehicle surface to burn, utilize the spraying to carry out moist to adhesion roller 18 circumference outer wall simultaneously, thereby can improve adhesion roller 18 and to the absorptive efficiency of dust, improve the efficiency of exploration when carrying out the protection to unmanned aerial vehicle.
This embodiment is used: at the in-process of unmanned aerial vehicle exploration, utilize the controller to pass through force (forcing) pump 41 with the water in the water tank 42 and spout in spraying dish 43, spraying dish 43 sets up in water storage dish 44 circumference outer wall, can make the even coverage unmanned aerial vehicle of spraying around to cooling down and protecting unmanned aerial vehicle, the high temperature that can effectually prevent the scene of fire causes the damage to unmanned aerial vehicle's protective cover plate 4 and relevant electronic components.
The above description is only for the preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art should be considered to be within the technical scope of the present invention, and the technical solutions and the inventive concepts thereof according to the present invention should be equivalent or changed within the scope of the present invention.
Claims (10)
1. An unmanned aerial vehicle for fire scene exploration comprises a fixed seat (1) and is characterized in that the outer wall of the bottom of the fixed seat (1) is fixedly provided with a top column (23) through a bolt, the outer wall of the bottom of the top column (23) is rotatably connected with an anti-shaking pan-tilt assembly (17) through a bearing, the outer wall of one side of the anti-shaking pan-tilt assembly (17) is rotatably connected with an exploration camera (22) through a bearing, the outer wall of the bottom of the fixed seat (1) is fixedly provided with a transparent cylindrical shell (8) through a bolt, the outer wall of one side of the transparent cylindrical shell (8) is fixedly provided with a mounting frame (21) through a bolt, the outer wall of one side of the mounting frame (21) is fixedly provided with a driving motor (20) through a bolt, the outer walls of the two sides of the transparent cylindrical shell (8) are rotatably connected with swing arms (19) through rotating, the inner wall of one side of each of the two swing arms (19) is rotatably connected with the same adhesion roller (18).
2. The unmanned aerial vehicle for fire scene exploration according to claim 1, wherein four supporting seats (37) are fixed on the outer wall of the fixing seat (1) through bolts, four outer walls on one side of the supporting seats (37) are rotatably connected with the telescopic rod (2) through rotating shafts, and four outer walls on one side of the telescopic rod (2) are respectively clamped on four outer walls on one side of the supporting seats (37) through buckles, four outer walls on the circumference of the telescopic end of the telescopic rod (2) are provided with second elastic pins (38), and the outer walls on the circumference of the second elastic pins (38) are clamped on the outer walls on the circumference of the bracket (3).
3. An unmanned aerial vehicle for fire scene exploration according to claim 2, wherein four telescopic rods (2) have mounting cylinders (34) welded to the telescopic ends, four mounting cylinders (34) have two cylindrical plates (35) welded to the inner circumferential wall, and the inner wall of one side of two cylindrical plates (35) in the same mounting cylinder (34) is fixed with the same double-shaft motor (33) through bolts.
4. The unmanned aerial vehicle for fire scene exploration according to claim 3, wherein four output ends of said double-shaft motor (33) are respectively fixed with a rotating frame (36) through bolts, two blades (40) are respectively rotatably connected to two side outer walls of eight rotating frames (36), and more than two heat dissipation holes (39) are respectively arranged on the circumference outer walls of four mounting cylinders (34).
5. The unmanned aerial vehicle for fire scene exploration according to claim 1, wherein a battery (15) is fixed on the inner wall of the top of the fixing base (1) through bolts, a heat dissipation copper sheet (16) is welded on the inner wall of one side of the fixing base (1), a control unit (13) is arranged on the inner wall of the top of the fixing base (1), a protective cover plate (4) is connected to the outer wall of the fixing base (1) in a sliding mode, and the protective cover plate (4) is fixed on the outer wall of the top of the fixing base (1) through bolts.
6. An unmanned aerial vehicle for fire scene exploration according to claim 1, wherein the outer wall of the bottom of the fixing base (1) is fixed with the temperature sensor (5) and the laser radar probe (6) through bolts respectively.
7. An unmanned aerial vehicle for fire scene exploration according to claim 1, wherein warning lights (14) are fixed on the outer walls of two sides of the fixing base (1) through bolts, a support (3) is fixed on the outer wall of the bottom of the fixing base (1) through bolts, and more than two hooks (11) are slidably connected to the outer wall of the circumference of the support (3).
8. A fire scene exploration unmanned aerial vehicle according to claim 1, fixing base (1) bottom outer wall has four to play post (31), four through the bolt fastening the post (31) circumference outer wall that rises and falls all has holding frame (30), four through the bolt fastening the post (31) both sides outer wall that rises and falls all rotates through the pivot and is connected with L type frame (29), four L type frame (29) inner wall all rotates and is connected with damper assembly (32), four damper assembly (32) keep away from the one end of L type frame (29) and rotate respectively connect in four holding frame (30) inner wall, four connecting rod (12) have all been welded to L type frame (29) bottom outer wall, are located two of homonymy connecting rod (12) circumference inner wall sliding connection has same bracing piece (9), two bracing piece (9) circumference outer wall all sliding connection has three non slipping spur (10).
9. The unmanned aerial vehicle for fire scene exploration according to claim 1, wherein the outer wall of the bottom of the fixing base (1) is fixed with a fixing rod (24) through a bolt, the inner wall of the circumference of the fixing rod (24) is slidably connected with an adjusting column (7), the outer wall of the circumference of the adjusting column (7) is provided with more than two first elastic pins (28), the outer wall of one side of the adjusting column (7) is welded with more than two springs (25), more than two springs (25) are welded with the same impact head (26) at the end of the adjusting column (7) away from the one end of the springs (25), the outer wall of one side of the impact head (26) is welded with a limit column (27), and the outer wall of the circumference of the limit column (27) is slidably.
10. The unmanned aerial vehicle for fire scene exploration according to claim 1, wherein the outer wall of the bottom of the fixing base (1) is fixed with a water tank (42) and a top plate (46) through bolts, the outer wall of the top plate (46) is fixed with a pressure pump (41) through bolts, the output end of each pressure pump (41) is fixed with a steel water pipe (45) through a flange, one end of each steel water pipe (45) is connected to the outer wall of one side of the water tank (42) through a flange, a water storage disc (44) is welded at one end of the other steel water pipe (45), and more than two spraying discs (43) are welded on the outer wall of the circumference of the water storage disc (44).
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| Application Number | Priority Date | Filing Date | Title |
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| CN202010891561.0A CN111959752A (en) | 2020-08-31 | 2020-08-31 | Unmanned aerial vehicle for fire scene exploration |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202010891561.0A CN111959752A (en) | 2020-08-31 | 2020-08-31 | Unmanned aerial vehicle for fire scene exploration |
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| CN111959752A true CN111959752A (en) | 2020-11-20 |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112439141A (en) * | 2020-12-07 | 2021-03-05 | 江苏东迈重工机械有限公司 | Buffer device in high-altitude operation protection robot |
| CN112802412A (en) * | 2020-12-31 | 2021-05-14 | 中国海洋大学 | Day and night commuting anti-gathering optical radar capable of carrying unmanned aerial vehicle in epidemic situation |
| CN113812390A (en) * | 2021-09-28 | 2021-12-21 | 海南大学 | Natural rubber tree system of dusting that unmanned aerial vehicle used |
| CN115514872A (en) * | 2022-11-01 | 2022-12-23 | 连云港市消防救援支队 | Special vehicle for fire scene investigation |
| US11673662B1 (en) * | 2022-01-05 | 2023-06-13 | Textron Innovations Inc. | Telescoping tail assemblies for use on aircraft |
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2020
- 2020-08-31 CN CN202010891561.0A patent/CN111959752A/en not_active Withdrawn
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112439141A (en) * | 2020-12-07 | 2021-03-05 | 江苏东迈重工机械有限公司 | Buffer device in high-altitude operation protection robot |
| CN112802412A (en) * | 2020-12-31 | 2021-05-14 | 中国海洋大学 | Day and night commuting anti-gathering optical radar capable of carrying unmanned aerial vehicle in epidemic situation |
| CN113812390A (en) * | 2021-09-28 | 2021-12-21 | 海南大学 | Natural rubber tree system of dusting that unmanned aerial vehicle used |
| US11673662B1 (en) * | 2022-01-05 | 2023-06-13 | Textron Innovations Inc. | Telescoping tail assemblies for use on aircraft |
| US20230211878A1 (en) * | 2022-01-05 | 2023-07-06 | Textron Innovations Inc. | Telescoping Tail Assemblies for Use on Aircraft |
| US20230264813A1 (en) * | 2022-01-05 | 2023-08-24 | Textron Innovations Inc. | Telescoping Tail Assemblies for Use on Aircraft |
| CN115514872A (en) * | 2022-11-01 | 2022-12-23 | 连云港市消防救援支队 | Special vehicle for fire scene investigation |
| CN115514872B (en) * | 2022-11-01 | 2024-05-28 | 连云港市消防救援支队 | Special vehicle for fire scene investigation |
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Application publication date: 20201120 |