CN109263883A - A kind of manned unmanned plane of composite material - Google Patents
A kind of manned unmanned plane of composite material Download PDFInfo
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- CN109263883A CN109263883A CN201811274723.5A CN201811274723A CN109263883A CN 109263883 A CN109263883 A CN 109263883A CN 201811274723 A CN201811274723 A CN 201811274723A CN 109263883 A CN109263883 A CN 109263883A
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Classifications
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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
- A62C—FIRE-FIGHTING
- A62C31/00—Delivery of fire-extinguishing material
- A62C31/005—Delivery of fire-extinguishing material using nozzles
-
- 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
-
- 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
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
-
- 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
- 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
-
- 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
-
- 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
- B64D47/04—Arrangements or adaptations of signal or lighting devices the lighting devices being primarily intended to illuminate the way ahead
-
- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62C—FIRE-FIGHTING
- A62C99/00—Subject matter not provided for in other groups of this subclass
- A62C99/0009—Methods of extinguishing or preventing the spread of fire by cooling down or suffocating the flames
- A62C99/0072—Methods of extinguishing or preventing the spread of fire by cooling down or suffocating the flames using sprayed or atomised water
-
- 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
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Pest Control & Pesticides (AREA)
- Health & Medical Sciences (AREA)
- Public Health (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
Abstract
The invention discloses a kind of manned unmanned planes of composite material, comprising: with respectively by unmanned planes more than three axis of corresponding motor driving, the execution module, the controlling terminal by wirelessly controlling unmanned plane and execution module respectively and for providing the battery of electric energy to execution module that are arranged on unmanned plane；Execution module includes: lighting system, radar life-detection instrument, GPS positioning system and/or high-definition camera；Further include: the fire extinguishing ball unmanned plane of ten or more the broken unmanned planes of detection, ten or more water spray unmanned planes and ten or more.Illumination rescue investigation composite material unmanned aerial vehicle group disclosed by the invention, six rotors can provide the angle for looking down the world for people, the image in disaster area can be transmitted in real time and be come out, rescue personnel is set to have the understanding of an entirety to disaster-stricken situation, radar life-detection instrument can detect the life entity in disaster area simultaneously, can rescue life entity.
Description
Technical field
The present invention relates to air vehicle technique field, more particularly to a kind of manned unmanned plane of composite material.
Background technique
Air crash, shipwreck, warring conflicts, the cruelly probably emergency events such as attack, natural calamity, existing search and rescue investigation way occurs
Mainly include that dispatch personnel carries out the inspection of the scene of a crime, using aircraft or unmanned plane carries out approaching prospecting, using satellite progress remote sensing at
As prospecting, but existing search and rescue survey system has some limitations, and the condition of a disaster especially occurs to off-lying sea, remote districts
The case where, it may cause the delay of rescue opportunity.
Dispatch personnel carries out the inspection of the scene of a crime, relies primarily on professional rescue worker on foot, or take the tools such as vehicle, ship
Go deep into disaster scene, field condition is examined on the spot, survival personnel are searched for and offer timely services, but by landform, sea
The sphere of action of the influence of condition, means of transport performance, personnel is extremely limited, and before fully understanding spot concrete condition, trade
Right dispatch personnel may cause secondary accident and occur.
It carries out approaching search and rescue using aviation aircrafts such as aircraft or unmanned planes and reconnoitre, it can be in the feelings for not going deep into disaster innerland
Under condition, scene is closely reconnoitred, searches for survival personnel, and implement to rescue by launching the modes such as goods and materials.Aircraft speed
Fastly, maneuverability is strong, can devastated be generally investigated and be approached on a large scale detailed survey, but by aviation aircraft voyage and flight speed
Degree is limited, when disaster occurs for the area such as high sea, island, foreign manor, Desert Area, even if with the high subsonics currently generally equipped
Fast aircraft, it is also desirable to which time a few hours reaches field operation, and needs to make a return voyage before running out of gas, although work may be selected in unmanned plane
It is dropped to running out of gas, but is limited by the influence of remote control distance, can not also implement operation to remote areas.
Remotely sensed image is carried out using satellite to reconnoitre, and refers mainly to cross top to disaster place in satellite using Optical Imaging Satellite
Scene is imaged in period, and image data is transmitted to ground system, and rescue worker is obtained by analysis satellite image
The information of disaster scene.The advantage of satellite remote sensing is to realize global arbitrary region fast by way of constellation networking
Speed revisits, and no geographical conditions restrict, and the imaging response time can foreshorten to hour grade even minute grade, but it is limited in that imaging
Resolution ratio is influenced by satellite orbital altitude, only up to be reached meter level at present to decimeter grade, be identified to the small scaled target such as personnel
Scarce capacity, and influenced seriously by weather conditions such as cloud layers, rainy weather can not implement operation.
Moreover, because various the condition of a disasters continuously emerge in recent years, especially occur at night and non-visual place urgent
The condition of a disaster, live illumination become the essential condition that commander obtains precision data, and traditional Drones for surveillance can not be in a short time
See the situation at scene clearly, it is difficult to carry out data and report, increase rescue work difficulty, waste valuable time, constrained
Imitate the speed of rescue.
Especially in small and medium-sized cities, road is crowded, and district vehicles disorderly stop to leave about, and seriously constrains the entrance of fire fighting truck,
To miss best rescue period.Generate various tragedy events.Meanwhile with the development of the city, high-rise resident building is more and more,
For high-rise building using traditional fire-fighting mode poor effect, fireman's rescue physical consumption waste is huge at present, can not find in room
Interior life entity pries open door and wastes a large amount of time.
Therefore, how the problem of a kind of manned unmanned plane of composite material is those skilled in the art's urgent need to resolve is provided.
Summary of the invention
In view of this, being designed reasonable, low in cost, solid resistance to the present invention provides a kind of manned unmanned plane of composite material
With, it is safe and reliable, easy to operate, time saving and energy saving, save fund, compact-sized and easy to use；One kind is provided simultaneously to be based on
Unmanned aviation aircraft is mounted in the in-orbit flight in spacecraft, utilized by the quick delivery system of the space-based of the manned unmanned aerial vehicle group
Its Global coverage characteristic breaches conventional lighter-than-air vehicles voyage and speed of a ship or plane limitation, disaster emergency response speed is improved, using starting with again
Unmanned aviation aircraft is delivered to devastated overhead and carries out approaching prospecting by section, overcomes asking for satellite imagery lack of resolution
Topic improves the efficiency of disaster emergency response.
To achieve the goals above, the present invention adopts the following technical scheme:
A kind of manned unmanned plane of composite material, comprising: with respectively by unmanned planes more than three axis of corresponding motor driving, setting
Execution module on unmanned plane, the controlling terminal by wirelessly controlling unmanned plane and execution module respectively and for executing
The battery of module offer electric energy；Execution module includes: lighting system, radar life-detection instrument, GPS positioning system and/or high definition
Camera；Further include: the fire extinguishing of ten or more the broken unmanned planes of detection, ten or more water spray unmanned planes and ten or more
Ball unmanned plane.
Preferably, broken unmanned plane is detected to include: unmanned plane, the broken motor being arranged on unmanned plane, be horizontally set on
The electric pushrod that connect on unmanned plane and with broken motor drive is arranged on electric pushrod nut seat and for smashing high-rise building
The broken hammer of room windowpane and the emergency survival packet being mounted on electric pushrod nut seat；Electric pushrod is by emergency survival packet
Premises is sent by the high-rise building windowpane smashed；It is placed with hand fire extinguisher in emergency survival packet, fire smothering blanket, disappears
Anti- filtering type self-saving respirator, lifesaving descent control device and the bright light torch with sound and light of alarm；
Preferably, the water tank that unmanned plane lower end is arranged in, the note of water tank upper end is arranged in water spray unmanned plane includes: unmanned plane
Water hole, the water-jet pump for connecting with water tank and being driven from waterproof machine and setting are in jetting pump discharge and for high-rise building glass
The water spout sprayed water in glass window；
Preferably, fire extinguishing ball unmanned plane include unmanned plane, be mounted on unmanned plane lower end and bottom surface right low left high setting deposit ball case,
It is placed on and deposits the sphere of the fire extinguishing in ball case, upper end is hinged on the rollover baffle deposited on ball case and be located at ramped bottom surface right end, setting
In the release motor for depositing ball case lower end, the gear being arranged on release motor output shaft, sending of with gear engaging and move horizontally
Button item is arranged in release upper end of the rack and is used to deposit the release that the fire extinguishing sphere in ball case is sent in high-rise building windowpane
The articulated stand that protrusive plate and both ends are respectively hinged at release rack gear and turn on one's side on baffle；Release rack gear passes through articulated stand band
Dynamic rollover baffle is swung up opening or is closed to lower swing.
It preferably, further include the manned unmanned plane of roof and the manned unmanned plane of floor；
The manned unmanned plane of roof includes at least two unmanned planes, the manned frame of roof being arranged in below unmanned plane, is arranged in roof
The load-carrying attention device linked up with and be arranged on the manned frame of roof on manned frame and with the connection of the manned frame connection of corresponding roof；
The manned unmanned plane of floor includes: that unmanned plane, the left end swing rod being hinged on unmanned plane, the foot that is arranged in swing rod right end step on frame
And the lanyard on unmanned plane is arranged in left end；
Lanyard and foot step on frame mounting.
Preferably, further include master control helicopter, be provided with linear drive apparatus on master control helicopter, driven in straight line
The connection ladder for being sent into fireman in master control helicopter in high-rise building is provided on dynamic device, in master control helicopter
On be provided with for people to be sent to the crane on ground from connection ladder；Linear drive apparatus is gear & rack structure or screw-nut
Structure.
Preferably, braking motor is provided on master control helicopter, braking motor is sequentially connected with reel, connects on reel
It is connected to wirerope, wirerope lower end is connect with crane.
Preferably, the unmanned plane body is made of light composite material, has heat-resisting ability, while the unmanned plane
Body is light, increases increase mission payload.
Preferably, the unmanned plane further includes heat shield, for protecting the fuel tank of aircraft not by region heat radiation of catching fire
It influences.
Preferably, the unmanned plane internal body is additionally provided with combustible gas probe and toxic gas detector, described
Combustible gas probe and the toxic gas detector are connect with the controlling terminal.
It can be seen via above technical scheme that compared with prior art, the present disclosure provides a kind of composite material loads
People's unmanned plane, has the advantages that
1, Drones for surveillance is rescued in illumination disclosed by the invention, and six rotors can provide the angle for looking down the world for people,
The image in disaster area can be transmitted in real time and be come out, rescue personnel is made to have the understanding of an entirety to disaster-stricken situation.
2, requirement of six rotors to takeoff and landing is lower, maneuverability, can ignore complicated surface state, can be low
Empty working flight precisely pinpoints, the position of trapped person is accurately positioned.
3, radar life-detection instrument can be under the non-visual environments such as the flame, smog, interior in the scene of a fire to vital sign mesh
Mark detection and rescue, it is higher than the efficiency of manual search.
4, radar life-detection instrument detection performance and the detection performance of index and currently used hand-held life detection radar
And index is identical, ensure that the accuracy of rescue search.
5, lighting system can provide floodlighting at the disaster relief scene of night and non-view, and the system illumination brightness is high, shine
It is remote to penetrate distance, in high air to surface rescue, investigation saliency advantage also can be rescue personnel, commander's execute-in-place, commander provide
It is effectively convenient.
6, illumination system performance and index are identical as the dedicated shadowless operating lamp performance of operating room and index, ensure that live photograph
Bright clarity, and shade and dark space will not be generated.
7, the unmanned plane can replace rescue personnel and scan for into non-visual dangerous region of search, can be to avoid two
The generation of secondary accident guarantees the maximum value of rescue.
8, detect whether disaster spot has methane, an oxidation by combustible gas probe and toxic gas detector
Carbon, nitric oxide etc. are flammable or toxic gas.
9, the unmanned plane can carry out search and rescue and data acquisition session into land-locked region, allow gold 24 hours
It is more valuable.
10, with strong applicability: be suitble to night and it is all it is non-depending in the case where play its distinctive effect.Strong flexibility:
Drones for surveillance's small volume, light and flexible, multiple functional is rescued in the illumination, can be mobile according to the flexible operation of commander, and
And precision is higher, avoids investigation fault that rescue is caused to omit.Cruise duration is long: the illumination rescues Drones for surveillance equipped with multiple
Power supply, each power supply use special process and technology development and production, and flight time longest can reach 60 minutes, mention for effectively rescue
For sufficiently ensureing.Significant effect: providing abundant brightness for rescue site, guarantee night and it is non-depending in the case where throw away and can carry out just
It is normal detect in the act, data collection and transmission report, and provide most intuitive field condition for commander in time, show convenient for commander
Field commander；Also suing and labouring simultaneously for rescue personnel, it is live after enough illuminances and rescue work to provide with equipment arrangement
Cleaning and equipment regular and collect.
Detailed description of the invention
In order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, to embodiment or will show below
There is attached drawing needed in technical description to be briefly described, it should be apparent that, the accompanying drawings in the following description is only this
The embodiment of invention for those of ordinary skill in the art without creative efforts, can also basis
The attached drawing of offer obtains other attached drawings.
Fig. 1 attached drawing is structural schematic diagram provided by the invention.
Fig. 2 attached drawing is the face upwarding assumption diagram of manned unmanned plane provided by the invention.
Fig. 3 attached drawing is the structural schematic diagram provided by the invention for detecting broken unmanned plane.
Fig. 4 attached drawing is the structural schematic diagram of water spray unmanned plane provided by the invention.
Fig. 5 attached drawing is the structural schematic diagram of fire extinguishing ball unmanned plane provided by the invention.
Fig. 6 attached drawing is the manned unmanned plane structural schematic diagram of roof provided by the invention.
Fig. 7 attached drawing is the manned unmanned plane structural schematic diagram of floor provided by the invention.
Fig. 8 attached drawing is the structural schematic diagram of master control helicopter provided by the invention.
Wherein, 1 is unmanned plane, and 2 be lighting system, and 3 be radar life-detection instrument, and 4 be GPS positioning system, and 5 take the photograph for high definition
As head, 6 be controlling terminal, and 7 be sensorcraft, and 8 be water spray unmanned plane, and 9 be fire extinguishing ball unmanned plane, 10 for roof it is manned nobody
Machine, 11 be the manned unmanned plane of floor, and 12 be master control helicopter, and 13 be broken motor, and 14 be electric pushrod, and 15 is bulky to be crushed
Head, 16 be emergency survival packet, and 17 be water tank, and 18 be water injection hole, and 19 be water-jet pump, and 20 be water spout, and 21 be fire extinguishing sphere, and 22 are
Deposit ball case, 23 be rollover baffle, and 24 be release motor, and 25 be release rack gear, and 26 be release protrusive plate, and 27 be articulated stand, 28
It is connection hook for the manned frame of roof, 29,30 be load-carrying attention device, and 31 be linear drive apparatus, and 32 be connection ladder, and 33 be pendulum
Bar, 34 step on frame for foot, and 35 be lanyard, and 36 be crane.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Referring to attached drawing 1-8, the rescue unmanned plane of the present embodiment, more than with three axis respectively by corresponding motor driving
Unmanned plane 1, the execution module, whole by the control for wirelessly controlling unmanned plane 1 and execution module respectively that is arranged on unmanned plane 1
Hold 6 and for providing the battery of electric energy to execution module；
Execution module includes lighting system 2, radar life-detection instrument 3, GPS positioning system 4 and/or high-definition camera 5.
Such as Fig. 3-8, the rescue group of planes of the present embodiment, the spray including the broken unmanned plane 7, ten of ten or more detections or more
The fire extinguishing ball unmanned plane 9 of water unmanned plane 8 and ten or more；
Fig. 3 detects broken unmanned plane 7 and includes unmanned plane 1, the broken motor 13 being arranged on unmanned plane 1, is horizontally set on nobody
On 14 nut seat of electric pushrod and for smashing height on machine 1 and with the electric pushrod 14 of broken motor 13 transmission connection, setting
The broken hammer 15 of floor room windowpane and the emergency survival packet 16 being mounted on 14 nut seat of electric pushrod；Electric pushrod 14
Emergency survival packet 16 is passed through to the high-rise building windowpane smashed and is sent into premises；It is placed in emergency survival packet 16 portable
Fire extinguisher, fire smothering blanket, filtering respiratory protective devise for self-rescue from fire, lifesaving descent control device and the bright light torch with sound and light of alarm；
Fig. 4, water spray unmanned plane 8 include unmanned plane 1, the water tank 17 that 1 lower end of unmanned plane is arranged in, the note that 17 upper end of water tank is arranged in
Water hole 18 connect with water tank 17 and is exported in water-jet pump 19 from the water-jet pump 19 of waterproof machine drive and setting and be used for height
The water spout 20 sprayed water in floor room windowpane；
Fig. 5, fire extinguishing ball unmanned plane 9 includes unmanned plane 1, is mounted on 1 lower end of unmanned plane and what bottom surface right low left high was arranged deposits ball case
22, it is placed on and deposits the sphere 21 of the fire extinguishing in ball case 22, upper end is hinged on the rollover deposited on ball case 22 and be located at ramped bottom surface right end
Baffle 23 is arranged in and deposits the release motor 24 of 22 lower end of ball case, the gear being arranged on 24 output shaft of release motor, nibbles with gear
Close and move horizontally release rack gear 25,25 upper end of release rack gear is set and for sending the fire extinguishing sphere 21 deposited in ball case 22
To in high-rise building windowpane release protrusive plate 26 and both ends be respectively hinged at release rack gear 25 and rollover baffle 23 on
Articulated stand 27；Release rack gear 25 drives rollover baffle 23 to be swung up opening or be closed to lower swing by articulated stand 27；
It can also further include the manned unmanned plane 10 of roof and the manned unmanned plane 11 of floor；
Fig. 6, the manned unmanned plane 10 of roof include at least two unmanned planes 1, the manned frame 28 of the roof being arranged in below unmanned plane 1,
It is arranged on the manned frame 28 of roof and links up with 29 with the connection that the manned frame 28 of corresponding roof connects and be arranged in the manned frame of roof
Load-carrying attention device 30 on 28；
Fig. 7, the manned unmanned plane 11 of floor include unmanned plane 1, left end be hinged on unmanned plane 1 swing rod 33, be arranged in swing rod 33
The foot of right end steps on frame 34 and the lanyard 35 on unmanned plane 1 is arranged in left end；
Fig. 8, lanyard 35 and foot step on the mounting of frame 34.
It can also further include master control helicopter 12, linear drive apparatus 31 is provided on master control helicopter 12,
The connection ladder 32 for being sent into fireman in master control helicopter 12 in high-rise building is provided on linear drive apparatus 31,
The crane 36 for people to be sent to ground from connection ladder 32 is provided on master control helicopter 12；Linear drive apparatus 31 is tooth
Take turns rack structure or screw-nut structure.
Braking motor is provided on master control helicopter 12, braking motor is sequentially connected with reel, is connected on reel
Wirerope, wirerope lower end are connect with crane 36.
Unmanned plane body is made of light composite material, has heat-resisting ability, while the unmanned plane body is light, increases
Increase mission payload.
Unmanned plane further includes heat shield, for protecting the fuel tank of aircraft not influenced by region heat radiation of catching fire.
Unmanned plane internal body is additionally provided with combustible gas probe and toxic gas detector, combustible gas probe and
Toxic gas detector is connect with controlling terminal；Disaster spot is detected by combustible gas probe and toxic gas detector
Whether there are the fuel gas such as methane, carbon monoxide, avoids that spot fire occurs.
It is controlled about flight: according to engine parameter and throttle position, vertical gyro, rate top being adjusted by controlling terminal
Spiral shell, magnetic row control the flight of unmanned plane to needle, radio altimeter, GPS positioning system 4；Analog module reception vertical gyro,
The signal that rate gyroscope, magnetic row are fed back to needle, radio altimeter, GPS positioning system 4, controls from exporting signal to steering engine
Plate, steering engine control panel control corresponding steering engine rotation；
Radar life-detection instrument 3 is by life signal, and GPS positioning system 4 is by GPS positioning signal, high-definition camera 5 by vision signal
Host is inputed to, host sends a signal to controlling terminal, shows life signal in controlling terminal.Image or vision signal, connect
Receive GPS position information.Above-mentioned module is all prior art module, and the application's generates good use by being combined to use
Effect.
Drones for surveillance is rescued in illumination of the invention, and preferably six axis aircraft, radar life-detection instrument are active radar and passive radar
Life detection and search system are that a kind of combination Active Radar and passive detection Radar Technology are with what is searched for for life detection
System.Active Radar detection system is using Radar Technology, biomedical engineering technology in the life detection equipment of one.It is main
It is made using the principle of reflection of electromagnetic wave, by various fine motions caused by detection human life activity, from these fine motions
To breathing, heartbeat for information about, thus identification whether there is or not life.Passive detection radar system be it is a kind of can to aerial, ground and
Naval target (transmission of electromagnetic signals) is positioned, the electronic detection system for identifying and tracking.Detection performance and index: active thunder
Up to detectivity: penetrate tangible media detection mode: apart from metope distance 30m, penetrating brick masonry wall (thickness 24cm) can be visited
Measure the human body limb fine motion behind wall in 10m: penetrating atomizing medium detection mode: penetrate smog, cloud, water mist etc. (away from
From >=50m) it is able to detect that the limbs fine motion of human body；Distance resolution :≤1m detects subtended angle: effective detecting area is subtended angle 120
Degree, azimuth and pitch angle；More human body targets: target number≤3 can be identified and distinguished between, human body surface radial distance is not less than
1m, orientation angles are not less than 15 degree between target；To life entity goal response time≤30s.Passive radar detection ability: excitation 60
Penetration capacity in rice: 4 layers of brick wall, 2 layers of steel and concrete structure wall；Detect in horizontal office penetration capacity in 300 meters: 3 layers of brick wall, steel reinforced concrete
1 layer of structure wall；Signal detection sensitivity: it is better than -105bm；Speed of detection: detectable signal 60 per minute；Positioning accuracy: excellent
In 8 meters；Working frequency range: 800MHZ/2GHz.Lighting system of the invention is using focusing shadowless lamp and LED operation shadowless lamp technology
It combines, focusing shadowless lamp is a kind of using computer-aided modular design, and plurality of LEDs light beam focusing illumination is most scientific
Radian lamp cap, multi-point source design, realizes long range depth illumination, center illumination highest, and energy conservation and environmental protection long service life, it
The main principle for forming umbra and penumbra using light irradiation object designs, and by multiple light-illuminatings, completely disappears umbra, and half
Shadow, which is also desalinated, becomes nothing, and by focusing technology, realizes the cover and dispersion irradiation of multiple strong light, it is ensured that irradiation object is without umbra
Occur with shadow.Illumination performance and index: illumination capability: maximum illumination distance can reach 100 meters, and multiple light focusings a little shine
It penetrates, multiple light dispersion high definitions are irradiated without shadow, and the irradiation for a long time of LED cold light source will not generate flammability temperature to irradiation object, are used
Service life, single lamp source damage, which will not generate irradiation object, to be significantly affected, when being blocked by multiple objects, together up to 50,000 hours or more
Sample can reach perfect shadowless lighting effect.
Concrete application case: certain urban traffic congestion, vehicle is disorderly parked in cell, and passageway for fire apparatus is occupied by private car.
Gas explosion occurs for one day, dry weather, 35 layers of high building of certain cell, and fire, the fire-fighting monitoring in resident kitchen occurs
Alarm senses flame, and control solenoid valve opening is sprayed water；Solenoid valve power-off, which is opened, sprays water；Solenoid valve is when being powered
Closure water route is waited, power-off when opens water route；The intensity of a fire is small, directly puts out.
One day, dry weather, 35 layers of high building of downtown cell occur gas explosion, fire occur, resident kitchen disappears
Anti- monitoring alarm senses flame, and control solenoid valve opening is sprayed water；Solenoid valve power-off, which is opened, sprays water；Solenoid valve is
It is closed water route when energization, power-off when opens water route；But Running-water Company's maintenance pipeline is encountered just and is cut off the water.
The induction of fire-fighting monitoring alarm, notifies the fire-fighting of other residents of this unit building to monitor by unit building fire-fighting processor
Alarm induction alarm buzzing prompts people's evacuation, and still, since the intensity of a fire is big, Circuit Interrupt, many people can not pass through fire and escape
It is raw, it have to escape to roof；
Community server (generally at property) observes the state of each fire-fighting monitoring alarm by display screen, can normally be
Green, it is improper to alarm for red to be orange, while audio alert or buzzing alarm, to facilitate property fire fighter accurate
Judgement kindling unit building or floor, starting detect broken unmanned plane 7 and are crushed windowpane, specifically, property fire fighter
It drives broken motor 13- electric pushrod 14- nut seat-to be crushed the tip of hammer 15 by battery by remote controler and hits glass,
It being smashed, emergency survival packet 16 is passed through the high-rise building windowpane feeding premises realization smashed and saved oneself by electric pushrod 14,
Certainly passing through radar can more accurately determine that other someone of which family improves to realize precisely dispensing and succours efficiency, reduce
The waste of fire-fighting equipment；Then starting water spray unmanned plane 8 by water-jet pump 19 by the water injection in water tank 17 into high level, pass through
The unmanned plane sprayed is sent in fire-fighting pond by remote control, carries out fast water injection by water injection hole 18, thus delay and reduce the intensity of a fire,
Water-jet pump 19 is common knowledge to motor power supply by motor driven, battery, and motor remote control is obvious common knowledge.It opens
Dynamic fire extinguishing ball unmanned plane 9 is protruded into building by motor-gear-rack gear-release protrusive plate 26, and articulated stand 27 drives rollover gear
Plate 23 is swung up opening, and fire extinguishing sphere 21 rolls into building under Gravitative Loads along bottom surface, release protrusive plate 26, realizes automatic
Fire extinguishing reduces the intensity of a fire.
The unmanned plane that section director server transfers attachment cell is supported, and is equipped with corresponding unmanned plane in each community
Remote controler can be distinguished by color, and the manned frame 28 of roof drops to roof, and people can be connected by connection hook 29
It connects, realize multiple unmanned planes while succouring, prevent from overloading by load-carrying attention device 30 certainly；By radar monitor it is lived live
Swing rod 33 is sent into the resident by family, the manned unmanned plane 11 of floor, and people step on frame 34 at station in foot, takes lanyard 35, swing rod 33
It is vertical to switch to, to be rescued.
Transfer master control helicopter 12, the manned unmanned plane 10 of roof and the manned unmanned plane of floor 11 in urban district total activation station
It helps, fire fighters air transportion to scene of fire field headquarters of going forward side by side is rescued.Fire fighters precisely enter from window according to radar finds life
Body is ordered, the time blindly found waste and physical consumption is avoided, is sent on master control helicopter 12 by ladder, master control
Helicopter 12 is sent to ground by crane 36, greatly improves rescue efficiency.
Each embodiment in this specification is described in a progressive manner, the highlights of each of the examples are with other
The difference of embodiment, the same or similar parts in each embodiment may refer to each other.For device disclosed in embodiment
For, since it is corresponded to the methods disclosed in the examples, so being described relatively simple, related place is said referring to method part
It is bright.
The foregoing description of the disclosed embodiments enables those skilled in the art to implement or use the present invention.
Various modifications to these embodiments will be readily apparent to those skilled in the art, as defined herein
General Principle can be realized in other embodiments without departing from the spirit or scope of the present invention.Therefore, of the invention
It is not intended to be limited to the embodiments shown herein, and is to fit to and the principles and novel features disclosed herein phase one
The widest scope of cause.
Claims (10)
1. a kind of manned unmanned plane of composite material characterized by comprising more than three axis respectively by corresponding motor driving
Unmanned plane (1), execution module on the unmanned plane (1) is set, by wirelessly controlling the unmanned plane (1) and institute respectively
State the controlling terminal (6) of execution module and for providing the battery of electric energy to the execution module；
The execution module includes: that lighting system (2), radar life-detection instrument (3), GPS positioning system (4) and/or high definition are taken the photograph
As head (5)；
Further include: ten or more detections are crushed unmanned plane (7), ten or more water spray unmanned planes (8) and ten or more
Fire extinguishing ball unmanned plane (9).
2. the manned unmanned plane of a kind of composite material according to claim 1, which is characterized in that described to detect broken unmanned plane
(7) include: the unmanned plane (1), be arranged broken motor (13) on the unmanned plane (1), be horizontally set on it is described nobody
In the electric pushrod (14) nut on machine (1) and with the electric pushrod (14) of broken motor (13) transmission connection, setting
On seat and it is used to smash the broken hammer (15) of high-rise building windowpane and is mounted on the electric pushrod (14) nut seat
Emergency survival packet (16)；The emergency survival packet (16) is passed through the high-rise building windowpane smashed by the electric pushrod (14)
It is sent into premises；Hand fire extinguisher, fire smothering blanket, fire-fighting filtering type is placed in the emergency survival packet (16) to save oneself breathing
Device, lifesaving descent control device and the bright light torch with sound and light of alarm.
3. the manned unmanned plane of a kind of composite material according to claim 1, which is characterized in that the water spray unmanned plane (8)
Include: the unmanned plane (1), setting the unmanned plane (1) lower end water tank (17), be arranged in the water tank (17) upper end
Water injection hole (18), the water-jet pump (19) that connect with the water tank (17) and driven by waterproof machine and be arranged in the jetting
Pump (19) outlet and the water spout (20) for spraying water into high-rise building windowpane.
4. the manned unmanned plane of a kind of composite material according to claim 1, which is characterized in that the fire extinguishing ball unmanned plane
(9) include the unmanned plane (1), be mounted on the unmanned plane (1) lower end and what bottom surface right low left high was arranged deposits ball case (22), puts
It sets and is hinged on described deposit on ball case (22) and positioned at the ramped bottom surface right side in the fire extinguishing sphere (21) deposited in ball case (22), upper end
The rollover baffle (23) at end is arranged in the release motor (24) for depositing ball case (22) lower end, is arranged in the release motor
(24) gear on output shaft, the release rack gear (25) for engaging and moving horizontally with gear, setting are in the release rack gear (25)
Upper end and for by the fire extinguishing sphere (21) deposited in ball case (22) be sent to the release in high-rise building windowpane extension
The articulated stand (27) that plate (26) and both ends are respectively hinged at the release rack gear (25) and turn on one's side on baffle (23)；It is described to send
Button item (25) drives the rollover baffle (23) to be swung up opening or be closed to lower swing by the articulated stand (27).
5. the manned unmanned plane of a kind of composite material according to claim 1, which is characterized in that further include roof it is manned nobody
Machine (10) and the manned unmanned plane of floor (11)；
The manned unmanned plane of roof (10) includes at least two unmanned planes (1), is arranged below the unmanned plane (1)
The manned frame of roof (28), the connection for being arranged on the manned frame of the roof (28) and being connected with the corresponding manned frame of roof (28)
The load-carrying attention device (30) linking up with (29) and being arranged on the manned frame of the roof (28)；
The manned unmanned plane of floor (11) includes: the swing rod that the unmanned plane (1), left end are hinged on the unmanned plane (1)
(33), the foot being arranged in the swing rod (33) right end steps on the lanyard of frame (34) and left end setting on the unmanned plane (1)
(35)；
The lanyard (35) and the foot step on frame (34) mounting.
6. the manned unmanned plane of a kind of composite material according to claim 1, which is characterized in that further include master control helicopter
(12), linear drive apparatus (31) are provided on the master control helicopter (12), on the linear drive apparatus (31)
The connection being provided with for the interior fireman of the master control helicopter (12) to be sent into high-rise building is terraced (32), in the master control
The crane (36) for people to be sent to ground from the connection terraced (32) is provided on helicopter (12) processed；The linear drives
Device (31) is gear & rack structure or screw-nut structure.
7. the manned unmanned plane of a kind of composite material according to claim 6, which is characterized in that in the master control helicopter
(12) braking motor is provided on, the braking motor is sequentially connected with reel, and wirerope, the wirerope are connected on reel
Lower end is connect with the crane (36).
8. the manned unmanned plane of a kind of composite material according to claim 1, which is characterized in that the unmanned plane body is by light
Composite material is made, and has heat-resisting ability, while the unmanned plane body is light, increases increase mission payload.
9. the manned unmanned plane of a kind of composite material according to claim 1, which is characterized in that the unmanned plane further includes preventing
Heat cover, for protecting the fuel tank of aircraft not influenced by region heat radiation of catching fire.
10. -9 described in any item a kind of manned unmanned planes of composite material according to claim 1, which is characterized in that it is described nobody
Machine internal body is additionally provided with combustible gas probe and toxic gas detector, the combustible gas probe and described toxic
Gas detector is connect with the controlling terminal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811274723.5A CN109263883A (en) | 2018-10-30 | 2018-10-30 | A kind of manned unmanned plane of composite material |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811274723.5A CN109263883A (en) | 2018-10-30 | 2018-10-30 | A kind of manned unmanned plane of composite material |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109263883A true CN109263883A (en) | 2019-01-25 |
Family
ID=65195206
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811274723.5A Withdrawn CN109263883A (en) | 2018-10-30 | 2018-10-30 | A kind of manned unmanned plane of composite material |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109263883A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110812749A (en) * | 2019-11-13 | 2020-02-21 | 符振锋 | Indoor eminence fire extinguisher |
| CN110917527A (en) * | 2019-12-23 | 2020-03-27 | 郑俊跃 | Fire extinguishing system of high-rise building |
| CN114010982A (en) * | 2021-11-10 | 2022-02-08 | 山东交通学院 | Non-contact type high-rise building fire accident integrated system based on unmanned aerial vehicle |
| CN114812311A (en) * | 2022-04-20 | 2022-07-29 | 中南大学 | Unmanned aerial vehicle directional blasting system and blasting method |
-
2018
- 2018-10-30 CN CN201811274723.5A patent/CN109263883A/en not_active Withdrawn
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110812749A (en) * | 2019-11-13 | 2020-02-21 | 符振锋 | Indoor eminence fire extinguisher |
| CN110917527A (en) * | 2019-12-23 | 2020-03-27 | 郑俊跃 | Fire extinguishing system of high-rise building |
| CN114010982A (en) * | 2021-11-10 | 2022-02-08 | 山东交通学院 | Non-contact type high-rise building fire accident integrated system based on unmanned aerial vehicle |
| CN114812311A (en) * | 2022-04-20 | 2022-07-29 | 中南大学 | Unmanned aerial vehicle directional blasting system and blasting method |
| CN114812311B (en) * | 2022-04-20 | 2023-01-31 | 中南大学 | Unmanned aerial vehicle directional blasting system and blasting method |
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Application publication date: 20190125 |