CN104494821B - The many rotor wing unmanned aerial vehicles of a kind of multifunction emergency rescue - Google Patents
The many rotor wing unmanned aerial vehicles of a kind of multifunction emergency rescue Download PDFInfo
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- CN104494821B CN104494821B CN201410817862.3A CN201410817862A CN104494821B CN 104494821 B CN104494821 B CN 104494821B CN 201410817862 A CN201410817862 A CN 201410817862A CN 104494821 B CN104494821 B CN 104494821B
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Abstract
The invention discloses the many rotor wing unmanned aerial vehicles of a kind of multifunction emergency rescue, belong to unmanned plane air rescue technical field. Frame of the present invention is stretched out six horns along its body, and carry frame passes through carry bar carry in unmanned plane organism bottom; Flight hoisting mechanism is arranged at the end of horn, the output of the electron speed regulator of this flight hoisting mechanism connects motor, the bottom of screw is provided with a Fast detachable unit, and screw is flexibly connected with motor by this Fast detachable unit, and Electric Machine Control screw rotates with different rotating speeds; Search mechanism and comprise amplify megaphone and the second camera assembly, the second camera assembly is used for searching the best region of throwing in; Location throwing mechanism comprises the first camera assembly and detacher, and the first camera assembly is for accurately locating release position, and detacher is used for carry, throws in relief goods or equipment. Unmanned plane of the present invention can carry emergency management and rescue goods and materials or equipment arrives rescue site fast, and input accuracy rate is high, and in time, rescue efficiency is high in rescue.
Description
Technical field
The present invention relates to unmanned plane air rescue technical field, more particularly, relate to the many rotors of a kind of multifunction emergency rescue withoutMan-machine.
Background technology
China is a natural calamity and the higher country of human accident occurrence frequency, seismic sea wave, volcano eruption, heavy rain, coldFloating ice freezes, high temperature and drought, mud-stone flow disaster etc., and people's the security of the lives and property has been arrived in serious threat. Under normal circumstances, wheneverWhen the condition of a disaster or accident occur, can be accompanied by the injured, stranded of personnel. And always there is following problem in traditional rescue mechanism: 1)Due to the condition of a disaster or scene of the accident situation conventionally more complicated, cause finding in time to treat rescue worker; 2) when the condition of a disaster or accident occurThere will be the situations such as road is obstructed, cause road surface rescue personnel and goods and materials not to be in time, easily miss best rescue opportunity,Rescue success rate is low; 3) ground rescue personnel enters the condition of a disaster or the scene of the accident, and self personal safety also can not get ensureing.
How to promote and bring into play emergency management and rescue means, scientificlly and effectively tackle disaster, open a life passage with ground aloft,Build the condition of a disaster accident rescue network guarantee system of vacant lot one, guarantee effective enforcement aerial, ground two line rescues, becomeThe problem of international community and inter-governmental extensive concern.
Through retrieval, China Patent No. ZL201120514059.4, Granted publication day is on September 5th, 2012, innovation and creation nameBe called: the comprehensive deliverance apparatus in waters, high-altitude, this application case comprises flight conveyer, is connected to the connection on described flight conveyerBlock, be connected to escape lowering means and water rescue device and the radio communication control on described flight conveyer by Connection CardSystem processed. This application case can be connected with Connection Card respectively by escape lowering means or water rescue device of replacing, divides other placesThe situation of reason building rescue or water life-saving, how more effectively more whole process can instruct captive by wireless communication control systemSafety operation deliverance apparatus and realize the adjusting of fireman to decrease speed and static line length, improve rescue efficiency, make byThe person of rescuing is out of danger as early as possible.
And for example China Patent No. ZL201320852797.9, Granted publication day is on June 4th, 2014, invention and created name is:For a goods delivery device for depopulated helicopter, this application case comprises support, spherical container, loop bracket, described supportTop is fixedly connected with unmanned plane belly, and bottom is provided with little axle and loop bracket travel range monitoring apparatus, one end of described little axle withLoop bracket connects, and the other end is connected with electric control system by shaft coupling, and described spherical container is arranged on loop bracket.Goods delivery device is arranged on to depopulated helicopter belly, can makes originally can not by unmanned plane computer system or remote computer controlThe depopulated helicopter of transporting cargo, the ability that possesses loading, transport and throw in goods. This application case can be used for rescue and relief work, fortuneSend first aid goods and materials, medicine etc. But above-mentioned application case complex structure, manufacturing cost are high, are difficult to popularize, particularly deliverance apparatus is thrownPut accuracy rate low, lack practicality.
Summary of the invention
1. the technical problem that invention will solve
The present invention is directed to the problems such as traditional emergency management and rescue scheme is found to treat rescue worker not in time, and rescue efficiency is low, one is providedThe many rotor wing unmanned aerial vehicles of multifunction emergency rescue; In the present invention, unmanned plane carries emergency management and rescue goods and materials or equipment arrival rescue site fast,Rescue personnel accurately controls input according to camera filmed image, and input accuracy rate is high, and in time, rescue efficiency is high in rescue.
2. technical scheme
For achieving the above object, technical scheme provided by the invention is:
The many rotor wing unmanned aerial vehicles of a kind of multifunction emergency rescue of the present invention, comprise frame, flight hoisting mechanism, search mechanism and fixedPosition throwing mechanism, wherein:
Described frame comprises horn and carry frame, and frame is stretched out six horns along its body, and described horn is folding structure;Organism bottom load has carry bar, and carry frame passes through this carry bar carry in unmanned plane organism bottom;
Described flight hoisting mechanism is arranged at the end of horn, and this flight hoisting mechanism comprises electron speed regulator, motor and spiralOar, the output of electron speed regulator connects motor, the bottom of screw is provided with a Fast detachable unit, screw by this Fast detachable unit withMotor is flexibly connected, and Electric Machine Control screw rotates with different rotating speeds;
Described search mechanism comprises amplify megaphone and the second camera assembly, and the second camera assembly is used for searching the best region of throwing in;
Described location throwing mechanism comprises the first camera assembly and detacher, and the first camera assembly is used for accurately location release position,Detacher is for carry, input relief goods or equipment.
Further, be mounted with GPS position indicator and wide-angle searchlight on described horn, the optical axis of wide-angle searchlight is at 60 °Rotation in scope.
Further, this rescue unmanned plane also comprises salvaging mechanism, and described salvaging mechanism comprises wire spool, cable and salvagingPincers, wire spool is arranged on carry frame, and described cable disc is around on wire spool, and cable is connected with salvaging pincers.
Further, the second described camera assembly comprises carry part, carry plate, X-axis brushless electric machine, The Cloud Terrace support, YAxle brushless electric machine, camera pedestal and Zoom camera, carry part is sleeved on carry bar, and this carry part and carry plate are connected,The bottom of carry plate is fixed with X-axis brushless electric machine, the rotation of X-axis brushless electric machine control The Cloud Terrace support; One end of The Cloud Terrace support is connectedThere is Y-axis brushless electric machine, the rotation of Y-axis brushless electric machine control camera pedestal; Described camera pedestal comprises base plate, the first sidePlate and the second side plate, the first side plate and the engaging of the second side plate are fixed on Zoom camera on base plate.
Further, the first described camera assembly comprises optically focused searchlight, camera and rotary head, rotary head carryOn carry bar, the both sides of this rotary head are provided with optically focused searchlight, and the bottom of rotary head is provided with camera, rotation cloudPlatform drives camera taking vertical direction as 360 ° of rotations of axle.
Further, described detacher comprises gangbar, tripping-bar and parabolic hook, and one end of gangbar and unhook motor connectConnect, the other end of this gangbar is connected with tripping-bar; Described parabolic hook is by forming more than the semicircular ring of 2, and tripping-bar runs throughParabolic hook, blocks the opening of parabolic hook.
Further, described unmanned plane body top is also provided with bucker.
3. beneficial effect
Adopt technical scheme provided by the invention, compared with existing known technology, there is following remarkable result:
(1) the many rotor wing unmanned aerial vehicles of a kind of multifunction emergency rescue of the present invention, it searches the best district of throwing in by the second camera assemblyTerritory, the first camera assembly is accurately located release position, and input accuracy rate is high; Detacher is by the Electric Machine Control that breaks off relations, can by carry inRelief goods on it or equipment, as required by a batch input, have increased the reasonability of throwing in; And relief goods or equipment load rapidly,Save the time for unmanned plane drops into rescue work, increased the promptness of rescue;
(2) the many rotor wing unmanned aerial vehicles of a kind of multifunction emergency rescue of the present invention, its carry frame, the first camera assembly, the second shootingAssembly and amplify megaphone all by carry bar carry in unmanned plane organism bottom, and horn is folding structure, non-working conditionUnder can be by unmanned plane quick-detachment, folding being put in a containing box, transport, easy to carry, can rapid-assembling when use, practicalityProperty is strong.
Brief description of the drawings
Fig. 1 is the structural representation of the many rotor wing unmanned aerial vehicles of a kind of multifunction emergency rescue of the present invention;
Fig. 2 is the structural representation of folded piece in the present invention;
Fig. 3 is many rotor wing unmanned aerial vehicle dismountings of the present invention, folding rear structural representation;
The schematic diagram that (a) in Fig. 4 is connected with screw with motor, Fast detachable unit for Fast detachable unit in the present invention with (b);
Fig. 5 be in the present invention carry in the structural representation of carry Gan Shangge mechanism;
Fig. 6 be in the present invention detacher schematic diagram is set;
Fig. 7 is the structural representation of the second camera assembly in the present invention.
Label declaration in schematic diagram:
1, bucker; 21, GPS position indicator; 22, wide-angle searchlight; 31, horn; 32, folded piece; 321, first connectPipe; 322, articulated elements; 323, second take over; 324, buckle; 33, carry frame;
41, motor; 42, Fast detachable unit; 421, Fast detachable unit base; 4211, base termination; 4212, fixing hole; 4213, fixedHole, position; 422, the Fast detachable unit seat of honour; 423, jump ring; 424, M3 screw; 425, alignment pin; 43, screw;
5, the first camera assembly; 51, optically focused searchlight; 52, camera; 53, rotary head; 61, wire spool; 62, lineCable; 63, salvage pincers; 7, the megaphone that amplifies;
8, the second camera assembly; 81, carry part; 82, carry plate; 83, X-axis brushless electric machine; 84, The Cloud Terrace support; 85,Y-axis brushless electric machine; 861, base plate; 862, the first side plate; 863, the second side plate; 87, Zoom camera;
91, unhook motor; 921, gangbar; 922, tripping-bar; 93, parabolic hook; 101, lifebuoy; 102, fire-fighting band;11, carry bar.
Detailed description of the invention
For further understanding content of the present invention, the present invention is described in detail in conjunction with the accompanying drawings and embodiments.
Embodiment 1
Referring to Fig. 1, in view of in the time facing flood damage or swimmer in the drowned accident of profundal zone generation, traditional water life-saving dressAlways put to exist and find to treat rescue worker not in time, in amateur rescue personnel's water, rescue success rate and only have 40%, and self dangerHigh problem, the present embodiment provides the many rotor wing unmanned aerial vehicles of emergency management and rescue on a kind of multifunctional water, comprises that frame, flight promoteMechanism, search mechanism and location throwing mechanism, wherein:
Described frame is stretched out 31, six horns 31 of six horns along its body and is uniformly-spaced arranged around body, can ensure unmannedThe stability of machine flight. The present embodiment horn 31 is folding structure, and its root is provided with folded piece. The concrete structure of folded pieceReferring to Fig. 2, described folded piece comprises that the first adapter 321, articulated elements 322, the second adapter 323 and buckle 324, the first connectPipe 321, the second adapter 323 and horn 31 fits, the first adapter 321 and second is taken over 323 and is connected by articulated elements 322 activitiesConnect; Described buckle 324 is arranged in the second adapter 323, and the first adapter 321, the second adapter 323 are limit by buckle 324Position is fixing.
Organism bottom load has carry bar 11, and carry frame 33, search mechanism, salvaging mechanism and location throwing mechanism are all by this extensionCarry bar 11 carries in unmanned plane organism bottom. Under non-working condition, can extract carry bar 11 out, by quick above-mentioned each mechanism of carryDismounting, then horn 31 is folded, folding rear effect is referring to Fig. 3, and so, folding rear unmanned plane takes up room very little, Neng GoufeiOften be positioned over easily in aluminum storage box, transport, easy to carry, also can rapid-assembling when use, practical.
Described flight hoisting mechanism is arranged at the end of six horns 31, and this flight hoisting mechanism comprises electron speed regulator, motor41 and screw 43, the end of horn 31 arranges motor cabinet, and motor 41 is installed on motor cabinet, the output of electron speed regulatorConnect motor 41, motor 41 is controlled screw 43 and is rotated with different rotating speeds. What deserves to be explained is, the present embodiment is at screw 43Bottom be provided with a Fast detachable unit 42, referring to (a) in Fig. 4 and (b), Fast detachable unit 42 comprises Fast detachable unit base 421, fastDisassemble the seat of honour 422 and jump ring 423, the middle part of Fast detachable unit base 421 is provided with base termination 4211, on base termination 4211, opensBe provided with external screw thread. On Fast detachable unit base 421, offer fixing hole 4212 and locating hole 4213 along the surrounding of base termination 4211,M3 screw 424 is fixed on Fast detachable unit base 421 on motor 41 through fixing hole 4212. The described Fast detachable unit seat of honour 422Bottom offers the screwed hole coordinating with base termination 4211, and also offers fixing hole and locating hole on the Fast detachable unit seat of honour 422,M3 screw 424 is fixing with screw 43 by the Fast detachable unit seat of honour 422 through fixing hole, the Fast detachable unit seat of honour 422 and screw 43Between also accompany jump ring 423. Alignment pin 425 passes the locating hole of offering on the Fast detachable unit seat of honour 422, when assembling screw 43,422 bottom thread holes, the Fast detachable unit seat of honour coordinate with the base termination 4211 of Fast detachable unit base 421, are screwed into after 90 ° locationPin 425 snaps in locating hole 4213, can ensure that screw 43 acceleration or decelerations rotate in the same direction time, and the Fast detachable unit seat of honour422 do not separate all the time with Fast detachable unit base 421, and then screw 43 does not depart from unmanned plane body and causes while ensureing unmanned plane operationAccident. Same, when dismounting screw 43, rightabout turns the Fast detachable unit seat of honour 422, and alignment pin 425 departs from locating hole 4213,It is quick release screw 43. Can screw 43 be installed on to the output of motor 41 in 3s by this Fast detachable unit 42,Or pull down from motor 41.
The present embodiment is also mounted with GPS position indicator 21 and wide-angle searchlight 22 on horn 31. GPS position indicator 21 is for insteadThe positional information of feedback unmanned plane, facilitates ground commanding to control unmanned plane during flying to rescue region. Wide-angle searchlight 22 adopts largePower LED electricity-saving lamp, model is LM-W150, power is 150w, adds blade inserting radiating aluminium sheet on it, so, wideAngle searchlight 22 can work long hours, and does not worry causing because lamp body is overheated fault, and searchlight extends service life. Wide-angle is visitedIlluminator 22 is by a tilt-top control, and its optical axis can rotate within the scope of 60 °, in the time there is dangerous situation in night, and wide-angle searchlight22 can be for ground provides intense light source, wide region searchlighting, and guarantee unmanned plane finds to treat rescue worker in time.
Referring to Fig. 5 and Fig. 7, described search mechanism comprises amplify megaphone 7 and the second camera assembly 8, and the megaphone 7 that amplifies is hungBe loaded on the crossbeam of carry frame 33, the megaphone 7 that amplifies is mainly used in conveying a message and treats rescue worker to ground, gives and treats rescue workerThe confidence that can be rescued, also can instruct and treat that rescue worker coordinates rescue, to increase the validity of rescue simultaneously. Described second takes the photographComprise the steady The Cloud Terrace of automatic increasing and Zoom camera 87 as assembly 8, automatically increase steady The Cloud Terrace and comprise carry part 81, carry plate 82, XAxle brushless electric machine 83, The Cloud Terrace support 84, Y-axis brushless electric machine 85, camera pedestal. Carry part 81 is sleeved on carry bar 11Upper, this carry part 81 is connected with carry plate 82, and the bottom of carry plate 82 is fixed with X-axis brushless electric machine 83, X-axis is brushless electricityThe output of machine 83 is connected with The Cloud Terrace support 84, and X-axis brushless electric machine 83 is controlled The Cloud Terrace support 84 and rotated. The Cloud Terrace support 84 isL-type structure, one end of The Cloud Terrace support 84 is fixed with Y-axis brushless electric machine 85, and Y-axis brushless electric machine 85 is controlled camera pedestal and is revolvedTurn. Described camera pedestal comprises base plate 861, the first side plate 862 and the second side plate 863, the first side plates 862 and the second sidePlate 863 engages and is bolted, and Zoom camera 87 is fixed on base plate 861. In the present embodiment, automatically increase steady The Cloud TerraceCan ensure that Zoom camera 87 is because the factors such as air-flow shake, ensure that photographic images is clear. Meanwhile, in the non-use of unmanned planeUnder state, also Zoom camera 87 fast dismantlings can be removed, while ensureing transport, Zoom camera 87 is not collided, and causes damaging.Zoom camera 87 adopts the video camera of 30 times of zooms, and this Zoom camera 87 is rotated by ground control's personnel control, for searchingSeek drowned personnel, determine the best region of throwing in.
The present embodiment mid frame, automatically increase steady The Cloud Terrace etc. and all adopt carbon fibre material preparation, it is very high that carbon fibre material is that one hasThe high-temperature fibre of strength and modulus, the main body rack of unmanned plane adopts carbon fibre material, can ensure that unmanned plane volume is little, heavyAmount is light, frame strength is high, and greatly extend service life.
Described location throwing mechanism comprises the first camera assembly 5 and detacher, and the first described camera assembly 5 comprises optically focused spyIlluminator 51, camera 52 and rotary head 53, rotary head 53 carries on carry bar 11, the both sides of this rotary head 53Be provided with optically focused searchlight 51, the bottom of rotary head 53 is provided with camera 52, rotary head 53 drive camera 52 withVertical direction is 360 ° of rotations of axle, and camera 52 adopts ccd high definition pick-up head. The first camera assembly 5 is mainly used inBefore throwing in lifebuoy 101, accurately locate the accuracy rate of release position to ensure to throw in, simultaneously in order also to protect in the time rescuing nightDemonstrate,prove high input accuracy rate, the present embodiment is specially provided with 2 power near the position of camera 52 and is on rotary head 53The LED electricity-saving lamp (being optically focused searchlight 51) of 90w, the light beam of optically focused searchlight 51 can be thrown in region by positive lock, noDisturbed by flight attitude, camera 52 uses that optically focused searchlight 51 can provide stable, picture sends ground control to clearlyCenter, is convenient to staff and determines input opportunity.
Described detacher is for carry, input relief goods or equipment, and the situation for the present embodiment for water life-saving, takes offHook device is mainly used in carry lifebuoy 101, and this lifebuoy 101 is fixed by rope, is placed on the vertical beam of carry frame 33, ensures to rescueRaw circle 101 does not swing with the wind. Referring to Fig. 6, detacher comprises gangbar 921, tripping-bar 922 and parabolic hook 93, gangbarOne end of 921 is connected with unhook motor 91, and the other end of this gangbar 921 is connected with tripping-bar 922; Described parabolic hook 93Can be by forming more than the semicircular ring of 2, tripping-bar 922 runs through parabolic hook 93, blocks the opening of parabolic hook 93, the present embodimentMiddle parabolic hook 93 comprises 2 semicircular ring, and 2 semicircular ring mark off two parabolic opportunitys, and in a semicircular ring, carry is connected with 2The rope of individual lifebuoy 101.
The present embodiment is searched drowned by 30 times of Zoom cameras of the steady cradle head control of automatic increasing of the second camera assembly 8 in boundless and indistinct watersPersonnel, after finding drowned personnel, rapidly near also tentatively irising out the best region of throwing in; Subsequently, ground control personnel are by theThe shooting picture that one camera assembly 5 is passed back, fine setting unmanned plane during flying position, accurately locates release position, and detacher is by the motor that breaks off relations91 control, and drive parabolic hook 93 retraction half by gangbar 921, throw in advance two lifebuoys 101, depending on input situation againDetermine the input opportunity of latter two lifebuoy 101, treat that rescue worker can catch rapidly a nearest lifebuoy 101,Buoyancy by lifebuoy 101 swims in the water surface, products for further rescue.
The present embodiment is searched the best region of throwing in by the second camera assembly 8, accurately location release position of the first camera assembly 5, andLifebuoy 101, as required by a batch input, is increased to the reasonability of throwing in, thrown in accuracy rate and greatly increased. Concrete applicationIn, can be according to rescue site actual conditions, the more lifebuoys 101 of carry, or point more multiple batches of input, carry and input principleSimilar. While being applied to other rescue sites, also can other relief goods of carry or equipment, during as forest fire, can carry manyIndividual fire-fighting band 102 or medical box etc. are rendered to and are needed region, repeat no more herein. The present embodiment lifebuoy 101 loads rapidly,Save the time for unmanned plane drops into rescue work, increased the promptness of rescue.
What deserves to be explained is, the present embodiment, in order to obtain better result of use, is also provided with bucker at unmanned plane body top1, this bucker 1 has ensured that unmanned plane still can normally drop into rescue work under rainy day condition. In addition, the present embodiment is also provided withSalvaging mechanism, described salvaging mechanism comprises wire spool 61, cable 62 and salvaging pincers 63, wire spool 61 is arranged at carry frameOn 33, described cable 62 coils on wire spool 61, and cable 62 is connected with salvaging pincers 63. Be applied to the present embodiment, beatDrag for the lifebuoy 101 that mechanism is mainly used for input to go out and drag for back, be convenient to the recovery of lifebuoy 101.
The many rotor wing unmanned aerial vehicles of a kind of multifunction emergency rescue described in embodiment 1, have taken into full account what emergency management and rescue were run a race against timeFeature, by carry frame 33, search mechanism, salvaging mechanism and location throwing mechanism all by carry bar 11 carries in nobodyMachine organism bottom, can rapid-assembling when use. The loading of relief goods or equipment is also very fast, does for unmanned plane drops into rescueIndustry has been saved the plenty of time, has improved the promptness of rescue. Search the best region of throwing in by the second camera assembly 8, first takes the photographPicture assembly 5 is location release position accurately, and by relief goods or equipment as required by a batch input, increased reasonability and the standard of throwing inReally rate, whole emergency management and rescue unmanned plane is multiple functional, practical, easy to utilize.
Below schematically the present invention and embodiment thereof are described, this description does not have restricted, shown in accompanying drawing alsoJust one of embodiments of the present invention, actual structure is not limited to this. So, if those of ordinary skill in the artEnlightened by it, in the situation that not departing from the invention aim, design the knot similar to this technical scheme without creationaryStructure mode and embodiment, all should belong to protection scope of the present invention.
Claims (4)
1. the many rotor wing unmanned aerial vehicles of multifunction emergency rescue, is characterized in that: comprise frame, flight hoisting mechanism, pursuit airplaneStructure and location throwing mechanism, wherein:
Described frame comprises horn (31) and carry frame (33), and frame is stretched out six horns (31) along its body, describedHorn (31) is folding structure, is mounted with GPS position indicator (21) and wide-angle searchlight (22) on horn (31), wideThe optical axis of angle searchlight (22) rotates within the scope of 60 °; Organism bottom load has carry bar (11), and carry frame (33) is logicalCross this carry bar (11) carry in unmanned plane organism bottom;
Described flight hoisting mechanism is arranged at the end of horn (31), and this flight hoisting mechanism comprises electron speed regulator, motorAnd screw (43) (41), the output of electron speed regulator connects motor (41), and the bottom of screw (43) is provided with oneFast detachable unit (42), screw (43) is flexibly connected with motor (41) by this Fast detachable unit (42), and motor (41) is controlled spiral shellRevolving oar (43) rotates with different rotating speeds;
Described search mechanism comprises the megaphone that amplifies (7) and the second camera assembly (8), and the second camera assembly (8) is for searchingSeek the best region of throwing in; Described the second camera assembly (8) comprises carry part (81), carry plate (82), X-axis brushless electric machine(83), The Cloud Terrace support (84), Y-axis brushless electric machine (85), camera pedestal and Zoom camera (87), carry part (81)Be sleeved on carry bar (11) upper, this carry part (81) is connected with carry plate (82), and the bottom of carry plate (82) is fixed withX-axis brushless electric machine (83), X-axis brushless electric machine (83) is controlled The Cloud Terrace support (84) rotation; One end of The Cloud Terrace support (84)Be fixed with Y-axis brushless electric machine (85), Y-axis brushless electric machine (85) is controlled camera pedestal rotation; Described camera pedestalComprise base plate (861), the first side plate (862) and the second side plate (863), the first side plate (862) and the second side plate (863)Engaging is fixed on Zoom camera (87) on base plate (861);
Described location throwing mechanism comprises the first camera assembly (5) and detacher, and the first camera assembly (5) is for accurately fixedPosition release position, detacher is for carry, input relief goods or equipment;
Rescue unmanned plane also comprises salvaging mechanism, and described salvaging mechanism comprises wire spool (61), cable (62) and salvaging pincers (63),It is upper that wire spool (61) is arranged at carry frame (33), and described cable (62) coils in wire spool (61) upper, cable (62)Be connected with salvaging pincers (63).
2. the many rotor wing unmanned aerial vehicles of a kind of multifunction emergency rescue according to claim 1, is characterized in that: described firstCamera assembly (5) comprises optically focused searchlight (51), camera (52) and rotary head (53), rotary head (53) carryUpper in carry bar (11), the both sides of this rotary head (53) are provided with optically focused searchlight (51), the end of rotary head (53)Portion is provided with camera (52), and rotary head (53) drives camera (52) taking vertical direction as 360 ° of rotations of axle.
3. the many rotor wing unmanned aerial vehicles of a kind of multifunction emergency rescue according to claim 2, is characterized in that: described unhookDevice comprises gangbar (921), tripping-bar (922) and parabolic hook (93), one end of gangbar (921) and unhook motor (91)Connect, the other end of this gangbar (921) is connected with tripping-bar (922); Described parabolic hook (93) is by more than 2Semicircular ring composition, tripping-bar (922) runs through parabolic hook (93), blocks the opening of parabolic hook (93).
4. the many rotor wing unmanned aerial vehicles of a kind of multifunction emergency rescue according to claim 3, is characterized in that: described is unmannedMachine body top is also provided with bucker (1).
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