CN112810817B - Aerial material hook type throwing unmanned aerial vehicle - Google Patents
Aerial material hook type throwing unmanned aerial vehicle Download PDFInfo
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- CN112810817B CN112810817B CN202110195431.8A CN202110195431A CN112810817B CN 112810817 B CN112810817 B CN 112810817B CN 202110195431 A CN202110195431 A CN 202110195431A CN 112810817 B CN112810817 B CN 112810817B
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- aerial vehicle
- unmanned aerial
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- box
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
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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
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/061—Frames
- B64C1/063—Folding or collapsing to reduce overall dimensions, e.g. foldable tail booms
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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
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/068—Fuselage sections
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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
- 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
- B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
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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
- B64D1/00—Dropping, ejecting, releasing or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
- B64D1/14—Absorbing landing shocks
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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
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
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- 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
- B64U2101/60—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The invention discloses an aerial material hook type throwing unmanned aerial vehicle, which comprises an unmanned aerial vehicle main body, a hood, a pod type holder and a throwing device, wherein six groups of unmanned aerial vehicle wings are arranged outside the hood in a surrounding manner, the pod type holder is arranged between two adjacent unmanned aerial vehicle wings outside the hood and is used for shooting high-definition pictures, a foot rest is arranged at the bottom end of the hood, the foot rest is arranged at two sides of the lower end of the hood and is obliquely fixed, the throwing device comprises a throwing device, a throwing box and a protective fixing frame, the throwing device is arranged at the lower end part of an installation frame plate, the throwing box is arranged below the throwing device, hooks are arranged at the upper end of the throwing box, and a shockproof protection pad is arranged at the bottom end of the throwing box; the throwing device is heavy in mounting load, various in throwing modes and high in power for the unmanned aerial vehicle flight platform due to the six-axis design, the number of reciprocating throwing operations is reduced, and the working efficiency is greatly improved. The throwing box effectively protects internal throwing materials, so that the throwing of the materials is completed smoothly.
Description
Technical Field
The invention relates to an unmanned aerial vehicle, in particular to an aerial material hook type throwing unmanned aerial vehicle.
Background
The unmanned plane is called as unmanned plane for short, and is a unmanned plane operated by radio remote control equipment and a self-contained program control device. The machine has no cockpit, but is provided with an automatic pilot, a program control device and other devices. Personnel on the ground, ships or on a mother machine remote control station track, position, remote control, telemetere and digital transmission through radar and other equipment. Can take off like a common plane under radio remote control or launch and lift off by using a boosting rocket, and can also be brought into the air by a master machine to put in flight. When recovered, the aircraft can automatically land in the same way as the landing process of a common aircraft, and can also be recovered by a parachute or a barrier net for remote control. Can be repeatedly used for a plurality of times. The method is widely used for air reconnaissance, monitoring, communication, anti-diving, electronic interference and the like. At present, the main stream is that an unmanned aerial vehicle carries various throwing materials, passes through various complex terrains and severe environments, and opens a throwing box to perform low-altitude throwing after reaching a throwing place.
The traditional unmanned aerial vehicle throwing box has the problems that the volume is too small, the loading materials are limited, the throwing is required to be carried repeatedly, the efficiency is low, the throwing mode is inflexible, for example, the throwing box cannot be filled when throwing large-volume materials such as cotton quilts and the like, the throwing cannot be changed into other modes, particularly, the problem that rescue materials cannot be maximally delivered at the highest speed on the scene of an accident, and the like, the rescue work is influenced to a certain extent, and rescue workers face serious tests; in addition, the protective layer on the outer layer of the traditional throwing material is not firm enough, and the material is easy to damage when falling to the ground after throwing, so that extra loss is caused, and improvement is needed.
Disclosure of Invention
The invention aims to provide an aerial material hook type throwing unmanned aerial vehicle, which aims to solve the problems in the background technology.
In order to achieve the above purpose, the present invention provides the following technical solutions:
The aerial material hook type throwing unmanned aerial vehicle comprises an unmanned aerial vehicle main body, a hood covered outside the unmanned aerial vehicle main body, a nacelle type tripod head and a throwing device with a damping function, wherein six groups of unmanned aerial vehicle wings with folding functions are arranged outside the hood in a surrounding mode;
the nacelle type cradle head is arranged between two adjacent unmanned aerial vehicle wings outside the hood and is used for shooting high-definition pictures;
The bottom end of the head cover is provided with a foot rest, the foot rest is arranged on two sides of the lower end of the head cover and is obliquely fixed, the upper end of the frame body is fixedly provided with a mounting frame plate, and the upper end of the mounting frame plate is provided with a battery electrically connected with the unmanned aerial vehicle main body;
The throwing device comprises a throwing device, a throwing box and a protection fixing frame for limiting the throwing box, the throwing device is arranged at the lower end part of the mounting frame plate, the throwing box is arranged below the throwing device, a hook matched with the throwing device is arranged at the upper end of the throwing box, and a shockproof protection pad is arranged at the bottom end of the throwing box;
the protection mount is including fixing the multiunit body in the foot rest lower extreme both sides, and multiunit body encircles and throws the case and enclose into a rectangular frame, and the body middle part is equipped with and throws case matched with guide pulley, and the body both ends are equipped with folding piece and carbon tube connecting piece that opens and shuts respectively, and body one end is through folding piece and the body clearance fit that its is adjacent that opens and shuts, and the body other end is through carbon tube connecting piece and the body rotation that its is adjacent.
Preferably, the tube body is a carbon fiber tube.
Preferably, unmanned aerial vehicle wing includes main arm, secondary arm and folding piece, and main arm one end and hood lateral wall fixed connection, the main arm other end pass through folding piece and secondary arm swing joint, and the one end that the main arm was kept away from to the secondary arm is equipped with the screw, and the screw is equipped with the motor that is used for driving screw pivoted with the junction of secondary arm.
Preferably, the nacelle type tripod head comprises a fixed bracket and a tripod head main body arranged at the lower end of the fixed bracket, wherein the fixed bracket is horizontally arranged between two adjacent unmanned aerial vehicle wings, and two ends of the fixed bracket are detachably connected with the main arm.
Preferably, the bottom end of the foot rest is fixed with a cross rod supporting piece for improving the placement stability of the foot rest.
Preferably, damping cotton is sleeved at two ends of the cross rod supporting piece.
Preferably, the shockproof protection pad is made of high-density sponge materials, and a spring device playing a role in cushioning is arranged at the end part of the shockproof protection pad.
Preferably, the spring devices are arranged in a plurality of groups, and are respectively arranged in the center and four corners of the lower end part of the shockproof protection pad.
Preferably, the hood comprises an upper shell and a lower shell, the upper shell is covered on the upper end part of the unmanned aerial vehicle body, the lower shell is covered on the lower end part of the unmanned aerial vehicle body, and the upper shell and the lower shell are mutually buckled.
Preferably, the outer surface of the head cover is in a streamline structure.
Compared with the prior art, the invention has the beneficial effects that: the throwing device is heavy in carrying load, the throwing modes are various, the six-axis design provides strong power for the unmanned aerial vehicle flight platform, the round-trip throwing operation times are reduced, the working efficiency is greatly improved, the throwing box effectively protects internal throwing materials, and the throwing of the materials is completed smoothly;
The high-definition nacelle type tripod head can provide clearer and wider visual field for operators, and because the tripod head adopts a quick-release structure, the tripod head is portable and simple to assemble and disassemble, in addition, the cover body arranged outside the unmanned aerial vehicle body adopts streamline design, wind resistance is effectively reduced, the upper wing of the unmanned aerial vehicle can be folded, occupied space is reduced after folding, and the unmanned aerial vehicle has the advantages of effectively limiting the transportation of the large unmanned aerial vehicle and being high in practicability.
Drawings
Fig. 1 is a schematic structural diagram of an aerial material hook type throwing unmanned aerial vehicle.
Fig. 2 is a schematic structural view of a throwing box in an aerial material hook type throwing unmanned aerial vehicle.
Fig. 3 is a schematic structural view of an opening and closing folding member in an aerial material hook type throwing unmanned aerial vehicle.
Fig. 4 is a schematic structural view of a hood in an aerial material hook type throwing unmanned aerial vehicle.
Fig. 5 is a schematic structural view of a shock-proof protection pad in an aerial material hook type throwing unmanned aerial vehicle.
Fig. 6 is a schematic structural view of a spring device in an aerial material hook type throwing unmanned aerial vehicle.
In the figure: 1. a head cover; 2. a main arm; 3. a secondary arm; 4. a folding member; 5. a motor; 6. a propeller; 7. a foot rest; 8. nacelle type cradle head; 9. a throwing device; 10. a battery; 11. casting the box; 12. a guide pulley; 13. a shock-proof protection pad; 1301. a spring device; 14. folding the folding piece; 15. a carbon tube connection; 16. damping cotton; 17. a tube body; 18. mounting a frame plate; 19. a hook; 20. and (5) fixing the bracket.
Detailed Description
The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
Referring to fig. 1-4, in the embodiment of the invention, an aerial material hook 19 type unmanned aerial vehicle for throwing comprises an unmanned aerial vehicle body, a hood 1 covered outside the unmanned aerial vehicle body, a nacelle type tripod head 8 and a throwing device with a damping function, wherein six groups of unmanned aerial vehicle wings with folding functions are arranged outside the hood 1 in a surrounding manner;
The bottom end of the head cover 1 is provided with foot frames 7, the foot frames 7 are arranged on two sides of the lower end of the head cover 1 and are obliquely fixed, the upper end part of the frame body is fixedly provided with a mounting frame plate 18, and the upper end of the mounting frame plate 18 is provided with a battery 10 electrically connected with the unmanned aerial vehicle main body; the head cover 1 comprises an upper shell and a lower shell, wherein the upper shell is covered at the upper end part of the unmanned aerial vehicle body, the lower shell is covered at the lower end part of the unmanned aerial vehicle body, and the upper shell and the lower shell are mutually buckled; the outer surface of the head cover 1 is of a streamline structure; the head cover 1 adopts an upper shell and a lower shell connecting and fixing mode, so that various components are effectively protected, meanwhile, the waterproof and dustproof effects on the outside are achieved, in addition, the head cover 1 is integrally in a streamline design, and wind resistance can be effectively reduced;
The throwing device comprises a throwing device 9, a throwing box 11 and a protection fixing frame for limiting the throwing box 11, wherein the throwing device 9 is arranged at the lower end part of a mounting frame plate 18, the throwing box 11 is arranged below the throwing device 9, the upper end of the throwing box is provided with a hook 19 matched with the throwing device 9, and the bottom end of the throwing box is provided with a shockproof protection pad 13;
The protection fixing frame comprises a plurality of groups of pipe bodies 17 fixed on two sides of the lower end part of the foot rest 7, the pipe bodies 17 encircle the throwing box 11 and form a rectangular frame, a guide pulley 12 matched with the throwing box 11 is arranged in the middle of each pipe body 17, folding members 14 and carbon pipe connecting members 15 are respectively arranged at two ends of each pipe body 17, one end of each pipe body 17 is movably matched with the adjacent pipe body 17 through the folding members 14, and the other end of each pipe body 17 is rotatably connected with the adjacent pipe body 17 through the carbon pipe connecting members 15;
The tube body 17 is a carbon fiber tube; under the limit of the upper pipe body 17 of the protection fixing frame, the protection fixing frame is guided by the guide pulley 12, so that the protection fixing frame can be accurately thrown to a designated throwing place, the hook 19 is arranged at the top of the throwing box 11, so that the protection fixing frame is convenient to connect with the throwing device 9, the shockproof protection pad is arranged at the bottom of the protection fixing frame, the greatest protection can be given to the throwing box 11 in a falling manner, the throwing box 11 is prevented from being broken, the damage to internal throwing materials can be avoided, and the throwing box can be recycled for multiple times;
The unmanned aerial vehicle wing comprises a main arm 2, a secondary arm 3 and a folding piece 4, one end of the main arm 2 is fixedly connected with the side wall of the hood 1, the other end of the main arm 2 is movably connected with the secondary arm 3 through the folding piece 4, a propeller 6 is arranged at one end, far away from the main arm 2, of the secondary arm 3, and a motor 5 for driving the propeller 6 to rotate is arranged at the joint of the propeller 6 and the secondary arm 3; the foldable horn of the unmanned aerial vehicle wing has the characteristics of strong structure, easy disassembly and assembly and attractive appearance, the folding piece 4 is connected with the main arm 2 and the secondary arm 3 of the unmanned aerial vehicle, and occupied space is reduced after folding, so that the limitation of the large unmanned aerial vehicle in transportation is effectively solved;
The nacelle type tripod head 8 is arranged between two adjacent unmanned aerial vehicle wings outside the hood 1 and is used for shooting high-definition pictures; the nacelle type tripod head 8 comprises a fixed bracket 20 and a tripod head main body arranged at the lower end of the fixed bracket 20, wherein the fixed bracket 20 is horizontally arranged between two adjacent unmanned aerial vehicle wings, and two ends of the fixed bracket 20 are detachably connected with the main arm 2; the cradle head main body is arranged between the two main arms through the fixed support 20, the structure is firm, meanwhile, the cradle head 8 is of a quick-dismantling structure, the disassembly and the assembly are portable and simple, in addition, the cradle head 8 is provided with a 4K high-definition camera, a high-speed processor controls the accurate operation of a motor to compensate each fine movement, so that a camera can keep a stable shooting angle, clear and stable pictures can be shot even under high-speed flight and severe vibration, and an operator can control the unmanned aerial vehicle to reach a target place to perform accurate casting;
A cross rod supporting piece for improving the placement stability of the foot rest 7 is fixed at the bottom end of the foot rest 7, and damping cotton 16 is sleeved at two ends of the cross rod supporting piece; the transverse frame supporting piece is fixed at the bottom end of the foot rest 7 and used for improving the stability of the foot rest 7 when the unmanned aerial vehicle falls to the ground, and in addition, the shock absorbing cotton 16 can effectively buffer the impact force caused by falling of the unmanned aerial vehicle, so that the stability is further enhanced;
The shockproof protection pad 13 is made of high-density sponge materials, and a spring device 1301 for buffering shock is arranged at the end part of the shockproof protection pad; the spring devices 1301 are arranged in the center and four corners of the lower end part of the shockproof protection pad 13 in a plurality of groups; the shock-proof protection pad 13 made of high-density sponge material can effectively absorb the impact from the outside, and the arrangement of the spring device 1301 is matched, so that the damage caused by the situation of facing the throwing box 11 body during absorption and landing is effectively slowed down.
The working principle of the invention is as follows: during operation, the throwing box 11 is placed below the throwing device 9, the hooks 19 are pulled to be fixed with buckling pieces on the throwing device, the pipe bodies 17 on the protection fixing frame are mutually folded to limit the throwing box 11, the motor 5 on the wing of the unmanned aerial vehicle is started to drive the propeller 6 to rotate, so that the unmanned aerial vehicle ascends, when the unmanned aerial vehicle moves to the bottom end of throwing, the folding piece 14 on the pipe bodies 17 is opened, the two adjacent pipe bodies are unfolded through the carbon pipe connecting piece 15, and finally the throwing device 9 is started under the guide of the guide pulley 12, so that the unmanned aerial vehicle is accurately thrown to a designated throwing place; the throwing device 9 is heavy in mounting load, the throwing mode is various, the six-axis design provides strong power for the unmanned aerial vehicle flight platform, the number of round-trip throwing operations is reduced, the working efficiency is greatly improved, and the throwing box 11 effectively protects internal throwing materials, so that the throwing of the materials is completed smoothly.
It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential characteristics thereof. The present embodiments are, therefore, to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Furthermore, it should be understood that although the present disclosure describes embodiments, not every embodiment is provided with a separate embodiment, and that this description is provided for clarity only, and that the disclosure is not limited to the embodiments described in detail below, and that the embodiments described in the examples may be combined as appropriate to form other embodiments that will be apparent to those skilled in the art.
Claims (5)
1. The aerial material hook type throwing unmanned aerial vehicle comprises an unmanned aerial vehicle main body and a hood (1) covered outside the unmanned aerial vehicle main body, and is characterized by further comprising a nacelle type tripod head (8) and a throwing device with a damping function, wherein six groups of unmanned aerial vehicle wings with folding functions are arranged outside the hood (1);
the nacelle type cradle head (8) is arranged between two adjacent unmanned aerial vehicle wings outside the head cover (1) and is used for shooting high-definition pictures;
the unmanned aerial vehicle comprises a head cover (1), and is characterized in that a foot rest (7) is arranged at the bottom end of the head cover (1), the foot rest (7) is arranged at two sides of the lower end of the head cover (1) and is obliquely fixed, a mounting frame plate (18) is fixed at the upper end of a frame body, and a battery (10) electrically connected with the unmanned aerial vehicle body is arranged at the upper end of the mounting frame plate (18);
The throwing device comprises a throwing device (9), a throwing box (11) and a protection fixing frame for limiting the throwing box (11), wherein the throwing device (9) is arranged at the lower end part of an installation frame plate (18), the throwing box (11) is arranged below the throwing device (9), a hook (19) matched with the throwing device (9) is arranged at the upper end of the throwing box, and a shockproof protection pad (13) is arranged at the bottom end of the throwing box;
The protection fixing frame comprises a plurality of groups of pipe bodies (17) fixed on two sides of the lower end part of the foot rest (7), the pipe bodies (17) encircle the throwing box (11) and form a rectangular frame in a surrounding mode, guide pulleys (12) matched with the throwing box (11) are arranged in the middle of the pipe bodies (17), folding pieces (14) and carbon pipe connecting pieces (15) are respectively arranged at two ends of the pipe bodies (17), one end of each pipe body (17) is in movable fit with the adjacent pipe bodies (17) through the folding pieces (14), and the other end of each pipe body (17) is in rotary connection with the adjacent pipe bodies (17) through the carbon pipe connecting pieces (15);
The nacelle type tripod head (8) comprises a fixed bracket (20) and a tripod head main body arranged at the lower end of the fixed bracket (20), wherein the fixed bracket (20) is horizontally arranged between two adjacent unmanned aerial vehicle wings, and two ends of the fixed bracket are detachably connected with the main arm (2);
A cross rod supporting piece for improving the placement stability of the foot rest (7) is fixed at the bottom end of the foot rest (7);
damping cotton (16) is sleeved at two ends of the cross rod support piece;
The shockproof protection pad (13) is made of high-density sponge materials, and a spring device (1301) playing a role in cushioning is arranged at the end part of the shockproof protection pad;
the spring devices (1301) are arranged in the center and four corners of the lower end part of the shockproof protection pad (13) in a plurality of groups.
2. An aerial material hook-type throwing unmanned aerial vehicle according to claim 1, wherein the tube body (17) is a carbon fiber tube.
3. The aerial material hook type throwing unmanned aerial vehicle according to claim 1, wherein the unmanned aerial vehicle wing comprises a main arm (2), a secondary arm (3) and a folding piece (4), one end of the main arm (2) is fixedly connected with the side wall of the hood (1), the other end of the main arm (2) is movably connected with the secondary arm (3) through the folding piece (4), one end, far away from the main arm (2), of the secondary arm (3) is provided with a propeller (6), and a motor (5) for driving the propeller (6) to rotate is arranged at the joint of the propeller (6) and the secondary arm (3).
4. The aerial material hook type throwing unmanned aerial vehicle according to claim 1, wherein the hood (1) comprises an upper shell and a lower shell, the upper shell is covered on the upper end part of the unmanned aerial vehicle body, the lower shell is covered on the lower end part of the unmanned aerial vehicle body, and the upper shell and the lower shell are mutually buckled.
5. An aerial material hook type throwing unmanned aerial vehicle according to claim 1, wherein the outer surface of the head cover (1) is of a streamline structure.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110195431.8A CN112810817B (en) | 2021-02-19 | 2021-02-19 | Aerial material hook type throwing unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110195431.8A CN112810817B (en) | 2021-02-19 | 2021-02-19 | Aerial material hook type throwing unmanned aerial vehicle |
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| Publication Number | Publication Date |
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| CN112810817A CN112810817A (en) | 2021-05-18 |
| CN112810817B true CN112810817B (en) | 2024-09-13 |
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| CN202110195431.8A Active CN112810817B (en) | 2021-02-19 | 2021-02-19 | Aerial material hook type throwing unmanned aerial vehicle |
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Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113320700B (en) * | 2021-07-01 | 2023-11-07 | 上海航谛科技有限公司 | Unmanned aerial vehicle with accurate air drop function |
| CN113879539B (en) * | 2021-11-03 | 2023-06-02 | 四川省天域航通科技有限公司 | Large unmanned aerial vehicle convenient for rescue material conveying |
| CN119503189A (en) * | 2025-01-21 | 2025-02-25 | 北京卓翼智能科技有限公司 | UAV launching device and launching system |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108313275A (en) * | 2018-03-28 | 2018-07-24 | 广西飞牛科技有限公司 | A kind of agricultural smog unmanned plane of the more rotors of multipurpose |
| CN208198834U (en) * | 2018-03-08 | 2018-12-07 | 山东奋斗信息科技有限公司 | A kind of height rescue unmanned plane |
| CN110271672A (en) * | 2019-08-01 | 2019-09-24 | 西藏新好科技有限公司 | A kind of goods and materials air transport device for animal husbandry |
| CN214356690U (en) * | 2021-02-19 | 2021-10-08 | 广西一号农服航空科技有限公司 | Aerial goods hook formula unmanned aerial vehicle of jettisoninging |
Family Cites Families (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104494821B (en) * | 2014-12-24 | 2016-05-04 | 马鞍山市靓马航空科技有限公司 | The many rotor wing unmanned aerial vehicles of a kind of multifunction emergency rescue |
| WO2016185467A1 (en) * | 2015-05-18 | 2016-11-24 | Sami Shamoon College Of Engineering (R.A) | Environmental monitoring uav system |
| WO2017041304A1 (en) * | 2015-09-11 | 2017-03-16 | SZ DJI Technology Co., Ltd. | Carrier for unmanned aerial vehicle |
| CN207274985U (en) * | 2017-08-14 | 2018-04-27 | 浙江大学华南工业技术研究院 | There is the unmanned plane that ejection is jettisoninged |
| CN107628260A (en) * | 2017-09-19 | 2018-01-26 | 中启翔宇（江苏）航空科技有限公司 | Unmanned plane multifunctional combination gondola |
| JP7052299B2 (en) * | 2017-11-07 | 2022-04-12 | 中国電力株式会社 | How to control unmanned aircraft and unmanned aircraft |
| CN207972809U (en) * | 2018-03-26 | 2018-10-16 | 重庆警察学院 | A kind of police accurate unmanned plane saving casting device |
| CN208828109U (en) * | 2018-09-18 | 2019-05-07 | 翼航东升东莞航空实业集团有限公司 | A forest fire inspection drone |
| CN210355118U (en) * | 2019-01-16 | 2020-04-21 | 哈瓦国际航空技术（深圳）有限公司 | A first aid case of jettisoninging for unmanned aerial vehicle |
| CN210000591U (en) * | 2019-05-24 | 2020-01-31 | 河北润阔农业科技有限公司 | unmanned aerial vehicle rescue goods and materials throwing device |
| CN111332472A (en) * | 2020-03-19 | 2020-06-26 | 陕西北斗金箭航空科技有限公司 | Projectile type fire extinguishing unmanned aerial vehicle |
| CN111470044A (en) * | 2020-03-31 | 2020-07-31 | 清华大学天津高端装备研究院洛阳先进制造产业研发基地 | Large capacity plant protection unmanned aerial vehicle |
-
2021
- 2021-02-19 CN CN202110195431.8A patent/CN112810817B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN208198834U (en) * | 2018-03-08 | 2018-12-07 | 山东奋斗信息科技有限公司 | A kind of height rescue unmanned plane |
| CN108313275A (en) * | 2018-03-28 | 2018-07-24 | 广西飞牛科技有限公司 | A kind of agricultural smog unmanned plane of the more rotors of multipurpose |
| CN110271672A (en) * | 2019-08-01 | 2019-09-24 | 西藏新好科技有限公司 | A kind of goods and materials air transport device for animal husbandry |
| CN214356690U (en) * | 2021-02-19 | 2021-10-08 | 广西一号农服航空科技有限公司 | Aerial goods hook formula unmanned aerial vehicle of jettisoninging |
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