CN110884677A - A winding and unwinding devices for mooring unmanned aerial vehicle - Google Patents
A winding and unwinding devices for mooring unmanned aerial vehicle Download PDFInfo
- Publication number
- CN110884677A CN110884677A CN201911258629.5A CN201911258629A CN110884677A CN 110884677 A CN110884677 A CN 110884677A CN 201911258629 A CN201911258629 A CN 201911258629A CN 110884677 A CN110884677 A CN 110884677A
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- cabin body
- unmanned aerial
- aerial vehicle
- mooring
- bottom plate
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F3/00—Ground installations specially adapted for captive aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60P—VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
- B60P3/00—Vehicles adapted to transport, to carry or to comprise special loads or objects
- B60P3/06—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles
- B60P3/11—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles for carrying aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/22—Ground or aircraft-carrier-deck installations installed for handling aircraft
- B64F1/225—Towing trucks
Abstract
The invention discloses a retraction device for a mooring unmanned aerial vehicle, which comprises a trailer, wherein a generator, a power box and a rotating shaft box are arranged on the trailer, a cabin body which is used for storing the mooring unmanned aerial vehicle and is matched with the mooring unmanned aerial vehicle is arranged on the trailer, the cabin body comprises a bottom plate, a cabin body arranged on the bottom plate and a baffle plate capable of opening and closing the cabin body, the cabin body is connected with the bottom plate in a sliding manner, the baffle plate is hinged with the bottom plate, and the retraction device also comprises a power mechanism which is arranged on the bottom plate and can drive the cabin body to slide relative to the bottom plate; the structure is simple, blades do not need to be disassembled and assembled when the tethered unmanned aerial vehicle takes off or recovers, and the preparation time is short; the mooring unmanned aerial vehicle can be towed to a place where work is needed along with the trailer, and can fly along with the trailer synchronously in the flying process, so that the universality is greatly improved.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to a winding and unwinding device for mooring an unmanned aerial vehicle.
Background
The unmanned aerial vehicle is used as equipment of a load video acquisition and transmission system, and has wide application in occasions such as movie shooting, news interview, field evidence collection, air patrol and the like. The existing unmanned aerial vehicle generally has the following two modes, one mode is an unmanned aerial vehicle with a power battery, and the power battery is used for providing power to drive a motor to rotate a propeller to generate power for flying; the other type is heavy unmanned aerial vehicle, is mooring unmanned aerial vehicle promptly, and its power supply is on ground, connects unmanned aerial vehicle through the power supply cable and provides power for unmanned aerial vehicle. The unmanned aerial vehicle corresponding to the former mode is limited by factors such as load, volume, flight time and the like, and cannot meet the requirement of long-time operation; mooring unmanned aerial vehicle system is by many rotor unmanned aerial vehicle, mooring cable, ground take off and land the platform and constitute, mooring unmanned aerial vehicle uses the long-time stagnation of ground power supply to hang and stop, simultaneously, data such as the high definition video that airborne equipment gathered can pass back to ground through the built-in optic fibre of mooring cable, have aerial long-time operation, the big advantage of data transmission bandwidth, but entire system stand alone type installation also can on-vehicle installation to can automatic synchronization follow the vehicle and remove.
At present, the mode of receiving and releasing of mooring unmanned aerial vehicle mainly has two kinds: one type is a ground lifting type, when a flight task is executed, a tethered unmanned aerial vehicle and ground equipment need to be dismounted from a transport vehicle, when the tethered unmanned aerial vehicle is recovered, the tethered unmanned aerial vehicle and the ground equipment need to be re-loaded, various equipment cannot be placed and reliably fixed according to a uniform fixed position, the operation is extremely complicated, the operation is limited by environmental factors, and the equipment cannot move; the other type of the retractable platform of the mooring unmanned aerial vehicle modified by the pick-up truck is adopted, the ground equipment is installed in the rear carriage of the modified pick-up truck, and the mooring unmanned aerial vehicle is installed on a lifting mechanism in the rear carriage of the pick-up truck; when the tethered unmanned aerial vehicle executes a flight task, the top of the rear carriage of the pick-up truck needs to be opened, the tethered unmanned aerial vehicle is jacked to the top of the rear carriage of the pick-up truck by using a lifting mechanism, a retraction platform is combined, and then the tethered unmanned aerial vehicle can be operated to take off; the retractable platform is positioned at the top of the rear carriage of the modified pick-up truck, the height of the retractable platform exceeds more than 1.7 meters, when the tethered unmanned aerial vehicle is released or recovered, personnel need to climb to the retractable platform on the roof to mount or dismount the blades of the unmanned aerial vehicle so as to take off or recover the tethered unmanned aerial vehicle, and the operation is dangerous and extremely inconvenient; the lifting mechanism has a complex structure and low use reliability.
In the prior art, chinese patent CN205952334U proposes a retraction system for a tethered unmanned aerial vehicle, which includes a retraction cabin for accommodating the tethered unmanned aerial vehicle, and the retraction cabin includes: the lifting platform is arranged in the inner space of the retraction cabin and is used for the mooring unmanned aerial vehicle to stay on; a slidable hatch; which is arranged at the top of the retractable compartment for opening and closing the inner space of the retractable compartment; cables for communication and power transmission; and the cable winding and unwinding equipment is used for winding and unwinding cables, is arranged in the inner space of the winding and unwinding cabin and is connected with the mooring unmanned aerial vehicle through cables. However, this system need set up the elevating platform, need will tie the unmanned aerial vehicle through operating system and lift out and fly again during the use, and the structure is comparatively complicated, complex operation, and it is higher to set up the height, is subject to environmental factor, and can not remove.
Disclosure of Invention
The invention provides a retraction device for a mooring unmanned aerial vehicle, aiming at solving the technical problems that the existing mooring unmanned mechanism is complex, complicated to operate and incapable of moving.
The technical scheme adopted by the invention is as follows: the retraction device for the tethered unmanned aerial vehicle comprises a trailer, wherein a generator, a power supply box and a rotating shaft box are arranged on the trailer, and a sealed cabin for storing the tethered unmanned aerial vehicle is arranged on the trailer; the cabin comprises a bottom plate, a cabin body above the bottom plate and a baffle capable of opening and closing the cabin body, the cabin body is connected with the bottom plate in a sliding mode, and the baffle is hinged to the bottom plate. The generator provides electric power for unmanned aerial vehicle, and the power supply box converts the electric power of generator into different voltage electric current and provides with electrical apparatus, and the pivot case is used for receiving and releasing of unmanned aerial vehicle cable. When the mooring unmanned aerial vehicle is in a non-working state, the mooring unmanned aerial vehicle is positioned on the bottom plate in the cabin body, and the cabin body provides a safe, stable, dust-free and rain-proof protection environment for the mooring unmanned aerial vehicle; when mooring unmanned aerial vehicle is in operating condition, open the baffle, the drive cabin body slides for the bottom plate, until mooring unmanned aerial vehicle exposes completely, can carry out mooring unmanned aerial vehicle's taking off. The invention provides a bearing platform with proper height and no potential safety hazard for the tethered unmanned aerial vehicle, and maintenance personnel can maintain the tethered unmanned aerial vehicle by standing on the ground; the structure is simple, blades do not need to be disassembled and assembled when the tethered unmanned aerial vehicle takes off or recovers, and the preparation time is short; the mooring unmanned aerial vehicle can be towed to a place where work is needed along with the trailer, and can fly along with the trailer synchronously in the flying process, so that the universality is greatly improved.
Further, the base plate is provided with a guide rail, the base plate is provided with a roller mechanism matched with the guide rail, the cabin body is arranged on the guide rail, and the cabin body can synchronously slide relative to the base plate along with the guide rail. The cabin body is arranged on the guide rail, the cabin body can move relative to the base plate along with the guide rail, and then the unmanned aerial vehicle is conveniently moored to open or close, and the roller mechanism reduces the friction force between the guide rail and the base plate, so that the guide rail can slide more smoothly relative to the base plate, and the structure is simple and the operation is convenient.
Further, the device also comprises a power mechanism for driving the guide rail to slide relative to the bottom plate; the power mechanism comprises a motor, a first synchronous belt wheel, a first synchronous belt, a second synchronous belt wheel, a rotating shaft, a third synchronous belt wheel, a second synchronous belt and a synchronous belt idler wheel which are sequentially connected. The motor and the rotating shaft are arranged below the bottom plate, the motor is connected with the first synchronous belt wheel and drives the second synchronous belt wheel to rotate through the first synchronous belt, the second synchronous belt wheel drives the rotating shaft to rotate, the rotating shaft drives the third synchronous belt wheel to rotate, the third synchronous belt wheel drives the synchronous belt idler wheel to rotate through the second synchronous belt, the second synchronous belt is connected with the guide rail, and then the guide rail is driven to move relative to the bottom plate.
Further, the roller mechanism comprises a transverse roller and a longitudinal roller. The transverse roller and the longitudinal roller enable the bottom plate and the guide rail to be attached more tightly in the transverse direction and the longitudinal direction, so that the bottom plate and the guide rail are connected more stably, and the derailment phenomenon can be avoided.
Further, the cabin body comprises a first cabin body, a second cabin body and a third cabin body which are connected in sequence, the second cabin body is arranged on the inner side of the first cabin body, the first cabin body is fixedly connected with the guide rail, and the second cabin body and the third cabin body are connected with the guide rail in a sliding manner. The guide rail is provided with a sliding chute matched with the second cabin body and the third cabin body, and the second cabin body and the third cabin body can slide on the guide rail, so that the length of the cabin body is further shortened. Compare in integral cabin body, move to the position that exposes the unmanned aerial vehicle completely at the cabin body from the position that shields the unmanned aerial vehicle of mooring, make the stroke distance of cabin body shorter through the slidable cabin body, reduced corresponding power take off and part quantity, area occupied is littleer, the structure is simpler, improved winding and unwinding devices's overall stability simultaneously.
Further, a locking mechanism is further arranged on the trailer. The cabin body and the guide rails can be fixed.
Further, the locking mechanism comprises a lock catch arranged on the guide rail and a clasp arranged at a position corresponding to the cabin. Simple structure and convenient operation.
Further, the bottom plate is provided with an opening and a cover plate for opening and closing the opening. The trailer is internally provided with a power box, a rotating shaft box and other components, and the opening can facilitate the maintenance of the components arranged in the trailer.
Further, a temperature adjusting mechanism is arranged in the trailer. The temperature adjusting mechanism provides a proper temperature suitable for working for heating components such as a power box, a rotating shaft box and the like in the trailer, so that the folding and unfolding device is suitable for different working environments and working conditions, the components are in a good working environment, and the service life of the components is prolonged.
Further, the cabin body and the baffle are both of a hollow structure made of steel plates, and the hollow structure is filled with flame-retardant rigid polyurethane foam plastics. The cabin body and the baffle that the steel sheet was made have guaranteed the cabin body and the good intensity and the rigidity of baffle, and fire resistance rigid polyurethane foam guarantees the environmental weatherability of the cabin body and baffle, thermal-insulated, thermal insulation performance, and then provides a safe, stable, thermal-insulated protective environment for mooring unmanned aerial vehicle.
The invention has the beneficial effects that:
1. the invention provides a bearing platform with proper height and no potential safety hazard for the tethered unmanned aerial vehicle, and maintenance personnel can maintain the tethered unmanned aerial vehicle by standing on the ground; the structure is simple, blades do not need to be disassembled and assembled when the tethered unmanned aerial vehicle takes off or recovers, and the preparation time is short; the mooring unmanned aerial vehicle can be towed to a place where work is needed along with the trailer, and can fly along with the trailer synchronously in the flying process, so that the universality is greatly improved.
2. The transverse roller and the longitudinal roller ensure that the bottom plate and the guide rail are attached more tightly in the transverse direction and the longitudinal direction, so that the bottom plate and the guide rail are connected more stably, and the derailment phenomenon is completely avoided.
3. Compared with an integral cabin body, the cabin body moves from a position for shielding the captive unmanned aerial vehicle to a position for completely exposing the captive unmanned aerial vehicle, the stroke distance of the cabin body is shorter by retracting the cabin body, the corresponding power output and the number of components are reduced, the occupied area is smaller, the structure is simpler, and the overall stability of the retraction device is improved.
4. The cabin body and the baffle plate made of the steel plate ensure good strength and rigidity of the cabin body and the baffle plate, and the fire-retardant rigid polyurethane foam plastic ensures environmental weather resistance, heat insulation and heat preservation performance of the cabin body and the baffle plate, so that a safe, stable and heat-insulated protection environment is provided for the mooring unmanned aerial vehicle.
Drawings
Fig. 1 is a tethered drone retrieval state diagram.
Fig. 2 is a tethered drone deployment state diagram.
Fig. 3 is a schematic structural view of the enclosure of fig. 2.
Fig. 4 is a top view of fig. 3. (omitting capsule body)
Fig. 5 is a right side view of fig. 3.
Labeled as:
4. a locking mechanism; 5. mooring the unmanned aerial vehicle;
11. a trailer frame; 12. towing the compartment; 13. a trailer tire; 14. an auxiliary support wheel; 15. a traction mechanism; 16. a generator; 17. a power supply box; 18. a pivot housing; 19. a temperature adjustment mechanism; 21. a base plate; 23. a baffle plate;
31. a motor; 32. a first timing pulley; 33. a first synchronization belt; 34. a second timing pulley; 35. a rotating shaft; 36. a third synchronous pulley; 37. a second synchronous belt; 38. a synchronous belt idler pulley;
211. a guide rail; 212. a transverse roller; 213. a longitudinal roller; 214. an opening; 215. a cover plate;
221. a first cabin; 222. a second cabin; 223. a third cabin;
Detailed Description
The invention is further described below with reference to the accompanying drawings.
The first embodiment is as follows:
as shown in fig. 1 to 5, the retraction device for a tethered unmanned aerial vehicle of the present invention includes a trailer, the trailer includes a trailer frame 11, a trailer box 12, trailer tires 13, auxiliary support wheels 14, and a traction mechanism 15, the trailer is provided with a generator 16, a power box 17, and a pivot box 18, the trailer is further provided with a sealed cabin for storing the tethered unmanned aerial vehicle 5, the cabin includes a bottom plate 21, a cabin body disposed on the bottom plate 21, and a baffle 23 capable of opening and closing the cabin body, the cabin body is slidably connected to the bottom plate 21, the baffle 23 is hinged to the bottom plate 21, and the retraction device further includes a power mechanism disposed on the bottom plate 21 and capable of driving the cabin body to slide relative to the bottom plate 21; the power mechanism comprises a motor 31, a first synchronous belt pulley 32, a first synchronous belt 33, a second synchronous belt pulley 34, a rotating shaft 35, a third synchronous belt pulley 36, a second synchronous belt 37 and a synchronous belt idler pulley 38 which are connected in sequence; the bottom plate 21 is provided with a guide rail 211, the bottom plate 21 is provided with a roller mechanism matched with the guide rail 211, the cabin body is arranged on the guide rail 211, and the cabin body can synchronously slide relative to the bottom plate 21 along with the guide rail 211; the trailer is also provided with a locking mechanism 4; the locking mechanism 4 comprises a lock catch arranged on the guide rail 211 and a clasp arranged at a position corresponding to the cabin; a cover plate 215 provided with an opening 214 and an openable/closable opening 214 on the bottom plate 21; a temperature adjusting mechanism 19 is arranged in the trailer, and the temperature adjusting mechanism 19 is an air conditioner.
The trailer adopts a single-shaft structure; the trailer frame 11 is formed by assembling and welding rectangular steel pipes, so that the rigidity in all directions is ensured; the trailer carriage 12 adopts a framework type sandwich plate structure, is bent and welded by steel plates, and flame-retardant rigid polyurethane foam plastic is filled between the inner skin and the outer skin to ensure good strength, rigidity, environmental weather resistance, heat insulation and heat preservation performance of the trailer carriage; the suspension system of the trailer is independently suspended by adopting a torsion bar type, so that the transportation smoothness of the whole vehicle is improved; an electromagnetic braking system is arranged on the trailer, so that the rapid braking and the high response speed are ensured; the trailer is provided with a hand braking system, so that the trailer can be safely braked in any parking state; the auxiliary trailer supporting wheels 14 can meet the parking requirements of urban roads, dirt roads, gobi roads and grasslands; the trailer tire 13 is a 6.50R16LT12 tire, the rated load of a single tire of the tire is 1060kg, the diameter is 750mm, and the requirements of height and load are met.
The generator is responsible for supplying power to the whole system, the power box converts 220V alternating current generated by the generator into 1000V direct current for the use of the tethered unmanned aerial vehicle, and the rotating shaft box is responsible for winding and unwinding 1000V direct current cables for supplying power to the tethered unmanned aerial vehicle, so that the tethered unmanned aerial vehicle is ensured to be smoothly lifted and landed; the air conditioner reduces the temperature in the trailer box to a proper working temperature, and the normal work of the power box and the rotating shaft box is ensured.
The working principle is as follows: as shown in fig. 1, the tethered unmanned aerial vehicle is in a non-working state, the unmanned aerial vehicle is mounted on a bottom plate in a cabin body, and the cabin body provides a safe, stable, dust-free and rain-proof protective environment for the tethered unmanned aerial vehicle; can move mooring unmanned aerial vehicle to the workplace that needs take off through pulling the trailer. When the tethered drone arrives at the work site, as shown in fig. 2, the tethered drone is in working condition. At first, open the baffle, drive the cabin body through power unit and slide for the bottom plate, until mooring unmanned aerial vehicle exposes completely, can start mooring unmanned aerial vehicle. The invention provides a bearing platform with proper height and no potential safety hazard for the tethered unmanned aerial vehicle, and maintenance personnel can maintain the tethered unmanned aerial vehicle by standing on the ground; the structure is simple, blades do not need to be disassembled and assembled when the tethered unmanned aerial vehicle takes off or recovers, and the preparation time is short; the mooring unmanned aerial vehicle can be towed to a place where work is needed along with the trailer, and can fly along with the trailer synchronously in the flying process, so that the universality is greatly improved.
Example two:
the present embodiment is a further improvement on the first embodiment, as shown in fig. 1, fig. 2, fig. 3 and fig. 5, the cabin includes a first cabin 221, a second cabin 222 and a third cabin 223 connected in sequence, the second cabin 222 is disposed inside the first cabin 221, the first cabin 221 is fixedly connected to the guide rail 211, and the second cabin 222 and the third cabin 223 are slidably connected to the guide rail 211.
The working principle is as follows: before the captive unmanned aerial vehicle is started, the second cabin body and the third cabin body are driven to move on the guide rail, the second cabin body is folded into the first cabin body, and the third cabin body and the first cabin body are arranged side by side. Compare in integral cabin body, move to the position that exposes the unmanned aerial vehicle completely at the cabin body from the position that shields the unmanned aerial vehicle of mooring, make the stroke distance of cabin body shorter through the cabin body of can drawing in, reduced corresponding power take off and part quantity, area is littleer, the structure is simpler, improved winding and unwinding devices's overall stability simultaneously.
Example three:
this embodiment is a further improvement on the first embodiment, and as shown in fig. 1 to 4, the roller mechanism includes a transverse roller 212 and a longitudinal roller 213.
The working principle is as follows: when the guide rail moves relative to the bottom plate, both the transverse roller and the longitudinal roller on the bottom plate can slide with the guide rail. The transverse roller and the longitudinal roller enable the bottom plate and the guide rail to be attached more tightly in the transverse direction and the longitudinal direction, so that the bottom plate and the guide rail are connected more stably, and the derailment phenomenon is completely avoided.
Example four:
in this embodiment, a further improvement is made on the basis of the first embodiment, as shown in fig. 1 to 4, the cabin and the baffle 23 are both hollow structures made of steel plates, and the hollow structures are filled with flame-retardant rigid polyurethane foam.
The working principle is as follows: the cabin body and the baffle that the steel sheet was made have guaranteed the cabin body and the good intensity and the rigidity of baffle, and fire resistance rigid polyurethane foam guarantees the environmental weatherability of the cabin body and baffle, thermal-insulated, thermal insulation performance, and then provides a safe, stable, thermal-insulated protective environment for mooring unmanned aerial vehicle.
The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention, and various modifications and changes may be made by those skilled in the art. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (10)
1. A winding and unwinding devices for mooring unmanned aerial vehicle, including the trailer, be provided with generator (16), power supply box (17) and pivot case (18) on the trailer, its characterized in that: a sealed cabin for storing the captive unmanned aerial vehicle (5) is arranged on the trailer;
the cabin comprises a bottom plate (21), a cabin body above the bottom plate (21) and a baffle (23) capable of opening and closing the cabin body, the cabin body is connected with the bottom plate (21) in a sliding mode, and the baffle (23) is hinged to the bottom plate (21).
2. The stowing and releasing device for mooring a drone of claim 1, characterized by: guide rails (211) are arranged on two sides of the base plate (21), roller mechanisms matched with the guide rails (211) are arranged on the base plate (21), the cabin body is arranged on the guide rails (211), and the cabin body can synchronously slide relative to the base plate (21) along with the guide rails (211).
3. The stowing and releasing device for mooring a drone of claim 2, characterized by: the device also comprises a power mechanism for driving the guide rail (211) to slide relative to the bottom plate (21);
the power mechanism comprises a motor (31), a first synchronous belt wheel (32), a first synchronous belt (33), a second synchronous belt wheel (34), a rotating shaft (35), a third synchronous belt wheel (36), a second synchronous belt (37) and a synchronous belt idler wheel (38) which are sequentially connected, the motor (31) and the synchronous belt idler wheel (38) are arranged on the bottom plate (21), and the second synchronous belt (37) is connected with the guide rail.
4. The stowing and releasing device for mooring a drone of claim 2, characterized by: the roller mechanism comprises a transverse roller (212) and a longitudinal roller (213).
5. The stowing and releasing device for mooring a drone of claim 2, characterized by: the cabin body comprises a first cabin body (221), a second cabin body (222) and a third cabin body (223) which are sequentially connected, the second cabin body (222) is arranged on the inner side of the first cabin body (221), the first cabin body (221) is fixedly connected with a guide rail (211), and the second cabin body (222) and the third cabin body (223) are slidably connected with the guide rail (211).
6. The stowing and releasing device for mooring a drone of claim 1, characterized by: and the trailer is also provided with a locking mechanism (4).
7. The stowing and releasing device for mooring a drone of claim 6, characterized by: the locking mechanism (4) comprises a lock catch arranged on the guide rail (211) and a clasp arranged at the corresponding position of the cabin body.
8. The stowing and releasing device for mooring a drone of claim 1, characterized by: the bottom plate (21) is provided with an opening (214) and a cover plate (215) capable of opening and closing the opening (214).
9. The stowing and releasing device for mooring a drone of claim 1, characterized by: a temperature adjusting mechanism (19) is arranged in the trailer.
10. The stowing and releasing device for mooring a drone of claim 1, characterized by: the cabin body and the baffle (23) are both of a hollow structure made of steel plates, and the hollow structure is filled with flame-retardant rigid polyurethane foam plastics.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911258629.5A CN110884677A (en) | 2019-12-10 | 2019-12-10 | A winding and unwinding devices for mooring unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911258629.5A CN110884677A (en) | 2019-12-10 | 2019-12-10 | A winding and unwinding devices for mooring unmanned aerial vehicle |
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| Publication Number | Publication Date |
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| CN110884677A true CN110884677A (en) | 2020-03-17 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201911258629.5A Pending CN110884677A (en) | 2019-12-10 | 2019-12-10 | A winding and unwinding devices for mooring unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115195573A (en) * | 2022-08-23 | 2022-10-18 | 江苏捷诚车载电子信息工程有限公司 | Unmanned aerial vehicle comprehensive guarantee transport vechicle |
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| KR102189033B1 (en) * | 2020-01-28 | 2020-12-10 | 주식회사 숨비 | Drone hangar for pickup truck with take-off and landing guide function and, drone operating system including the same |
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|---|---|---|---|---|
| CN2611202Y (en) * | 2003-04-11 | 2004-04-14 | 中国人民解放军军事交通学院 | Expandable square cabin |
| US20180001812A1 (en) * | 2016-06-30 | 2018-01-04 | Michael Jerome Friemel | Rotorcraft Transport Trailer |
| US20190322206A1 (en) * | 2018-04-18 | 2019-10-24 | Frédéric Lamy | Road transport apparatus for helicopter |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN115195573A (en) * | 2022-08-23 | 2022-10-18 | 江苏捷诚车载电子信息工程有限公司 | Unmanned aerial vehicle comprehensive guarantee transport vechicle |
| CN115195573B (en) * | 2022-08-23 | 2024-03-19 | 江苏捷诚车载电子信息工程有限公司 | Unmanned aerial vehicle comprehensive guarantee transport vehicle |
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