CN111942266B - Unmanned aerial vehicle platform of taking off and land - Google Patents
Unmanned aerial vehicle platform of taking off and land Download PDFInfo
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- CN111942266B CN111942266B CN202010951348.4A CN202010951348A CN111942266B CN 111942266 B CN111942266 B CN 111942266B CN 202010951348 A CN202010951348 A CN 202010951348A CN 111942266 B CN111942266 B CN 111942266B
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- aerial vehicle
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- claw
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- 210000000078 claw Anatomy 0.000 claims abstract description 78
- 230000007246 mechanism Effects 0.000 claims abstract description 35
- 230000009471 action Effects 0.000 claims abstract description 8
- 230000007306 turnover Effects 0.000 claims description 11
- 241000276425 Xiphophorus maculatus Species 0.000 claims description 3
- 238000005452 bending Methods 0.000 claims description 3
- 230000000694 effects Effects 0.000 abstract description 5
- 238000013459 approach Methods 0.000 abstract description 4
- 238000000034 method Methods 0.000 description 10
- 230000008569 process Effects 0.000 description 10
- 238000011084 recovery Methods 0.000 description 6
- 230000003028 elevating effect Effects 0.000 description 3
- 238000011835 investigation Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000004064 recycling Methods 0.000 description 1
- 238000012876 topography Methods 0.000 description 1
- 230000032258 transport Effects 0.000 description 1
Classifications
-
- 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
- B60—VEHICLES IN GENERAL
- B60P—VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
- B60P7/00—Securing or covering of load on vehicles
- B60P7/06—Securing of load
- B60P7/08—Securing to the vehicle floor or sides
- B60P7/0892—Securing to the vehicle floor or sides by preventing lateral movement of the load, e.g. using stop blocks
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- Engineering & Computer Science (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Health & Medical Sciences (AREA)
- Public Health (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention belongs to the technical field of multifunctional robots, and particularly relates to an unmanned aerial vehicle taking-off and landing platform, which comprises a movable unmanned platform, wherein a cabin with an open top is arranged on the unmanned platform, and an openable or closable cover plate is arranged at the open part of the cabin; the apron of the cabin is in an upper state close to the hatch or in a lower state at the bilge under the action of the lifting mechanism; still be equipped with the stop gear that keeps between two parties to unmanned aerial vehicle in the cabin, stop gear includes the claw that keeps between two parties that carries out spacingly to unmanned aerial vehicle foot rest, the claw that pushes between two parties sets up two in the cabin symmetry, and two the claw that keeps between two centers are in the clamping state that mutually approaches or the open condition that keeps away from under actuating mechanism's effect.
Description
Technical Field
The invention belongs to the technical field of multifunctional robots, and particularly relates to an unmanned aerial vehicle take-off and landing platform.
Background
When the investigation task or the rescue and relief work of topography are complicated, personnel can not participate in directly for the safety, related investigation is carried out through unmanned aerial vehicle at present to obtain effective information for personnel, but because the task that needs to be detected is more, a plurality of unmanned aerial vehicle equipment is needed to cooperate, and all the plurality of unmanned aerial vehicle equipment needs personnel to operate to realize accurate starting release, unmanned investigation detection, recovery and closing, etc., and unmanned aerial vehicle is the most commonly used equipment in unmanned aerial vehicle equipment, but unmanned aerial vehicle takes off and land very inconveniently in the complex environment, has brought very big puzzlement for the user.
Disclosure of Invention
The invention aims to provide an unmanned aerial vehicle take-off and landing platform, which can realize take-off and landing of an unmanned aerial vehicle without manual direct contact, ensures the safety of the unmanned aerial vehicle in the take-off and landing process, and expands the application range of the unmanned aerial vehicle.
In order to achieve the above purpose, the present invention adopts the following technical scheme: an unmanned aerial vehicle taking-off and landing platform comprises a movable unmanned platform, wherein a cabin with an open top is arranged on the unmanned platform, and an openable or closable cover plate is arranged at the open part of the cabin; the apron of the cabin is in an upper state close to the hatch or in a lower state at the bilge under the action of the lifting mechanism; still be equipped with the stop gear that keeps between two parties to unmanned aerial vehicle in the cabin, stop gear includes the claw that keeps between two parties that carries out spacingly to unmanned aerial vehicle foot rest, the claw that pushes between two parties sets up two in the cabin symmetry, and two the claw that keeps between two centers are in the clamping state that mutually approaches or the open condition that keeps away from under actuating mechanism's effect.
Preferably, the centering pushing claw is in a 'herringbone' shape formed by intersecting two claw arms, and a U-shaped groove for inserting and adapting the unmanned aerial vehicle foot rest is formed in the inner side of the intersecting part of the two claw arms.
Preferably, the centering pushing claw is hinged with the surface of the parking apron at the intersection of the two claw arms through a hinge shaft; the driving mechanism comprises a driving motor with an output shaft connected with the hinge shaft, when the hinge shaft is driven to rotate by the output shaft of the driving motor, the two centering pushing claws rotate along with the hinge shaft to be in a clamping state close to each other or an opening state far away from each other, and the rotating surface of the centering pushing claws is perpendicular to the plate surface of the parking apron.
Preferably, the driving motor and the hinge shaft are arranged on the lower plate surface of the parking apron; the centering pushing claw is connected with the hinge shaft at the intersection of the two claw arms through a connecting rod, and a bending structure is arranged between the connecting rod and the centering pushing claw; a strip-shaped groove for avoiding the connecting rod is arranged in the plate surface of the parking apron, and the notch directions of the two strip-shaped grooves deviate from each other.
Preferably, the lifting mechanism comprises a screw rod, wherein two ends of the screw rod are fixed on the inner wall of the cabin through mounting seats, the length direction of the screw rod is vertical, a first sliding block sliding along the length direction of the screw rod is arranged on the screw rod, and the first sliding block is fixedly connected with the parking apron.
Preferably, the lifting mechanisms are arranged in two groups and are respectively positioned at opposite angles of the rectangular platy parking apron, wherein a first sliding block in the lifting mechanisms is connected to the side edge of the parking apron; the lower plate surface of the other two corners of the parking apron is provided with a supporting block, the inner wall of the engine room corresponding to the supporting block is provided with a guide rail with the length consistent with the length direction of the screw rod, and the supporting block moves on the guide rail along the length direction of the guide rail.
Preferably, the cover plate is hinged with the edge of the opening of the cabin; and a cover plate turnover mechanism is arranged between the cover plate and the engine room.
Preferably, the cover plate turnover mechanism comprises a turnover driving rod, wherein one end of the turnover driving rod is hinged with the side surface of the cabin, and the other end of the turnover driving rod is in sliding connection with the side edge of the cover plate; a cover plate guide groove for sliding the end part of the overturning driving rod is formed in the side edge of the hinged end of the cover plate, and the groove length direction of the cover plate guide groove is consistent with the length direction of the side edge of the cover plate; the hinged end of the overturning driving rod is provided with a power source for driving the overturning driving rod to hinge and rotate.
Preferably, the end parts of the overhanging ends of the claw arms are provided with cushion blocks, and when the two centering pushing claws are in a clamping state adjacent to each other, the cushion blocks are pressed against the plate surface of the parking apron.
Preferably, a sensor for positioning the unmanned aerial vehicle is arranged on the inner wall of the cabin; and a charging unit for charging the unmanned aerial vehicle is further arranged in the engine room.
The invention has the beneficial effects that:
1) Two in stop gear pushes away the claw and moves to the clamping state that mutually approaches from the open state that keeps away from under actuating mechanism's effect, in the middle part position with unmanned aerial vehicle propelling movement to the apron in the motion process, carry out spacing fixedly to unmanned aerial vehicle when pushing away the claw in the middle simultaneously is in the clamping state, guarantee unmanned aerial vehicle's stability on the apron, elevating system drives the apron and moves to the lower position state of bilge department from the upper position state that is close to the hatch place, personnel control apron is closed, accomplish unmanned aerial vehicle and retrieve work.
2) When the two centering pushing claws move from the opening state far away to the clamping state close to each other, the inner side walls of the two centering pushing claws are abutted to the vertical foot frames and push the vertical foot frames to move, and the vertical foot frames drive the unmanned aerial vehicle to gradually move to the centering position. When unmanned aerial vehicle is in the intermediate position on the air park, the vertical foot rest is located the U type inslot of two claw arm crossing departments, prevents the horizontal removal of foot rest, and when the claw arm of "people" style of calligraphy was in the clamping state that is close to each other, two claw arms were pressed and are leaned on unmanned aerial vehicle's horizontal foot rest's top, realize spacing to unmanned aerial vehicle upper and lower direction, guaranteed unmanned aerial vehicle and parked the stability on the air park.
3) And two first sliding blocks and two supporting blocks in the lifting mechanism respectively support four corners of the parking apron, so that the stability of the parking apron in the lifting process is ensured, and the parking apron is free from offset and inclination in lifting.
Drawings
FIG. 1 is a schematic view of a structure of the invention in a state that a cover plate is opened and a middle pushing claw is clamped;
FIG. 2 is a schematic view of the structure of the invention in the state that the cover plate is opened and the middle pushing claw is opened;
FIG. 3 is a schematic view of the internal structure of the present invention;
FIG. 4 is a side view of the cover plate of the present invention in a closed position;
FIG. 5 is a schematic cross-sectional view taken at B-B of FIG. 4;
Fig. 6 is a side view of the invention in an open state of the cover plate.
The actual correspondence between each label and the component name of the invention is as follows:
unmanned platform-10; -a nacelle-20;
A cover plate-21; cover plate guide slots-211;
Tarmac-22; a drive motor-221; a hinge shaft-222; a connecting rod-223;
-a bar-shaped slot 224;
A centering pushing claw-23; claw arm-231; u-shaped groove-232; cushion block-233;
A screw rod-24; a first slider 241;
A guide rail-25; a supporting block-251;
Flip drive rod-26.
Detailed Description
For ease of understanding, the specific structure and manner of operation of the invention will be further described below with reference to the accompanying drawings.
An unmanned aerial vehicle taking-off and landing platform comprises a movable unmanned platform 10, wherein a cabin 20 with an open top is arranged on the unmanned platform 10, and an openable or closable cover plate 21 is arranged at the open part of the cabin 20; the apron 22 of the cabin 20 is in an upper state close to a hatch or in a lower state at the bilge under the action of an elevating mechanism; still be equipped with the stop gear that keeps between two parties to unmanned aerial vehicle in cabin 20, stop gear includes the claw 23 that keeps between two parties that carries out spacingly to unmanned aerial vehicle foot rest, the claw 23 that keeps between two parties sets up two in cabin 20 symmetry, and two claw 23 that keep between two are in the clamping state that is close to each other or the open condition that keeps away from under actuating mechanism's effect. Unmanned aerial vehicle places in unmanned aerial vehicle's cabin 20 of platform 10, and unmanned aerial vehicle platform 10 transports unmanned aerial vehicle to appointed place, and this unmanned aerial vehicle take-off and land platform mainly includes unmanned aerial vehicle release and unmanned aerial vehicle recovery two working processes, unmanned aerial vehicle release working process: the staff controls the open state of the cover plate 21, the apron 22 of the unmanned aerial vehicle ascends from the lower state at the bilge to the upper state at the position close to the hatch under the action of the lifting mechanism, and the unmanned aerial vehicle starts to fly out from the hatch of the cabin 20 to finish the release process. The unmanned aerial vehicle recycling working process comprises the following steps: when unmanned aerial vehicle accomplishes the task and flies back to the hatch department of cabin 20, apron 21 is in the open state and waits for unmanned aerial vehicle to fly back in the cabin this moment, unmanned aerial vehicle parks on the apron 22 that is in the host computer state, two pushing claws 23 placed in the middle among the stop gear move to the clamping state that is close to each other from the open state that keeps away from under actuating mechanism's effect, the middle part position of apron 22 is pushed unmanned aerial vehicle to in the motion process, carry out spacing fixed to unmanned aerial vehicle when pushing claw 23 placed in the middle of while is in the clamping state, guarantee unmanned aerial vehicle's stability on apron 22, elevating system drives apron 22 and moves to the lower state of cabin bottom department from the host computer state that is close to the hatch department, personnel control apron 21 is closed, accomplish unmanned aerial vehicle and retrieve the work.
Because unmanned aerial vehicle is when parking, the foot rest of its lower part supports whole fuselage, and the foot rest includes vertical foot rest and horizontal foot rest, and horizontal foot rest is horizontal on the air park 22, and the vertical foot rest is connected between horizontal foot rest and unmanned aerial vehicle. Limiting the foot rest of unmanned aerial vehicle in the middle is actually performed in the middle of limiting the foot rest of unmanned aerial vehicle, so the centering pushing claw 23 is designed into a structure which is convenient for limiting the foot rest, the centering pushing claw 23 is in a 'herringbone' shape formed by intersecting two claw arms 231, and the inner side of the intersecting part of the two claw arms 231 is provided with a U-shaped groove 232 for the insertion of the unmanned aerial vehicle foot rest. When the two centering pushing claws 23 move from the open state far away to the clamping state close to each other, the inner side walls of the claw arms 231 are abutted against the vertical horse and push the vertical horse to move, and the vertical horse drives the unmanned aerial vehicle to gradually move to the centering position. When the drone is in a centered position on the tarmac 22, the vertical leg is located in the U-shaped slot 232 where the two claw arms 231 meet, preventing the leg from moving horizontally. In addition, when the claw arms 231 in the shape of the Chinese character 'lambdoidal' are in the mutually adjacent clamping state, the two claw arms 231 are pressed above the horizontal foot stand of the unmanned aerial vehicle, so that the limiting of the unmanned aerial vehicle in the vertical direction is realized, and the stability of the unmanned aerial vehicle parked on the apron 22 is ensured.
The centering pushing claw 23 is hinged with the plate surface of the apron 22 at the intersection of the two claw arms 231 through a hinge shaft 222; the driving mechanism comprises a driving motor 221 with an output shaft connected with a hinge shaft 222, when the output shaft of the driving motor 221 drives the hinge shaft 222 to rotate, the two centering pushing claws 23 rotate along with the hinge shaft 222 to be in a clamping state close to each other or an opening state far away from each other, and a rotating surface of the centering pushing claws 23 is perpendicular to the plate surface of the apron 22.
The driving motor 221 and the hinge shaft 222 are both arranged on the lower plate surface of the apron 22; the centering pushing claw 23 is connected with the hinge shaft 222 at the intersection of the two claw arms 231 through a connecting rod 223, and a bending structure is arranged between the connecting rod 223 and the centering pushing claw 23; the strip-shaped grooves 224 for avoiding the connecting rods 223 are arranged in the plate surface of the apron 22, and the notch directions of the two strip-shaped grooves 224 are opposite.
When the centering pushing claw 23 needs to move from the opening state far away from each other to the clamping state close to each other, the driving motor starts 221 to work, the output shaft of the driving motor drives the hinge shaft 222 to rotate so as to drive the connecting rod 223 to rotate, the centering pushing claw 23 reversely moves in the bar-shaped groove 224 from the opening state far away from each other to the clamping state close to each other along the groove length direction, the connecting rod 223 is in the vertical state, and the centering pushing claw 23 is in the horizontal state.
The lifting mechanism comprises a screw rod 24 with two ends fixed on the inner wall of the cabin 20 through mounting seats, the length direction of the screw rod 24 is vertical, a first sliding block 241 sliding along the length direction of the screw rod 24 is arranged on the screw rod 24, and the first sliding block 241 is fixedly connected with the parking apron 22.
The lifting mechanisms are arranged in two groups and are respectively positioned at opposite angles of the rectangular platy apron 22, wherein a first sliding block 241 in the lifting mechanism is connected to the side edge of the apron 22; the lower plate surfaces at the other two corners of the apron 22 are provided with supporting blocks 251, the inner wall of the cabin 20 corresponding to the supporting blocks 251 is provided with guide rails 25 with the length consistent with the length direction of the screw rods 24, and the supporting blocks 251 move on the guide rails 25 along the length direction.
The two first sliding blocks 241 and the two supporting blocks 251 in the lifting mechanism respectively support the four corners of the apron 22, so that the stability of the apron 22 in the lifting process is ensured, and the apron 22 is free from offset and inclination in lifting. It should be noted that the screws 24 at the two opposite corners are consistent during movement.
The cover plate 21 is hinged with the edge of the opening of the cabin 20; a cover plate turnover mechanism is arranged between the cover plate 21 and the engine room 20. The cover plate turnover mechanism comprises a turnover driving rod 26, one end of which is hinged with the side surface of the cabin 20, and the other end of which is in sliding connection with the side edge of the cover plate 21; a cover plate guide groove 211 for sliding the end part of the overturning driving rod 26 is formed in the side edge of the hinged end of the cover plate 21, and the groove length direction of the cover plate guide groove 211 is consistent with the length direction of the side edge of the cover plate 21; the hinged end of the turning driving rod 26 is provided with a power source for driving the turning driving rod to hinge and rotate.
The overhanging end portion of the claw arm 231 is provided with a pad 233, and when the two centering claws 23 are in a clamping state adjacent to each other, the pad 233 is pressed against the plate surface of the apron 22. The pad 233 is generally made of a material having a cushioning property, such as a rubber material, and when the two centering pushers 23 are in a clamping state adjacent to each other, the pad 233 plays a good cushioning role to avoid the direct collision of the claw arms 231 with the apron 22.
A sensor for positioning the unmanned aerial vehicle is arranged on the inner wall of the cabin 20; a charging unit for charging the unmanned aerial vehicle is further arranged in the cabin 20.
The release and recovery process of the unmanned aerial vehicle is specifically described below:
the release process comprises the following steps: when the unmanned aerial vehicle needs to execute a task, the unmanned aerial vehicle is loaded on the unmanned aerial vehicle platform 10 to reach a preset take-off position, an operator needs to control the cover plate 21 to open at a distance at the moment, the overturning driving rod 26 is hinged to rotate under the action of a power source, the end part of the overturning driving rod 26 slides in the cover plate guide groove 211 until the end part of the overturning driving rod slides to abut against the groove end of the cover plate guide groove 211, the cover plate 21 is opened to the maximum position at the moment, the overturning driving rod 26 stops rotating, and the unmanned aerial vehicle enters a waiting flying state.
After the cover plate 21 is opened, the lifting mechanism pushes the apron 22 from a low-level state to a high-level state at the hatch of the cabin 20, a driving motor 221 positioned at the bottom of the apron 22 starts to work, under the action of a connecting rod 223, the centering pushing claw 23 rotates to be opened, a U-shaped groove 232 positioned between two claw arms 23 is separated from a vertical stand of the unmanned aerial vehicle, and the claw arms 23 are changed from a state of being pressed against the horizontal stand of the unmanned aerial vehicle to a state of being far away from the horizontal stand. The drone is started and flies out of the nacelle 20 to perform the task.
The recovery process comprises the following steps: after the unmanned aerial vehicle finishes the task, unmanned aerial vehicle platform 10 waits for unmanned aerial vehicle to fly back at the preset position, the apron 21 of cabin 20 department is opened and is in the recovery stage this moment, when unmanned aerial vehicle flies into in the cabin 20, horizontal foot rest is placed on the apron 22, the concrete position of unmanned aerial vehicle is detected to the sensor on the inner wall of cabin 20 this moment, two centering pushing claws 23 by the open state motion that keeps away from each other to the clamping state that mutually approaches, when the claw arm 231 of "people" form moves, its inside wall leans on with unmanned aerial vehicle's on and promotes the vertical foot rest and removes, the vertical foot rest drives unmanned aerial vehicle and gradually moves to the position of centering of apron 22, when unmanned aerial vehicle is in the position of centering on apron 22, the vertical foot rest is located the U type groove 232 of two claw arm 231 crossing department, prevent the horizontal removal of foot rest. In addition, when the claw arms 231 in the shape of the Chinese character 'lambdoidal' are in the mutually adjacent clamping state, the two claw arms 231 are pressed above the horizontal foot stand of the unmanned aerial vehicle, so that the limiting of the unmanned aerial vehicle in the vertical direction is realized, and the stability of the unmanned aerial vehicle parked on the apron 22 is ensured.
After the unmanned aerial vehicle stops stably on the air park 22, the lifting mechanism is started to drive the air park 22 to move from a high-position state to a low-position state, and the cover plate 21 is rotated to be closed, so that recovery of the unmanned aerial vehicle is completed.
Claims (8)
1. An unmanned aerial vehicle platform of taking off and land, its characterized in that: the unmanned aerial vehicle comprises a movable unmanned aerial vehicle platform (10), wherein a cabin (20) with an open top is arranged on the unmanned aerial vehicle platform (10), and an openable or closable cover plate (21) is arranged at the open position of the cabin (20); the apron (22) of the cabin (20) is in an upper state close to a hatch or in a lower state at the bilge under the action of a lifting mechanism; the unmanned aerial vehicle cabin is characterized in that a limiting mechanism for limiting centering of the unmanned aerial vehicle is further arranged in the cabin (20), the limiting mechanism comprises centering pushing claws (23) for limiting a tripod of the unmanned aerial vehicle, two centering pushing claws (23) are symmetrically arranged in the cabin (20), and the two centering pushing claws (23) are in a clamping state or a far-away opening state which are adjacent to each other under the action of a driving mechanism;
the centering pushing claw (23) is in a herringbone shape formed by intersecting two claw arms (231), and a U-shaped groove (232) for inserting and adapting a unmanned aerial vehicle foot rest is formed in the inner side of the intersecting part of the two claw arms (231);
The centering pushing claw (23) is hinged with the plate surface of the parking apron (22) at the intersection of the two claw arms (231) through a hinge shaft (222); the driving mechanism comprises a driving motor (221) with an output shaft connected with a hinge shaft (222), when the hinge shaft (222) is driven to rotate by the output shaft of the driving motor (221), the two centering pushing claws (23) rotate along with the hinge shaft (222) to be in a clamping state close to each other or an opening state far away from each other, and the rotating surface of the centering pushing claws (23) is perpendicular to the plate surface of the parking apron (22);
And a charging unit for charging the unmanned aerial vehicle is further arranged in the engine room (20).
2. The unmanned aerial vehicle landing platform of claim 1, wherein: the driving motor (221) and the hinge shaft (222) are arranged on the lower plate surface of the parking apron (22); the centering pushing claw (23) is connected with the hinge shaft (222) through a connecting rod (223) at the intersection of the two claw arms (231), and a bending structure is arranged between the connecting rod (223) and the centering pushing claw (23); a strip-shaped groove (224) for avoiding a connecting rod (223) is arranged in the plate surface of the parking apron (22), and the notch directions of the two strip-shaped grooves (224) are opposite.
3. The unmanned aerial vehicle landing platform of claim 1, wherein: the lifting mechanism comprises a screw rod (24) with two ends fixed on the inner wall of the engine room (20) through mounting seats, the length direction of the screw rod (24) is vertical, a first sliding block (241) sliding along the length direction of the screw rod (24) is arranged on the screw rod, and the first sliding block (241) is fixedly connected with the parking apron (22).
4. A unmanned aerial vehicle landing platform according to claim 3, wherein: the lifting mechanisms are arranged in two groups and are respectively positioned at opposite angles of the rectangular platy parking apron (22), and a first sliding block (241) in the lifting mechanisms is connected to the side edge of the parking apron (22); the lower plate surfaces at the other two corners of the parking apron (22) are provided with supporting blocks (251), the inner wall of the cabin (20) corresponding to the supporting blocks (251) is provided with guide rails (25) with the length consistent with the length direction of the screw rods (24), and the supporting blocks (251) move on the guide rails (25) along the length direction of the guide rails.
5. The unmanned aerial vehicle landing platform of claim 1, wherein: the cover plate (21) is hinged with the edge of the opening of the cabin (20); a cover plate turnover mechanism is arranged between the cover plate (21) and the engine room (20).
6. The unmanned aerial vehicle landing platform of claim 5, wherein: the cover plate turnover mechanism comprises a turnover driving rod (26) with one end hinged with the side surface of the cabin (20) and the other end in sliding connection with the side edge of the cover plate (21); a cover plate guide groove (211) for sliding the end part of the overturning driving rod (26) is formed in the side edge of the hinged end of the cover plate (21), and the groove length direction of the cover plate guide groove (211) is consistent with the length direction of the side edge of the cover plate (21); the hinged end of the overturning driving rod (26) is provided with a power source for driving the overturning driving rod to hinge and rotate.
7. The unmanned aerial vehicle landing platform of claim 1, wherein: the end parts of the overhanging ends of the claw arms (231) are provided with cushion blocks (233), and when the two centering pushing claws (23) are in a clamping state adjacent to each other, the cushion blocks (233) are pressed against the plate surface of the parking apron (22).
8. The unmanned aerial vehicle landing platform of claim 1, wherein: and a sensor for positioning the unmanned aerial vehicle is arranged on the inner wall of the cabin (20).
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| Application Number | Priority Date | Filing Date | Title |
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| CN202010951348.4A CN111942266B (en) | 2020-09-11 | 2020-09-11 | Unmanned aerial vehicle platform of taking off and land |
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| CN113352976B (en) * | 2021-07-26 | 2024-07-23 | 成都时代星光科技有限公司 | Vehicle-mounted intelligent unmanned aerial vehicle airport |
| CN113697103A (en) * | 2021-08-03 | 2021-11-26 | 浙江大华技术股份有限公司 | Reconnaissance robot |
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| CN212709136U (en) * | 2020-09-11 | 2021-03-16 | 中国人民解放军陆军炮兵防空兵学院 | Unmanned aerial vehicle take-off and landing platform |
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| CN207466991U (en) * | 2017-10-30 | 2018-06-08 | 深圳市大疆创新科技有限公司 | Unmanned machine positioning device and airplane parking area |
| CN108008737A (en) * | 2017-11-29 | 2018-05-08 | 安徽玄同工业设计有限公司 | A kind of release of vehicle-mounted unmanned aerial vehicle and retracting device |
| IL256112A (en) * | 2017-12-05 | 2018-01-31 | Yefim Kereth | Capture and storage unit for airborne drone |
| KR20190092964A (en) * | 2018-01-31 | 2019-08-08 | 한서대학교 산학협력단 | Simplified horizon controlling landing field apparatus |
| CN111483385B (en) * | 2019-01-28 | 2023-08-29 | 中光电智能机器人股份有限公司 | Monitoring system and control method thereof |
| CN110001988A (en) * | 2019-04-03 | 2019-07-12 | 南京利剑无人机科技有限公司 | A kind of vehicle-mounted multi-rotor unmanned aerial vehicle landing platform |
| CN210316752U (en) * | 2019-06-27 | 2020-04-14 | 上海复亚智能科技有限公司 | Unmanned aerial vehicle multimachine hangar |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN212709136U (en) * | 2020-09-11 | 2021-03-16 | 中国人民解放军陆军炮兵防空兵学院 | Unmanned aerial vehicle take-off and landing platform |
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