CN113120248A - Air park with buffering function for taking off and landing of civil unmanned aerial vehicle - Google Patents
Air park with buffering function for taking off and landing of civil unmanned aerial vehicle Download PDFInfo
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- CN113120248A CN113120248A CN202110429523.8A CN202110429523A CN113120248A CN 113120248 A CN113120248 A CN 113120248A CN 202110429523 A CN202110429523 A CN 202110429523A CN 113120248 A CN113120248 A CN 113120248A
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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
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/007—Helicopter portable landing pads
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Abstract
The invention discloses a buffer-action apron for the take-off and landing of a civil unmanned aerial vehicle, which comprises an unmanned aerial vehicle stopping platform, a support plate, a first screw rod, a buffer plate, a limiting plate, a protective plate and a second screw rod, wherein the two ends of the side edge of the unmanned aerial vehicle stopping platform are fixedly connected with connecting plates, the lower surfaces of the connecting plates are rotatably connected with lifting rods, the buffer plates are arranged, when the unmanned aerial vehicle stops on the surfaces of the buffer plates, the buffer plates can move towards the lower ends in the stopping platform, and the first damping springs at the upper ends of telescopic rods can be extruded towards the lower ends through the position movement of the buffer plates, the damping blocks can be driven by the adjusting rods to move in fixed blocks and extrude the second damping springs towards the inner sides, the moving range of the buffer plates can be buffered through the elasticity between the first damping springs and the second damping springs, so that the buffer effect between the unmanned aerial vehicle and the stopping, avoid unmanned aerial vehicle to appear bumping bad condition when stopping to fall.
Description
Technical Field
The invention belongs to the technical field of air park, and particularly relates to an air park with a buffering function for taking off and landing of a civil unmanned aerial vehicle.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, the developed countries also actively expand the industrial application and develop the unmanned aerial vehicle technology, and the unmanned aerial vehicle is an unmanned aerial vehicle as the name suggests. Since the birth of the 20 th century, people at that time have developed the idea of pilotless aircraft because of their safety considerations. Until the 30 s of the 20 th century, fisher, uk, transformed a "queen" twin fixed wing aircraft into an unmanned drone, opening the introduction of unmanned aerial vehicles into the aviation history.
The following problems are now presented for most unmanned aerial vehicle air parks on the market at present:
1. most unmanned aerial vehicle air park on the market at present directly stagnates the unmanned aerial vehicle on the surface of the air park in the using process, but in the process of stopping the unmanned aerial vehicle, the existing air park has poor buffering effect, so that the unmanned aerial vehicle directly collides with the surface of the air park, and the unmanned aerial vehicle is easy to damage;
2. in the use process of most unmanned aerial vehicles on the market, the unmanned aerial vehicles are exposed at the upper end of the parking apron, so that the unmanned aerial vehicles are easy to collide with external objects, the unmanned aerial vehicles fall off from the surface of the parking apron, and the unmanned aerial vehicles are seriously damaged;
3. most unmanned aerial vehicle air park on the market at present generally need adjust the air park height in the use, but current regulation mode is generally through artifical manual adjusting the air park height, and this kind of mode is comparatively troublesome.
Disclosure of Invention
The invention aims to overcome the defects in the prior art and provide a buffer apron for taking off and landing of a civil unmanned aerial vehicle, so as to solve the problem of poor buffer effect in the background technology.
In order to achieve the purpose, the invention provides the following technical scheme: a civil unmanned aerial vehicle takes off and lands with parking apron that has a cushioning effect, includes parking platform, backup pad, lead screw I, buffer board, limiting plate, guard plate and lead screw II, both ends of the side edge of the parking platform are fixedly connected with the connecting plate, the lower surface of the connecting plate is rotatably connected with the lifting rod, the other end of the lifting rod is arranged in the backup pad, both sides of the interior of the parking platform are fixedly connected with the connecting guide rail, the inner side of the two connecting guide rails is slidably connected with the sliding block, the middle of the sliding block is fixedly connected with the buffer board, both sides of the interior bottom end of the parking platform are fixedly connected with the telescopic rod, the other end of the two telescopic rod is fixedly connected with the lower surface of the buffer board, the upper ends of the two telescopic rods are respectively sleeved with the damping spring I, the other end of the, two the inside hollow structure that is of fixed block, the equal sliding connection in inside both sides of fixed block has the snubber block, two fixedly connected with damping spring two in the middle of the snubber block, snubber block one side is rotated and is connected with the regulation pole, it connects in buffer board lower surface one side to adjust the rotation of the pole other end.
Preferably, the upper surface of the supporting plate is provided with a connecting groove, the inside of the supporting plate is rotatably connected with a first screw rod, and one end of the first screw rod is in transmission connection with a driving motor.
Preferably, the surfaces of two ends of the screw rod are provided with threads in opposite directions, the two ends of the screw rod are both slidably connected with moving rings, the two ends of each moving ring are provided with adjusting spiral rings, the inner side surfaces of the adjusting spiral rings are provided with threads, the upper surfaces of the adjusting spiral rings are rotatably connected with lifting rods, the other ends of the lifting rods are rotatably connected to the lower surface of the connecting plate, and rotating shafts are arranged in the middle of the lifting rods.
Preferably, the bottom end inside the supporting plate is fixedly connected with a limiting guide rail, two sides of the upper surface of the limiting guide rail are respectively connected with a limiting sliding block in a sliding mode, and the upper ends of the two limiting sliding blocks are respectively and fixedly connected to the lower end of the adjusting spiral ring.
Preferably, the protection plates are fixedly connected to two sides of the upper surface of the shutdown platform, and the driving tracks are arranged inside the protection plates.
Preferably, the two sides inside the driving crawler are provided with connecting gears, the two connecting gears and the two connecting gear ends are fixedly connected with a screw rod II, one side of each connecting gear is sleeved with a connecting belt, and one end of each connecting belt is connected with a driving motor in a transmission mode.
Preferably, both ends of one side of the protection plate are rotatably connected with a second screw rod, the other end of the second screw rod is rotatably connected to the side edge of the fixed plate, and the lower end of the fixed plate is fixedly connected to the upper surface of the shutdown platform.
Preferably, the two surfaces of the screw rod are in threaded connection with adjusting rings, moving rods are fixedly connected with the middle of the adjusting rings, connecting rods are fixedly connected to two ends of one side of each moving rod, and the other ends of the connecting rods are fixedly connected to the side edges of the limiting plates.
Preferably, the upper surface of the buffer plate is provided with a plurality of anti-skid contacts, and the anti-skid contacts are uniformly distributed on the upper surface of the buffer plate.
Preferably, the inner side surface of the limiting plate is provided with a plurality of protective strips, and the protective strips are made of sponge materials.
Compared with the prior art, the invention provides the air park with the buffering function for the taking off and landing of the civil unmanned aerial vehicle, which has the following beneficial effects:
1. according to the invention, through the arranged buffer plate, when the unmanned aerial vehicle stops on the surface of the buffer plate, the buffer plate can move towards the lower end in the shutdown platform, and through the movement of the position of the buffer plate, on one hand, the first damping spring at the upper end of the telescopic rod can be extruded towards the lower end, on the other hand, the adjusting rod can drive the damping block to move in the fixed block and extrude the second damping spring inwards;
2. according to the invention, through the arranged connecting belt, the connecting belt can be driven by the driving motor to rotate, two connecting gears in the driving crawler belt can be rotated, and through the rotation of the connecting gears, the driving crawler belt can be rotated, so that two screw rods II can be rotated together;
3. according to the invention, the first screw rod is arranged, the first screw rod can be driven to rotate by the driving motor, the surfaces of the two ends of the first screw rod are provided with threads in opposite directions, the adjusting spiral rings at the two ends of the first screw rod can keep moving in opposite directions by the rotation of the first screw rod, the moving ring in the middle of the adjusting spiral ring can slide on the surface of the first screw rod by adjusting the position of the spiral ring, the lifting rod can be extruded inwards by moving the position of the moving ring, the lifting rod can rotate around the rotating shaft in the middle, and thus the height position of the shutdown platform at the other end of the lifting rod can be adjusted, and the operation is convenient;
4. according to the invention, through the arrangement of the limiting guide rail and the limiting slide block, in the process that the adjusting spiral ring moves on the surface of the screw rod, the limiting slide block is driven to slide on the limiting guide rail through the adjusting spiral ring, the adjusting spiral ring can be prevented from rotating, so that the rotating condition of the moving ring can be prevented, the stability of the device is increased, through the arranged anti-slip contacts, and through the arrangement of the plurality of anti-slip contacts on the surface of the buffer plate, the friction force between the lower end of the unmanned aerial vehicle and the buffer plate can be increased, so that the sliding condition of the unmanned aerial vehicle on the surface of a shutdown platform can;
5. according to the invention, through the arranged protective strips, the plurality of protective strips are arranged on the inner side surface of the limiting plate, the sponge material is arranged in the protective strips, when the limiting plate fixes the position of the unmanned aerial vehicle, the protective strips can be in contact with the unmanned aerial vehicle, and the pressure effect of the limiting plate on the unmanned aerial vehicle can be reduced through the effect of soft texture of the sponge, so that the situation that the unmanned aerial vehicle is damaged due to the fact that the limiting plate is over-pressurized can be prevented.
Drawings
The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the principles of the invention without limiting the invention in which:
fig. 1 is a schematic structural diagram of a buffer-acting apron for taking off and landing of a civil unmanned aerial vehicle, which is provided by the invention;
fig. 2 is a top view of a buffer-acting apron for taking off and landing of a civil unmanned aerial vehicle, which is provided by the invention;
fig. 3 is a cross-sectional view of a parking platform in a buffer-action apron for taking off and landing of a civil unmanned aerial vehicle, which is provided by the invention;
fig. 4 is a cross-sectional view of a support plate in a buffering apron for taking off and landing of a civil unmanned aerial vehicle, which is provided by the invention;
fig. 5 is a cross-sectional view of a protective plate in a buffer-action apron for taking off and landing of a civil unmanned aerial vehicle, which is provided by the invention;
fig. 6 is a front view of a limiting plate in an apron with a buffering function for taking off and landing of a civil unmanned aerial vehicle, which is provided by the invention;
fig. 7 is an enlarged view of a buffer-acting apron for taking off and landing of a civil unmanned aerial vehicle, which is provided by the invention, in fig. 2;
fig. 8 is an enlarged view of B in fig. 3 of the buffering apron for taking off and landing of the civil unmanned aerial vehicle provided by the invention;
in the figure: 1. a shutdown platform; 2. a support plate; 3. a lifting rod; 4. a connecting plate; 5. a first screw rod; 6. (ii) modulating a spiro ring; 7. a moving ring; 8. limiting a guide rail; 9. a limiting slide block; 10. a buffer plate; 11. an anti-slip contact; 12. a limiting plate; 13. a protection plate; 14. a fixing plate; 15. a second screw rod; 16. an adjusting ring; 17. a travel bar; 18. a connecting rod; 19. a telescopic rod; 20. a first damping spring; 21. adjusting a rod; 22. a fixed block; 23. a damper block; 24. a second damping spring; 25. connecting the guide rails; 26. a slider; 27. driving the caterpillar; 28. a connecting belt; 29. a connecting gear; 30. a protective strip; 31. and connecting the grooves.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-8, the present invention provides the following technical solutions: a buffer parking apron for civil unmanned aerial vehicle lifting comprises a parking platform 1, a supporting plate 2, a first screw rod 5, a buffer plate 10, a limiting plate 12, a protecting plate 13 and a second screw rod 15, wherein both ends of the side edge of the parking platform 1 are fixedly connected with connecting plates 4, the lower surface of each connecting plate 4 is rotatably connected with a lifting rod 3, the other end of each lifting rod 3 is arranged inside the corresponding supporting plate 2, both sides inside the parking platform 1 are fixedly connected with connecting guide rails 25, the inner sides of the two connecting guide rails 25 are respectively and slidably connected with sliding blocks 26, the middle of each sliding block 26 is fixedly connected with the buffer plate 10, both sides of the bottom end inside the parking platform 1 are respectively and fixedly connected with telescopic rods 19, the other ends of the two telescopic rods 19 are fixedly connected to the lower surface of the buffer plate 10, the upper ends of the two telescopic rods 19 are respectively sleeved with a first damping spring 20, the interior of each of the two fixing blocks 22 is of a hollow structure, two sides of the interior of each fixing block 22 are slidably connected with the corresponding shock absorption block 23, a second shock absorption spring 24 is fixedly connected between the middle of each shock absorption block 23, one side of each shock absorption block 23 is rotatably connected with an adjusting rod 21, the other end of each adjusting rod 21 is rotatably connected to one side of the lower surface of the corresponding buffer plate 10, when the unmanned aerial vehicle stops on the surface of the corresponding buffer plate 10, the buffer plates 10 can move towards the lower ends in the shutdown platform 1, and the first shock absorption springs 20 at the upper ends of the telescopic rods 19 can be extruded towards the lower ends through the movement of the buffer plates 10, the adjusting rods 21 can drive the shock absorption blocks 23 to move in the fixing blocks 22 and extrude the second shock absorption springs 24 towards the inner sides, the moving range of the buffer plates 10 can be buffered through the elastic, avoid unmanned aerial vehicle to appear bumping bad condition when stopping to fall.
In the invention, preferably, the upper surface of the support plate 2 is provided with a connecting groove 31, the support plate 2 is internally and rotatably connected with a first screw rod 5, one end of the first screw rod 5 is in transmission connection with a driving motor, and the first screw rod 5 can be rotated through a cloud stack of the driving motor.
In the invention, preferably, the surfaces of two ends of a first screw rod 5 are provided with threads in opposite directions, two ends of the first screw rod 5 are both slidably connected with moving rings 7, two ends of each moving ring 7 are both provided with adjusting spiral rings 6, the inner side surface of each adjusting spiral ring 6 is provided with threads, the upper surface of each adjusting spiral ring 6 is rotatably connected with a lifting rod 3, the other end of each lifting rod 3 is rotatably connected with the lower surface of a connecting plate 4, a rotating shaft is arranged in the middle of each lifting rod 3, the first screw rod 5 is driven to rotate by a driving motor, the surfaces of two ends of the first screw rod 5 are provided with threads in opposite directions, the adjusting spiral rings 6 at two ends of the first screw rod 5 can keep moving in opposite directions by the rotation of the first screw rod 5, the moving ring 7 in the middle of the adjusting spiral rings 6 can slide on the surface of the first screw rod 5 by the movement of the, thereby can adjust the 3 other ends of lifter and halt the high position of platform 1, it is comparatively convenient.
In the invention, preferably, the bottom end inside the supporting plate 2 is fixedly connected with a limiting guide rail 8, two sides of the upper surface of the limiting guide rail 8 are both slidably connected with limiting sliders 9, the upper ends of the two limiting sliders 9 are both fixedly connected to the lower end of the adjusting spiral ring 6, and when the adjusting spiral ring 6 moves on the surface of the screw rod I5, the limiting sliders 9 are driven by the adjusting spiral ring 6 to slide on the limiting guide rail 8, so that the adjusting spiral ring 6 can be prevented from rotating, the movable ring 7 is prevented from rotating, and the stability of the device is improved.
In the invention, preferably, the protection plates 13 are fixedly connected to both sides of the upper surface of the shutdown platform 1, the driving crawler 27 is arranged in each protection plate 13, and the two second screw rods 15 can rotate together by the driving crawler 27.
In the invention, preferably, the two sides inside the driving crawler 27 are both provided with the connecting gears 29, one ends of the two connecting gears 29 and one end of the connecting gear 29 are both fixedly connected with the second lead screw 15, one side of the connecting gear 29 is sleeved with the connecting belt 28, one end of the connecting belt 28 is in transmission connection with the driving motor, the connecting belt 28 is driven to rotate by the driving motor, the two connecting gears 29 inside the driving crawler 27 can be rotated, the driving crawler 27 can be rotated by the rotation of the connecting gears 29, and therefore the two lead screws 15 can be rotated together.
In the invention, preferably, two ends of one side of the protection plate 13 are both rotatably connected with the second screw rod 15, the other end of the second screw rod 15 is rotatably connected to the side edge of the fixing plate 14, and the lower end of the fixing plate 14 is fixedly connected to the upper surface of the shutdown platform 1.
According to the invention, preferably, the adjusting ring 16 is in threaded connection with the surface of the second screw rod 15, the moving rod 17 is fixedly connected to the middle of the adjusting ring 16, the connecting rods 18 are fixedly connected to two ends of one side of the moving rod 17, the other end of each connecting rod 18 is fixedly connected to the side edge of the limiting plate 12, the adjusting ring 16 on the surface of the second screw rod 15 can be moved through rotation of the second screw rod 15, the moving rod 17 can drive the limiting plate 12 to move through position movement of the adjusting ring 16, the unmanned aerial vehicle can be extruded inwards through position movement of the limiting plate 12, so that the unmanned aerial vehicle can be fixed at the upper end of the shutdown platform 1, and the situation.
In the invention, preferably, the upper surface of the buffer plate 10 is provided with a plurality of anti-skid contacts 11, and the anti-skid contacts 11 are uniformly distributed on the upper surface of the buffer plate 10, so that the friction force between the lower end of the unmanned aerial vehicle and the buffer plate 10 can be increased, and the situation that the unmanned aerial vehicle slides on the surface of the shutdown platform 1 can be effectively prevented.
In the invention, preferably, the plurality of protective strips 30 are arranged on the inner side surface of the limiting plate 12, the protective strips 30 are made of sponge materials, when the limiting plate 12 fixes the position of the unmanned aerial vehicle, the protective strips 30 can be in contact with the unmanned aerial vehicle, and the pressure effect of the limiting plate 12 on the unmanned aerial vehicle can be reduced through the soft effect of the sponge material, so that the situation that the unmanned aerial vehicle is damaged due to the fact that the limiting plate 12 is over-stressed can be prevented.
The working principle and the using process of the invention are as follows: when the device is used, the device is placed at a designated position, the height of the shutdown platform 1 is adjusted, the screw rod I5 is driven to rotate by the driving motor, threads in opposite directions are arranged on the surfaces of the two ends of the screw rod I5, the adjusting screw rings 6 at the two ends of the screw rod I5 can keep moving in opposite directions by the rotation of the screw rod I5, the moving ring 7 in the middle of the adjusting screw ring 6 can slide on the surface of the screw rod I5 by the movement of the position of the moving ring 7, the lifting rod 3 can be extruded inwards by the moving ring 7, the lifting rod 3 can rotate around the rotating shaft in the middle, so that the height position of the shutdown platform 1 at the other end of the lifting rod 3 can be adjusted, the device is convenient and fast, when the adjusting screw ring 6 moves on the surface of the screw rod I5, the limiting slide block 9 is driven by the adjusting screw ring 6, thereby preventing the movable ring 7 from rotating, increasing the stability of the device, when the unmanned aerial vehicle stops on the surface of the buffer plate 10, the buffer plate 10 can move towards the lower end in the shutdown platform 1, on one hand, the lower end can extrude the first damping spring 20 at the upper end of the telescopic rod 19 through the movement of the buffer plate 10, on the other hand, the adjusting rod 21 can drive the damping block 23 to move in the fixed block 22 and extrude the second damping spring 24 inwards, the movement range of the buffer plate 10 can be buffered through the elastic force between the first damping spring 20 and the second damping spring 24, thereby increasing the buffering effect between the unmanned aerial vehicle and the shutdown platform 1, avoiding the situation that the unmanned aerial vehicle is damaged when the unmanned aerial vehicle stops, the surface of the buffer plate 10 is provided with a plurality of anti-skid contacts 11, increasing the friction force between the lower end of the unmanned aerial vehicle and the buffer plate 10, thereby effectively preventing the unmanned aerial vehicle from sliding on the surface of the shutdown, the connecting belt 28 is driven to rotate by the driving motor, the two connecting gears 29 in the driving crawler 27 can be rotated, the driving crawler 27 can be rotated by the rotation of the connecting gears 29, so that the two second lead screws 15 can be rotated together, the adjusting rings 16 on the surfaces of the second lead screws 15 can be moved by the rotation of the second lead screws 15, the moving rods 17 can drive the limiting plates 12 to move by the movement of the adjusting rings 16, the unmanned aerial vehicle can be extruded inwards by the movement of the limiting plates 12, so that the unmanned aerial vehicle can be fixed at the upper end of the shutdown platform 1, the unmanned aerial vehicle is prevented from falling from the upper surface of the shutdown platform 1, the inner side surfaces of the limiting plates 12 are provided with a plurality of protective strips 30, the protective strips 30 are made of sponge materials, when the limiting plates 12 fix the position of the unmanned aerial vehicle, the protective strips 30 can be in contact with the unmanned aerial vehicle, can reduce the pressure effect that limiting plate 12 caused to unmanned aerial vehicle to can prevent to appear that pressure is too big between limiting plate 12 and the unmanned aerial vehicle and cause the condition that unmanned aerial vehicle appears damaging.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (10)
1. The utility model provides a civil unmanned aerial vehicle takes off and land with air park that has cushioning effect, includes shutdown platform (1), backup pad (2), lead screw (5), buffer board (10), limiting plate (12), guard plate (13) and lead screw two (15), its characterized in that: the two ends of the side edge of the shutdown platform (1) are fixedly connected with connecting plates (4), the lower surface of each connecting plate (4) is rotatably connected with a lifting rod (3), the other end of each lifting rod (3) is arranged inside a supporting plate (2), two sides inside the shutdown platform (1) are fixedly connected with connecting guide rails (25), the inner sides of the two connecting guide rails (25) are respectively and slidably connected with a sliding block (26), the middle of each sliding block (26) is fixedly connected with a buffer plate (10), two sides of the bottom end inside the shutdown platform (1) are respectively and fixedly connected with telescopic rods (19), the other ends of the two telescopic rods (19) are fixedly connected with the lower surface of the buffer plate (10), the upper ends of the two telescopic rods (19) are respectively sleeved with a damping spring I (20), the other ends of the damping spring I (20) are fixedly connected with the lower surface of the buffer plate (10), and two sides, two fixed block (22) are inside to be hollow structure, the equal sliding connection in both sides of fixed block (22) has snubber block (23), two fixedly connected with damping spring two (24) in the middle of snubber block (23), snubber block (23) one side is rotated and is connected with regulation pole (21), it rotates to connect in buffer board (10) lower surface one side to adjust pole (21) other end.
2. The air park with the buffering function for taking off and landing of civil unmanned aerial vehicles according to claim 1, is characterized in that: the connecting groove (31) has been seted up to backup pad (2) upper surface, backup pad (2) inside rotation is connected with lead screw (5), the transmission of lead screw (5) one end is connected with driving motor.
3. The air park with the buffering function for taking off and landing of civil unmanned aerial vehicles according to claim 1, is characterized in that: the utility model discloses a lead screw, including lead screw one (5) both ends surface, the equal sliding connection in lead screw one (5) both ends has shift ring (7), two shift ring (7) both ends all are provided with adjusts spiro (6), it is provided with the screw thread to adjust spiro (6) inboard surface, it is connected with lifter (3) to adjust spiro (6) upper surface rotation, lifter (3) other end rotates and connects at connecting plate (4) lower surface, be provided with the pivot in the middle of lifter (3).
4. The air park with the buffering function for taking off and landing of civil unmanned aerial vehicles according to claim 1, is characterized in that: the bottom fixedly connected with limit guide rail (8) in backup pad (2), the equal sliding connection in limit guide rail (8) upper surface both sides has limit slider (9), two equal fixed connection in limit slider (9) upper end is adjusting spiro (6) lower extreme position.
5. The air park with the buffering function for taking off and landing of civil unmanned aerial vehicles according to claim 1, is characterized in that: shut down platform (1) upper surface both sides equal fixedly connected with guard plate (13), guard plate (13) inside is provided with drive track (27).
6. The air park with the buffering function for taking off and landing of civil unmanned aerial vehicles according to claim 5, is characterized in that: the inside both sides of drive track (27) all are provided with connecting gear (29), two with the equal fixedly connected with lead screw two (15) of connecting gear (29) one end, connecting band (28) have been cup jointed to connecting gear (29) one side, connecting band (28) one end transmission is connected with driving motor.
7. The air park with the buffering function for taking off and landing of civil unmanned aerial vehicles according to claim 1, is characterized in that: the two ends of one side of the protection plate (13) are rotatably connected with a second screw rod (15), the other end of the second screw rod (15) is rotatably connected to the side of the fixing plate (14), and the lower end of the fixing plate (14) is fixedly connected to the upper surface of the shutdown platform (1).
8. The air park with the buffering function for taking off and landing of civil unmanned aerial vehicles according to claim 1, is characterized in that: the utility model discloses a lead screw two (15) surface threaded connection has adjustable ring (16), fixedly connected with carriage release lever (17) in the middle of adjustable ring (16), the equal fixedly connected with connecting rod (18) in carriage release lever (17) one side both ends, connecting rod (18) other end fixed connection is at limiting plate (12) side.
9. The air park with the buffering function for taking off and landing of civil unmanned aerial vehicles according to claim 1, is characterized in that: the anti-skid device is characterized in that a plurality of anti-skid contacts (11) are arranged on the upper surface of the buffer plate (10), and the anti-skid contacts (11) are uniformly distributed on the upper surface of the buffer plate (10).
10. The air park with the buffering function for taking off and landing of civil unmanned aerial vehicles according to claim 1, is characterized in that: the inner side surface of the limiting plate (12) is provided with a plurality of protective strips (30), and the protective strips (30) are made of sponge materials.
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| Application Number | Priority Date | Filing Date | Title |
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| CN202110429523.8A CN113120248A (en) | 2021-04-21 | 2021-04-21 | Air park with buffering function for taking off and landing of civil unmanned aerial vehicle |
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| CN202110429523.8A CN113120248A (en) | 2021-04-21 | 2021-04-21 | Air park with buffering function for taking off and landing of civil unmanned aerial vehicle |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113665830A (en) * | 2021-09-27 | 2021-11-19 | 南通大学 | Small-sized unmanned aerial vehicle parking device |
| CN113699903A (en) * | 2021-07-28 | 2021-11-26 | 广西电网有限责任公司电力科学研究院 | Unmanned aerial vehicle shutdown platform for instant intelligent disaster investigation of power transmission line |
| CN113859567A (en) * | 2021-11-15 | 2021-12-31 | 北京卓翼智能科技有限公司 | Intelligent automatic take-off and landing platform for unmanned aerial vehicle |
| CN114248944A (en) * | 2022-01-13 | 2022-03-29 | 福建中量智汇科技有限公司 | Iris centering device of unmanned aerial vehicle parking apron |
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| CN113859567B (en) * | 2021-11-15 | 2024-05-28 | 北京卓翼智能科技有限公司 | Unmanned aerial vehicle intelligent automatic take-off and landing platform |
| CN114248944A (en) * | 2022-01-13 | 2022-03-29 | 福建中量智汇科技有限公司 | Iris centering device of unmanned aerial vehicle parking apron |
| CN114248944B (en) * | 2022-01-13 | 2024-02-27 | 福建中量智汇科技有限公司 | Iris centering device of unmanned aerial vehicle apron |
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