Communication unmanned aerial vehicle take-off and landing platform

Abstract

The utility model discloses a communication unmanned aerial vehicle take-off and landing platform, and relates to the field of communication unmanned aerial vehicles, the communication unmanned aerial vehicle take-off and landing platform comprises a parking plate, a storage cover, a supporting seat and a storage box, the bottom of the parking plate is provided with a buffer structure, the buffer structure comprises a baffle ring and a damping seat, the baffle ring is fixedly installed on the upper portion of the damping seat, and the storage cover is fixedly installed on the baffle ring. Eight damping springs are fixedly installed on the upper portion of the damping seat and in the baffle ring, two transverse shafts are symmetrically and fixedly installed on the outer portion of the damping seat, and square blocks are fixedly installed at one ends of the two transverse shafts. According to the communication unmanned aerial vehicle take-off and landing platform, the buffer structure and the storage structure are arranged, the buffer structure can effectively release impact force brought by forced landing of an unmanned aerial vehicle, the situation that the unmanned aerial vehicle is damaged due to counter-acting force is avoided, and the storage structure is used for storing the unmanned aerial vehicle by controlling lifting and closing of the platform. And the unmanned aerial vehicle take-off and landing platform is more convenient and lighter.

Description

Technical Field

[0001] The utility model relates to the field of unmanned aerial vehicle take-off and landing platforms, in particular to the field of communication unmanned aerial vehicles. Background Art

[0002] As a practical platform specially built for communication drones, it is often used for drone takeoff and docking. By flexibly constructing drone take-off and landing points, the use of drones becomes more convenient and safer.

[0003] Although traditional communication drone take-off and landing platforms provide technologies for drone take-off and forced landing, they do not have a buffering function in the event of an forced landing, which can easily cause the drone to rebound or its parts to be damaged due to the impact force during forced landing. They also do not have a storage function and cannot be stored when not in use, such as during carrying, transportation or storage, resulting in inconvenience in carrying and transportation, and the storage process is also prone to occupying too much space.

[0004] Therefore, a communication UAV take-off and landing platform is designed to solve the technical problems in the background technology. Utility Model Content

[0005] The main purpose of the utility model is to provide a communication UAV take-off and landing platform, which can effectively solve the technical problems in the background technology.

[0006] In order to achieve the above purpose, the technical solution adopted by the utility model is:

[0007] A communication UAV take-off and landing platform comprises a parking plate, a storage cover, a support seat and a storage box. A buffer structure is arranged at the bottom of the parking plate, and the buffer structure comprises a retaining ring and a shock absorbing seat. The retaining ring is fixedly mounted on the upper part of the shock absorbing seat, and eight shock absorbing springs are fixedly mounted at the upper part of the shock absorbing seat and the inner position of the retaining ring. Two horizontal axes are symmetrically fixedly mounted on the outside of the shock absorbing seat, and four square blocks are fixedly mounted on one end of each of the two horizontal axes.

[0008] As a further solution of the utility model, a convex strip is glued and connected to the inner wall of the retaining ring near the position of the shutdown plate, and the outer part of the shutdown plate is adaptively matched with the convex strip.

[0009] As a further solution of the utility model, four limit plates are symmetrically installed on the inner wall of the support seat, and a limit rod and a rack are respectively fixedly installed at the same side position of the four limit plates.

[0010] As a further solution of the utility model, a storage structure is provided on the outside of the horizontal axis, and the storage structure includes a storage cover, which is rotatably connected to the horizontal axis, and two gears are fixedly installed at symmetrical positions at both ends of the bottom of the storage cover, and a support rod is movably installed on the side of the two gears away from the storage cover, a square groove is provided at one end of the support rod, and a support spring is fixedly installed inside the square groove.

[0011] As a further solution of the utility model, the gear is meshedly connected with the rack, the other end of the support spring is fixedly connected to the square block, and the square block is adaptively matched with the square groove opened at one end of the support lever.

[0012] As a further solution of the utility model, support grooves are provided at symmetrical positions on the outside of the support seat, a baffle is fixedly installed on the inner wall of the support groove, and two sliding shafts are symmetrically fixedly installed on the outside of the support seat at positions perpendicular to the two support grooves, a storage lever is fixedly installed at one end of the two sliding shafts, a circular groove is provided at one end of the storage lever, and a storage spring is fixedly installed between the inside of the circular groove and the sliding shaft, and storage grooves are symmetrically provided on both sides of the storage box.

[0013] The beneficial effects of the utility model are as follows: by setting a shock-absorbing structure, the shock-absorbing spring can provide a buffering force to the parking board when the UAV docks on the parking board, creating a more stable forced landing environment for the UAV, and avoiding unnecessary damage to the UAV during forced landing. By setting a retaining ring, when the parking board contacts the retaining ring, the retaining ring restricts it. A shock-absorbing seat is fixedly installed at the bottom of the retaining ring, and the shock-absorbing seat is connected to the support lever to control the vertical height of the parking board, while ensuring that the parking board will not sway left and right due to deviating from the ideal track.

[0014] By setting up the storage structure, when the support lever is in a non-stationary state relative to the support seat, the gear is subjected to the external force in the vertical direction and contacts the rack to produce a rotation effect. At the same time, the storage cover also rotates synchronously with the gear. When the support lever is at the bottom, the storage cover opening is facing downward, and the shutdown board is in a closed state. When the support lever is at the top, the storage cover opening is facing upward, and the shutdown board is in a fully open state. The flexible use of the storage structure makes the drone take-off and landing platform more convenient and lightweight. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] Figure 1 This is a schematic diagram of the overall structure of a communication UAV take-off and landing platform of the utility model;

[0016] Figure 2 This is an enlarged view of the buffer structure of a communication UAV take-off and landing platform of the utility model;

[0017] Figure 3This is a schematic diagram of the storage structure of a communication UAV take-off and landing platform of the utility model;

[0018] Figure 4 This is a partial cutaway view of a communication UAV take-off and landing platform of the utility model;

[0019] Figure 5 This is a schematic diagram of a communication UAV take-off and landing platform in a fully opened state according to the utility model;

[0020] Figure 6 The utility model is a schematic diagram of a closed state of a communication UAV take-off and landing platform.

[0021] In the figure: 1. shutdown plate; 2. storage cover; 3. support seat; 4. storage box; 5. buffer structure; 6. retaining ring; 7. shock-absorbing spring; 8. shock-absorbing seat; 9. horizontal axis; 10. square block; 11. storage structure; 12. gear; 13. limit plate; 14. limit rod; 15. rack; 16. support lever; 17. sliding shaft; 18. storage lever; 19. support groove; 20. retaining plate; 21. storage groove; 22. support spring; 23. storage spring. DETAILED DESCRIPTION

[0022] In order to make the technical means, creative features, objectives and effects achieved by the present invention easy to understand, the present invention is further described below in conjunction with specific implementation methods.

[0023] like Figure 1-Figure 6 As shown, a communication UAV take-off and landing platform includes a parking plate 1, a storage cover 2, a support seat 3 and a storage box 4. A buffer structure 5 is arranged at the bottom of the parking plate 1. The buffer structure 5 includes a retaining ring 6 and a shock-absorbing seat 8. The retaining ring 6 is fixedly installed on the upper part of the shock-absorbing seat 8, and eight shock-absorbing springs 7 are fixedly installed at the upper part of the shock-absorbing seat 8 and the inner position of the retaining ring 6. Two horizontal axes 9 are symmetrically fixedly installed on the outside of the shock-absorbing seat 8, and four square blocks 10 are fixedly installed at one end of the two horizontal axes 9.

[0024] In this embodiment, a convex strip is glued and connected to the inner wall of the retaining ring 6 near the shutdown plate 1, and the outer part of the shutdown plate 1 is adaptively matched with the convex strip.

[0025] The stop plate 1 is slidably connected to the inner wall of the retaining ring 6. When the stop plate 1 is forced to slide upward, the convex strips on the inner wall of the retaining ring 6 connected by glue can limit the stop plate 1 and prevent the stop plate 1 from detaching from the retaining ring 6 due to external force.

[0026] In this embodiment, four limit plates 13 are symmetrically mounted on the inner wall of the support seat 3 , and a limit rod 14 and a rack 15 are fixedly mounted on the same side of the four limit plates 13 .

[0027] Four limit plates 13 are distributed on the inner wall of the support seat 3, and each two limit plates 13 form a group, and a gap is left between each two limit plates 13 to limit the vertical movement of the shutdown plate 1. The limit rod 14 is located on the same side of each group of limit plates 13, and the rack 15 is located on the other side of each group of limit plates 13.

[0028] In this embodiment, a storage structure 11 is provided on the outside of the horizontal axis 9, and the storage structure 11 includes a storage cover 2, which is rotatably connected to the horizontal axis 9, and two gears 12 are fixedly installed at symmetrical positions at both ends of the bottom of the storage cover 2, and a support rod 16 is movably installed on the side of the two gears 12 away from the storage cover 2, a square groove is provided at one end of the support rod 16, and a support spring 22 is fixedly installed inside the square groove.

[0029] By sliding the support lever 16, the gear 12 and the rack 15 can be driven to rotate. When the gear 12 rotates, the gear 12 will drive the storage cover 2 to rotate. The gear 12 rotates exactly one circle during the entire rotation cycle, and the rotation circumference is consistent with the displacement distance of the support lever 16, so that when the support lever 16 is at the lowest position, the storage cover 2 and the shutdown plate 1 are relatively closed, and when the support lever 16 is at the highest position, the storage cover 2 and the shutdown plate 1 are relatively opened.

[0030] In this embodiment, the gear 12 is meshed with the rack 15 , the other end of the support spring 22 is fixedly connected to the square block 10 , and the square block 10 is adaptively matched with a square groove opened at one end of the support lever 16 .

[0031] When the support lever 16 is pulled outward, the support lever 16 can be slid in the vertical direction. When the support lever 16 is slid to the highest or lowest end, the outward pulling force is stopped. The support lever 16 moves inward due to the pulling force of the support spring 22, and at the same time is restricted by the four blocks 10 and does not leave the support seat 3.

[0032] In this embodiment, support grooves 19 are provided at symmetrical positions on the outside of the support seat 3, a baffle 20 is fixedly installed on the inner wall of the support groove 19, and two sliding shafts 17 are symmetrically fixedly installed on the outside of the support seat 3 at a vertical position to the two support grooves 19, a storage lever 18 is fixedly installed at one end of the two sliding shafts 17, a circular groove is provided at one end of the storage lever 18, and a storage spring 23 is fixedly installed between the inside of the circular groove and the sliding shaft 17, and storage grooves 21 are symmetrically provided on both sides of the storage box 4.

[0033] The sliding shaft 17 slides up and down through the storage groove 21, and the support seat 3 is fixed at the highest or lowest end by setting the storage lever 18. When the storage lever 18 is pulled outward, the storage lever 18 can be slid in the vertical direction. When the storage lever 18 is slid to the highest or lowest end, the outward pulling force is stopped, and the storage lever 18 moves inward under the pulling force of the storage spring 23.

[0034] It should be noted that the utility model is a communication drone take-off and landing platform. When in use, the storage lever 18 is pulled to make the storage lever 18 move outward under force, and the restriction of the storage groove 21 on the storage lever 18 is released. When the storage lever 18 is slid to the highest point, the outward pulling force on the storage lever 18 is stopped. The storage lever 18 is restricted in the storage groove 21 under the pulling force of the storage spring 23, and an outward pulling force is applied to the support lever 16 to release the restriction of the support groove 19 on the support lever 16. By sliding the support lever 16, the support lever 16 is made to slide upward. While the support lever 16 slides upward, the gear 12 and the rack 15 rotate together. During the rotation of the gear 12, the storage cover 2 rotates synchronously with the gear 12, and the circumference of one rotation of the output wheel 12 is consistent with the displacement distance of the support lever 16. When the support lever 16 is at the highest point, the storage cover 2 and the shutdown plate 1 are in a fully open state.

[0035] A buffer structure 5 is provided at the bottom of the shutdown plate 1, and the shutdown plate 1 is slidably connected to the inner wall of the retaining ring 6. When the shutdown plate 1 is forced to slide upward, the convex strips on the inner wall of the retaining ring 6 connected by glue can limit the shutdown plate 1, thereby preventing the shutdown plate 1 from separating from the retaining ring 6 due to external force. The shutdown plate 1 is connected to the shock-absorbing seat 8 through the shock-absorbing spring 7. The shutdown plate 1 benefits from the spring properties of the shock-absorbing spring 7 and can flexibly change its relative vertical position with the shock-absorbing seat 8.

[0036] The above shows and describes the basic principle and main features of the utility model and the advantages of the utility model. The technicians in this industry should understand that the utility model is not limited by the above embodiments, and the above embodiments and descriptions are only for explaining the principle of the utility model. Without departing from the spirit and scope of the utility model, the utility model will have various changes and improvements, and these changes and improvements fall within the scope of the utility model to be protected.

Claims

1. A communication drone take-off and landing platform, comprising a parking plate (1), a storage cover (2), a support seat (3) and a storage box (4), characterized in that: A buffer structure (5) is provided at the bottom of the shutdown plate (1), and the buffer structure (5) comprises a retaining ring (6) and a shock absorbing seat (8), wherein the retaining ring (6) is fixedly mounted on the upper part of the shock absorbing seat (8), and eight shock absorbing springs (7) are fixedly mounted at the upper part of the shock absorbing seat (8) and the inner position of the retaining ring (6), and two transverse axes (9) are symmetrically fixedly mounted on the outside of the shock absorbing seat (8), and four square blocks (10) are fixedly mounted on one end of each of the two transverse axes (9).

2. A communication UAV take-off and landing platform according to claim 1, characterized in that: The inner wall of the retaining ring (6) is glued with a convex strip near the stop plate (1), and the outer portion of the stop plate (1) is adaptively matched with the convex strip.

3. A communication UAV take-off and landing platform according to claim 1, characterized in that: Four limiting plates (13) are symmetrically mounted on the inner wall of the support seat (3), and limiting rods (14) and racks (15) are respectively fixedly mounted at positions on the same side of the four limiting plates (13).

4. A communication UAV take-off and landing platform according to claim 1, characterized in that: A storage structure (11) is arranged outside the transverse axis (9), and the storage structure (11) comprises a storage cover (2). The storage cover (2) is rotatably connected to the transverse axis (9), and two gears (12) are fixedly installed at symmetrical positions at both ends of the bottom of the storage cover (2). A support lever (16) is movably installed on one side of the two gears (12) away from the storage cover (2), and a square groove is provided at one end of the support lever (16), and a support spring (22) is fixedly installed inside the square groove.

5. A communication UAV take-off and landing platform according to claim 4, characterized in that: The gear (12) is meshedly connected with the rack (15), the other end of the support spring (22) is fixedly connected to the square block (10), and the square block (10) is adaptively matched with a square groove opened at one end of the support lever (16).

6. The communication UAV take-off and landing platform according to claim 1, characterized in that: A support groove (19) is provided at a symmetrical position on the outside of the support seat (3), a blocking piece (20) is fixedly installed on the inner wall of the support groove (19), and two sliding shafts (17) are symmetrically fixedly installed on the outside of the support seat (3) at a position perpendicular to the two support grooves (19), one end of each of the two sliding shafts (17) is fixedly installed with a storage lever (18), one end of each of the storage levers (18) is provided with a circular groove, and a storage spring (23) is fixedly installed between the inside of the circular groove and the sliding shaft (17), and storage grooves (21) are symmetrically provided on both sides of the storage box (4).

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