CN216546798U

CN216546798U - Unmanned aerial vehicle kinetic energy comprehensive test platform

Info

Publication number: CN216546798U
Application number: CN202220329395.XU
Authority: CN
Inventors: 赵安民
Original assignee: Tianjin Yikexin Technology Co ltd
Current assignee: Tianjin Yikexin Technology Co ltd
Priority date: 2022-02-18
Filing date: 2022-02-18
Publication date: 2022-05-17
Anticipated expiration: 2032-02-18

Abstract

The utility model provides an unmanned aerial vehicle kinetic energy comprehensive test platform, which relates to the technical field of unmanned tests and comprises a plate body, wherein a limiting frame is fixedly arranged on the surface of the plate body, a straight groove is formed in the surface of the limiting frame, a round rod is sleeved in the straight groove, a folded plate is fixedly arranged on the surface of the round rod, a table body is fixedly arranged on the surface of the folded plate, and a chest expander is arranged on the surface of the table body. According to the unmanned aerial vehicle, by arranging the folding plate, a worker can connect the unmanned aerial vehicle frame with the hook of the chest expander through the rope, so that the vertical kinetic energy of the unmanned aerial vehicle can be tested, the folding plate can be pulled to move and rotate, the chest expander is parallel to the plate body, the pin rod is inserted into the sleeve block, the folding plate is fixed, the transverse kinetic energy of the unmanned aerial vehicle can be tested through the chest expander, the comprehensive kinetic energy of the unmanned aerial vehicle can be tested, the operation is simple, and the unmanned aerial vehicle can be conveniently used by the worker.

Description

Unmanned aerial vehicle kinetic energy comprehensive test platform

Technical Field

The utility model relates to the technical field of unmanned testing, in particular to an unmanned aerial vehicle kinetic energy comprehensive testing platform.

Background

In unmanned aerial vehicle's test procedure, often need use test platform to test unmanned aerial vehicle's kinetic energy, and current test platform is in the use, and it often is fixed, often only can test unmanned aerial vehicle's vertical direction kinetic energy in the use, need test horizontal kinetic energy, when testing unmanned aerial vehicle's kinetic energy comprehensively, need build test platform again, this process complex operation, the staff of being not convenient for uses.

SUMMERY OF THE UTILITY MODEL

The utility model aims to solve the defects in the prior art and provides a comprehensive test platform for kinetic energy of an unmanned aerial vehicle.

In order to achieve the purpose, the utility model adopts the following technical scheme: the utility model provides an unmanned aerial vehicle kinetic energy integrated test platform, the package rubbing board body, the fixed surface of plate body installs spacing, the straight flute has been seted up on spacing surface, the inside cover of straight flute is equipped with the round bar, the fixed surface of round bar installs the folded plate, the fixed surface of folded plate installs the stage body, the surface mounting of stage body has the chest expander, spacing section of thick bamboo is equipped with admittedly on spacing surface, spacing section of thick bamboo's inside cover is equipped with the pin rod, the fixed surface of folded plate installs the pocket, pin rod and pocket sliding connection.

In order to support the plate body, the utility model is improved in that a support leg is fixedly arranged at the bottom of the plate body, and a round hole is formed in the bottom of the support leg.

In order to fix the folded plate stably, the utility model has the improvement that a tension spring is fixedly arranged between the pin rod and the limiting cylinder, and one end of the pin rod is fixedly provided with a pull ring.

In order to facilitate pulling of the folded plate, the folded plate is improved in that a notch is formed in the surface of the folded plate, and a straight rod is fixedly installed inside the notch.

In order to fix the folded plate stably, the utility model improves that the surface of the folded plate is fixedly provided with an attaching pad, and the material of the attaching pad is one of sponge, foam and resin.

In order to conveniently lift the unmanned aerial vehicle, the unmanned aerial vehicle lifting device is improved in that a supporting structure is arranged on the surface of the plate body and comprises a sleeve, the sleeve is fixedly connected with the plate body, a vertical plate is connected inside the sleeve in a sliding mode, a U-shaped plate is fixedly installed on one side of the vertical plate, a clamping groove is formed in the surface of the vertical plate, and an elastic sheet is fixedly installed at the bottom of the sleeve.

In order to enable the unmanned aerial vehicle to be placed stably, the unmanned aerial vehicle is improved in the utility model that silica gel pads are fixedly arranged on the surfaces of the U-shaped plates and are symmetrically distributed.

Compared with the prior art, the utility model has the advantages and positive effects that,

1. according to the utility model, by arranging the folding plate, a worker can connect the unmanned aerial vehicle frame with the hook of the chest expander through the rope, so that the vertical kinetic energy of the unmanned aerial vehicle can be tested, the folding plate can be pulled to move and rotate, the chest expander is parallel to the plate body, the pin rod is inserted into the sleeve block, the folding plate is fixed, the horizontal kinetic energy of the unmanned aerial vehicle can be tested through the chest expander, the comprehensive kinetic energy of the unmanned aerial vehicle can be tested, the operation is simple, and the use of the worker is facilitated.

2. According to the unmanned aerial vehicle support structure, by means of the support structure, a worker can place the unmanned aerial vehicle on the U-shaped plate and push the vertical plate to slide along the sleeve, the U-shaped plate can be located at a proper height, the elastic pieces can be clamped into the clamping grooves, the height of the U-shaped plate is fixed, and therefore the unmanned aerial vehicle can be located at a proper height, and the worker can lift the unmanned aerial vehicle to test in time.

Drawings

Fig. 1 is a schematic view of the overall structure of an unmanned aerial vehicle kinetic energy comprehensive test platform provided by the utility model;

fig. 2 is a schematic side view of the kinetic energy comprehensive test platform of the unmanned aerial vehicle according to the present invention;

fig. 3 is a schematic structural diagram of a position a in fig. 2 of the unmanned aerial vehicle kinetic energy comprehensive test platform provided by the utility model;

fig. 4 is a schematic structural view of the unmanned aerial vehicle kinetic energy comprehensive test platform in a bottom view.

Illustration of the drawings:

1. a plate body; 2. a limiting frame; 3. a round bar; 4. folding the plate; 5. a table body; 6. a chest expander; 7. a limiting cylinder; 8. a pin rod; 9. sleeving blocks; 10. supporting legs; 11. a tension spring; 12. a straight rod; 13. attaching a pad; 14. a sleeve; 15. a vertical plate; 16. a U-shaped plate; 17. a card slot; 18. a spring plate; 19. a silica gel pad.

Detailed Description

In order that the above objects, features and advantages of the present invention can be more clearly understood, the present invention will be further described with reference to the accompanying drawings and examples. It should be noted that the embodiments and features of the embodiments of the present application may be combined with each other without conflict.

In the description of the present invention, it is to be understood that the terms "length", "width", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on the orientations or positional relationships illustrated in the drawings, and are used merely for convenience in describing the present invention and for simplicity in description, and do not indicate or imply that the devices or elements referred to must have a particular orientation, be constructed in a particular orientation, and be operated, and thus, are not to be construed as limiting the present invention. Further, in the description of the present invention, "a plurality" means two or more unless specifically defined otherwise.

Example one

As shown in fig. 1 to 4, the present invention provides a technical solution: an unmanned aerial vehicle kinetic energy comprehensive test platform comprises a plate body 1, a limiting frame 2 is fixedly installed on the surface of the plate body 1, a straight groove is formed in the surface of the limiting frame 2, a round rod 3 is sleeved inside the straight groove, a folded plate 4 is fixedly installed on the surface of the round rod 3, a table body 5 is fixedly installed on the surface of the folded plate 4, a chest expander 6 is installed on the surface of the table body 5, a limiting cylinder 7 is fixedly installed on the surface of the limiting frame 2, a pin rod 8 is sleeved inside the limiting cylinder 7, a sleeve block 9 is fixedly installed on the surface of the folded plate 4, the pin rod 8 is in sliding connection with the sleeve block 9, a worker can connect a hook of the unmanned aerial vehicle frame and the chest expander 6 through a rope, so that the vertical kinetic energy of an unmanned aerial vehicle can be tested, the folded plate 4 can be pulled to move and rotate, the chest expander 6 is parallel to the plate body 1, the pin rod 8 is inserted into the sleeve block 9, the folded plate 4 is fixed, and the transverse kinetic energy of the unmanned aerial vehicle can be tested through the chest expander 6, thereby test unmanned aerial vehicle's comprehensive kinetic energy, easy operation makes things convenient for the staff to use.

As shown in fig. 1-4, a support leg 10 is fixedly installed at the bottom of a plate body 1, a round hole is formed at the bottom of the support leg 10, a worker can use a proper bolt set to pass through the round hole to fix the support leg 10, the plate body 1 is prevented from shaking in the using process and affecting the test result, a tension spring 11 is fixedly installed between a pin rod 8 and a limiting cylinder 7, one end of the pin rod 8 is fixedly provided with a pull ring, the tension spring 11 can pull the pin rod 8 and prevent the pin rod 8 from easily moving, the pull ring can facilitate the worker to pull the pin rod 8, a notch is formed in the surface of a folded plate 4, a straight rod 12 is fixedly installed inside the notch so that the worker can use the straight rod 12 to drive the folded plate 4 to move, a bonding pad 13 is fixedly installed on the surface of the folded plate 4, the bonding pad 13 is made of one of sponge, foam and resin, and the sponge, the foam and the resin all have certain elasticity, the application pad 13 can fill the gap between the folded plate 4 and the plate body 1, so that the folded plate 4 is more stable in the test process.

Example two

As shown in fig. 1-2, the surface of plate body 1 is provided with holds in the palm puts the structure, hold in the palm and put the structure and include sleeve 14,

sleeve

14 and 1 fixed connection of plate body, sleeve 14's inside sliding connection has riser 15, one side fixed mounting of riser 15 has U-shaped plate 16, draw-in groove 17 has been seted up on riser 15's surface, sleeve 14's bottom fixed mounting has shell fragment 18, the staff can place unmanned aerial vehicle on U-shaped plate 16, and promote riser 15 and slide along sleeve 14, make U-shaped plate 16 can be in suitable height, and inside shell fragment 18 can block into draw-in groove 17, highly fixing U-shaped plate 16, thereby make unmanned aerial vehicle can be in suitable height, so that the staff can rise unmanned aerial vehicle in time and test.

As shown in fig. 1-2, the fixed surface of U-shaped plate 16 has silica gel pad 19, and silica gel pad 19 is the symmetric distribution, and silica gel pad 19 can increase the frictional force between unmanned aerial vehicle and U-shaped plate 16, makes unmanned aerial vehicle can be more stable putting the in-process.

The working principle is as follows: when testing the vertical kinetic energy of the unmanned aerial vehicle, the frame of the unmanned aerial vehicle can be connected with the hook of the chest expander 6 through a proper rope, then the unmanned aerial vehicle can be controlled to rise, the vertical kinetic energy of the unmanned aerial vehicle can be tested through the chest expander 6, when the horizontal kinetic energy of the unmanned aerial vehicle needs to be tested, the pull ring can be pulled outwards, the pin rod 8 is pulled out of the sleeve block 9, the straight rod 12 can be pulled to drive the folded plate 4 to move, the round rod 3 can move along the limiting frame 2, the round rod 3 is moved to the other end of the straight groove, the folded plate 4 is rotated, the other side of the folded plate 4 is contacted with the plate body 1, the chest expander 6 is parallel to the plate body 1, the pin rod 8 can be loosened, the pin rod 8 can be pulled by the tension spring 11, the pin rod 8 can be inserted into the sleeve block 9 at the position, the folded plate 4 can be fixed, then the horizontal movement of the unmanned aerial vehicle can be controlled through the tension, the horizontal movement of the unmanned aerial vehicle can be tested through the chest expander 6, and laminating pad 13 can fill the space between folded plate 4 and the plate body 1, make folded plate 4 more stable in the testing process, and in the testing process, the staff can stimulate riser 15 and remove, make U-shaped board 16 be in suitable height, and inside shell fragment 18 can block into draw-in groove 17, fix riser 15, can put the unmanned aerial vehicle that needs to carry out the test on U-shaped board 16, silica gel pad 19 can make unmanned aerial vehicle put stably, so that staff control unmanned aerial vehicle rises and removes, and in the testing process, can outwards stir shell fragment 18, make shell fragment 18 shift out draw-in groove 17, can fall U-shaped board 16, prevent that U-shaped board 16 from influencing going on of test.

The above description is only a preferred embodiment of the present invention, and not intended to limit the present invention in other forms, and any person skilled in the art may apply the above modifications or changes to the equivalent embodiments with equivalent changes by using the technical contents disclosed in the above description to other fields, but any simple modification, equivalent change and change made to the above embodiments according to the technical essence of the present invention still belong to the protection scope of the technical solution of the present invention.

Claims

1. The utility model provides an unmanned aerial vehicle kinetic energy integrated test platform, includes plate body (1), its characterized in that: the utility model discloses a limiting device, including plate body (1), plate body (2), straight flute have been seted up on the surface of limiting frame (2), the inside cover of straight flute is equipped with round bar (3), the fixed surface of round bar (3) installs folded plate (4), the fixed surface of folded plate (4) installs stage body (5), the surface mounting of stage body (5) has chest expander (6), the surface of limiting frame (2) is equipped with spacing section of thick bamboo (7) admittedly, the inside cover of spacing section of thick bamboo (7) is equipped with pin rod (8), the fixed surface of folded plate (4) installs pocket (9), pin rod (8) and pocket (9) sliding connection.

2. The unmanned aerial vehicle kinetic energy comprehensive test platform of claim 1, characterized in that: the bottom of the plate body (1) is fixedly provided with a supporting leg (10), and a round hole is formed in the bottom of the supporting leg (10).

3. The unmanned aerial vehicle kinetic energy comprehensive test platform of claim 1, characterized in that: a tension spring (11) is fixedly mounted between the pin rod (8) and the limiting cylinder (7), and a pull ring is fixedly mounted at one end of the pin rod (8).

4. The unmanned aerial vehicle kinetic energy comprehensive test platform of claim 1, characterized in that: the surface of the folded plate (4) is provided with a gap, and a straight rod (12) is fixedly arranged in the gap.

5. The unmanned aerial vehicle kinetic energy comprehensive test platform of claim 1, characterized in that: the fixed surface of folded plate (4) installs laminating pad (13), the material of laminating pad (13) is one of sponge, foam and resin.

6. The unmanned aerial vehicle kinetic energy comprehensive test platform of claim 1, characterized in that: the surface of plate body (1) is provided with and holds in the palm puts the structure, hold in the palm and put the structure and include sleeve (14), sleeve (14) and plate body (1) fixed connection, the inside sliding connection of sleeve (14) has riser (15), one side fixed mounting of riser (15) has U-shaped board (16), draw-in groove (17) have been seted up on the surface of riser (15), the bottom fixed mounting of sleeve (14) has shell fragment (18).

7. The unmanned aerial vehicle kinetic energy comprehensive test platform of claim 6, characterized in that: the surface of the U-shaped plate (16) is fixedly provided with silica gel pads (19), and the silica gel pads (19) are symmetrically distributed.