A device for horizontal calibration detection of a drone wing

Abstract

The utility model relates to unmanned aerial vehicle wing level calibration detection technical field discloses a kind of unmanned aerial vehicle wing level calibration detection devices, including base and support seat, the top of the base is provided with fixed frame, the right side fixedly connected with support seat in the top of the base, the top of the support seat is fixedly connected with top plate, the inside fixed mounting of the fixed frame has second cylinder.This unmanned aerial vehicle wing level calibration detection device is provided with second cylinder and other parts, opens second cylinder, and the fixed block can be moved using second telescopic link, so as to conveniently adjust the position of level ruler, when it is necessary to replace level ruler, the elasticity of reset spring can be used to pull the movable block forward, at this time, the guide rod will guide the movable block in the guide groove, so that the level ruler can be conveniently and quickly assembled and disassembled, and the problem of inconvenient automatic adjustment of the position of level ruler during detection is solved, and the problem of inconvenient quick assembly and disassembly is also solved.

Description

Technical Field

[0001] This utility model relates to the field of drone wing level verification and testing technology, specifically a device for drone wing level verification and testing. Background Technology

[0002] The drone wing leveling and testing device is mainly used to detect the levelness of the drone wing, thereby ensuring the stability of the drone during flight. Its core is to measure the relative position of the wing and the fuselage, and then use a level ruler placed on the wing to determine whether there is any tilt or deviation.

[0003] The existing design of the device for verifying and testing the level of UAV wings is not convenient for automatically adjusting the position of the level ruler during the testing process, nor is it convenient for quick loading and unloading. Therefore, its structure needs to be improved.

[0004] Now, a novel device for verifying and testing the horizontal alignment of UAV wings is proposed to solve the above problems. Utility Model Content

[0005] The purpose of this invention is to provide a device for verifying and testing the level of a drone wing, in order to solve the problems mentioned in the background art, such as the inconvenience of automatically adjusting the position of the level ruler during the testing process and the inconvenience of quick loading and unloading.

[0006] To achieve the above objectives, this utility model provides the following technical solution: a device for leveling and inspecting the wings of a UAV, comprising a base and a support base. A fixed frame is provided at the top of the base, and a support base is fixedly connected to the right side of the top of the base. A top plate is fixedly connected to the top of the support base. A second cylinder is fixedly installed inside the fixed frame. A second telescopic rod is movably connected to one side of the second cylinder. A fixed block is fixedly connected to one side of the second telescopic rod. An installation groove is provided inside one side of the fixed block. A guide groove is provided at the rear end of the installation groove. A return spring is fixedly connected to the rear end inside the installation groove. A guide rod is provided inside the return spring. A movable block is fixedly connected to the front end of the return spring and the guide rod. A level is placed between the movable block and the fixed block.

[0007] As a further technical solution of this utility model, the rear end of the guide rod is movable and embedded inside the guide groove.

[0008] As a further technical solution of this utility model, a testing platform is fixedly connected to the left side of the top of the base, and an industrial camera is fixedly installed on one side of the bottom of the top plate.

[0009] As a further technical solution of this utility model, a fixing rod is fixedly connected between the base and the fixing seat, and a fixing seat is fixedly connected to the right side of the fixing frame. The fixing seat is sleeved on the outside of the fixing rod and is movable.

[0010] As a further technical solution of this utility model, a connecting seat is fixedly connected to one side of the front end of the base, and a controller is fixedly connected to the top of the connecting seat.

[0011] As a further technical solution of this utility model, a first cylinder is fixedly installed at the top of the top plate, and a first telescopic rod is movably connected to the bottom of the first cylinder. The bottom of the first telescopic rod penetrates the interior of the top plate and is fixedly connected to the top of the fixed frame.

[0012] Compared with the prior art, the beneficial effects of this utility model are: the device for checking and testing the level of UAV wings not only makes it easy to adjust the position and quickly install and remove the level ruler, but also makes it easy to view the real-time deviation in a timely manner, and makes it easy to flexibly adjust the height of the test placement according to the height of the wings.

[0013] The system is equipped with a second cylinder, a second telescopic rod, a level, a movable block, a mounting groove, a return spring, and a guide rod. When the second cylinder is opened, the second telescopic rod can move the fixed block, which makes it easy to adjust the position of the level. When the level needs to be replaced, the elasticity of the return spring can be used to pull the movable block forward. At this time, the guide rod will guide the movement in the guide groove, making it easy to install and remove the level quickly.

[0014] The system is equipped with a base, connector, controller, testing platform, and industrial camera. The industrial camera on top allows for real-time monitoring of the level gauge data and real-time transmission to the controller screen for easy viewing. This enables timely correction when there is a deviation in the levelness of the wing.

[0015] The system includes a support base, a fixed rod, a top plate, a first cylinder, a first telescopic rod, a fixed frame, and a fixed seat. When the first cylinder is opened, the first telescopic rod can be used to move the fixed frame downwards. At this time, the fixed seat can be guided and raised on the fixed rod, so that the level can be automatically placed according to the height of the wing when placing it, making it more flexible in use. Attached Figure Description

[0016] Figure 1 This is a frontal cross-sectional view of the present invention.

[0017] Figure 2 This is a top view of the connection method between the fixed block and the movable block of this utility model;

[0018] Figure 3 This is a front view structural diagram of the connection method between the controller and the base of this utility model;

[0019] Figure 4 This is a side view of the connection between the fixing rod and the fixing seat of this utility model.

[0020] In the diagram: 1. Base; 2. Connecting seat; 3. Controller; 4. Detection table; 5. Support seat; 6. Fixing rod; 7. Top plate; 8. First cylinder; 9. First telescopic rod; 10. Fixing frame; 11. Fixing seat; 12. Second cylinder; 13. Second telescopic rod; 14. Level; 15. Movable block; 16. Mounting slot; 17. Return spring; 18. Guide rod; 19. Industrial camera; 20. Fixing block; 21. Guide slot. Detailed Implementation

[0021] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0022] Please see Figure 1-4 This utility model provides an embodiment of a device for verifying and testing the level of a drone wing, including a base 1 and a support 5. A fixed frame 10 is provided at the top of the base 1, and the support 5 is fixedly connected to the right side of the top of the base 1. A top plate 7 is fixedly connected to the top of the support 5. A second cylinder 12 is fixedly installed inside the fixed frame 10. A second telescopic rod 13 is movably connected to one side of the second cylinder 12. A fixed block 20 is fixedly connected to one side of the second telescopic rod 13. An installation groove 16 is provided inside one side of the fixed block 20. A guide groove 21 is provided at the rear end of the installation groove 16. A return spring 17 is fixedly connected to the rear end inside the installation groove 16. A guide rod 18 is provided inside the return spring 17. A movable block 15 is fixedly connected to the front end of the return spring 17 and the guide rod 18. A level 14 is placed between the movable block 15 and the fixed block 20.

[0023] The rear end of the guide rod 18 is movable and embedded inside the guide groove 21;

[0024] Specifically, such as Figure 1 and Figure 2 As shown, when the second cylinder 12 is opened, the second telescopic rod 13 can drive the fixed block 20 to move, thereby facilitating the adjustment of the position of the level 14. When the level 14 needs to be replaced, the elasticity of the return spring 17 can be used to pull the movable block 15 forward. At this time, the guide rod 18 will guide the movement in the guide groove 21, making it easy and quick to install and remove the level 14.

[0025] A testing platform 4 is fixedly connected to the top left side of the base 1, and an industrial camera 19 is fixedly installed on one side of the bottom of the top plate 7.

[0026] A connecting seat 2 is fixedly connected to one side of the front end of the base 1, and a controller 3 is fixedly connected to the top of the connecting seat 2;

[0027] Specifically, such as Figure 1 and Figure 3 As shown, the industrial camera 19 on the top facilitates real-time monitoring of the data from the level ruler 14 and transmits it to the screen of the controller 3 for easy viewing, making it convenient to correct any deviations in the levelness of the wings in a timely manner.

[0028] A fixing rod 6 is fixedly connected between the base 1 and the fixing seat 11. The fixing seat 11 is fixedly connected to the right side of the fixing frame 10. The fixing seat 11 is sleeved on the outside of the fixing rod 6 and is movable.

[0029] A first cylinder 8 is fixedly installed at the top of the top plate 7, and a first telescopic rod 9 is movably connected to the bottom of the first cylinder 8. The bottom of the first telescopic rod 9 passes through the interior of the top plate 7 and is fixedly connected to the top of the fixed frame 10.

[0030] Specifically, such as Figure 1 and Figure 4 As shown, when the first cylinder 8 is opened, the first telescopic rod 9 can drive the fixed frame 10 to move downward. At this time, the fixed seat 11 can be guided and raised on the fixed rod 6, so that the level ruler 14 can be automatically placed according to the height of the wing when it is placed, making it more flexible in use.

[0031] Working principle: When using this utility model, firstly, the first cylinder 8 is opened, and the first telescopic rod 9 can drive the fixed frame 10 to move downward. At this time, the fixed seat 11 can be guided and raised on the fixed rod 6, so that the level ruler 14 can be automatically placed according to the height of the wing, making it more flexible in use. Then, the second cylinder 12 is opened, and the second telescopic rod 13 can drive the fixed block 20 to move, thereby facilitating the adjustment of the placement position of the level ruler 14. When the level ruler 14 needs to be replaced, the elasticity of the return spring 17 can be used to pull the movable block 15 forward. At this time, the guide rod 18 will guide the movement in the guide groove 21, making it easy to quickly install and remove the level ruler 14. Finally, the industrial camera 19 on the top can be used to monitor the data of the level ruler 14 in real time and transmit it to the screen of the controller 3 in real time, so as to facilitate real-time viewing and timely correction when there is a deviation in the levelness of the wing.

[0032] It will be apparent to those skilled in the art that this invention is not limited to the details of the exemplary embodiments described above, and that it can be implemented in other specific forms without departing from the spirit or essential characteristics of this invention. Therefore, the embodiments should be considered illustrative and non-limiting in all respects, and the scope of this invention is defined by the appended claims rather than the foregoing description. Thus, it is intended that all variations falling within the meaning and scope of equivalents of the claims be included within this invention. No reference numerals in the claims should be construed as limiting the scope of the claims.

Claims

1. A device for verifying and testing the horizontal alignment of a UAV wing, comprising a base (1) and a support (5), characterized in that: A fixed frame (10) is provided at the top of the base (1). A support seat (5) is fixedly connected to the right side of the top of the base (1). A top plate (7) is fixedly connected to the top of the support seat (5). A second cylinder (12) is fixedly installed inside the fixed frame (10). A second telescopic rod (13) is movably connected to one side of the second cylinder (12). A fixed block (20) is fixedly connected to one side of the second telescopic rod (13). An installation groove (16) is provided inside one side of the fixed block (20). A guide groove (21) is provided at the rear end of the installation groove (16). A return spring (17) is fixedly connected to the rear end of the installation groove (16). A guide rod (18) is provided inside the return spring (17). A movable block (15) is fixedly connected to the front end of the return spring (17) and the guide rod (18). A level (14) is placed between the movable block (15) and the fixed block (20).

2. The device for level verification and testing of UAV wings according to claim 1, characterized in that: The rear end of the guide rod (18) is movable and embedded inside the guide groove (21).

3. The device for level verification and testing of UAV wings according to claim 1, characterized in that: A testing platform (4) is fixedly connected to the left side of the top of the base (1), and an industrial camera (19) is fixedly installed on one side of the bottom of the top plate (7).

4. The device for level verification and testing of UAV wings according to claim 1, characterized in that: A fixing rod (6) is fixedly connected between the base (1) and the fixing seat (11), and a fixing seat (11) is fixedly connected to the right side of the fixing frame (10). The fixing seat (11) is sleeved on the outside of the fixing rod (6) and is movable.

5. The device for level verification and testing of UAV wings according to claim 1, characterized in that: A connecting seat (2) is fixedly connected to one side of the front end of the base (1), and a controller (3) is fixedly connected to the top of the connecting seat (2).

6. The device for level verification and testing of UAV wings according to claim 1, characterized in that: The top of the top plate (7) is fixedly installed with a first cylinder (8), and the bottom of the first cylinder (8) is movably connected with a first telescopic rod (9). The bottom of the first telescopic rod (9) penetrates the interior of the top plate (7) and is fixedly connected to the top of the fixed frame (10).

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