A device for detecting the performance of a drone

Abstract

The utility model relates to an unmanned plane technical field discloses an unmanned plane performance detection device, including box and four rotor unmanned plane, the top fixedly connected with casing of box, the front end right side of box is rotatively connected with the box cover, the inner wall top middle part of casing is rotatively connected with the top middle part of box between electric gyro outside ring, the inner wall left and right sides of electric gyro outside ring are rotatively connected with electric gyro inside ring, the inner wall top and bottom of electric gyro inside ring are rotatively connected with electric gyro main shaft, the rear end top and bottom of electric gyro main shaft all are fixedly connected with the slide frame. In the utility model, through the tension strip pull and move the top block, then the plug -in board is inserted into the plug -in frame, then through the second spring and tightly push the top block, can let the top block be inserted in the top and bottom of four rotor unmanned plane firmly, thereby installs four rotor unmanned plane, according to the above steps, also can also take down four rotor unmanned plane.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) technology, specifically to a UAV performance testing device. Background Technology

[0002] Drones can replace human workers in dangerous scenarios (such as fire rescue and power line inspection) to ensure safety; improve efficiency and reduce costs in fields such as agricultural plant protection and geographic surveying; and can also be used for aerial filming and scientific research exploration, expanding the dimensions of human observation and action.

[0003] The multi-rotor UAV multi-degree-of-freedom test and training platform is a professional device for simulating UAV flight attitude. It can conduct teaching and training in a controlled environment without actual take-off, and can also verify flight control algorithms, ensuring training safety and data accuracy, thus assisting UAV teaching and research and development.

[0004] Existing drone performance testing devices have the following problems: they are inconvenient to quickly disassemble or install drones, and usually require the use of wrenches or bolts to install or disassemble drones, which is not only time-consuming and laborious, but also easy to scratch the coating on the surface of drones. In order to address the above problems, a drone performance testing device is proposed. Utility Model Content

[0005] The purpose of this invention is to provide a drone performance testing device, which solves the problem in the background art of the inconvenience of quickly disassembling or installing drones.

[0006] To achieve the above objectives, this utility model provides the following technical solution: a drone performance testing device, comprising a housing and a quadcopter drone. A shell is fixedly connected to the top of the housing. A cover is rotatably connected to the right front end of the housing. An outer ring of an electric gyroscope is rotatably connected between the top center of the inner wall of the shell and the top center of the housing. Inner rings of an electric gyroscope are rotatably connected to the left and right sides of the inner wall of the outer ring. An electric gyroscope spindle is rotatably connected to the top and bottom of the inner wall of the inner ring. Sliding frames are fixedly connected to the top and bottom of the rear end of the electric gyroscope spindle. A top block is slidably connected to the inner wall of the sliding frame. A second spring is fixedly connected to one end of the top block, and one end of the second spring is fixedly connected to the sliding frame. The other end of the top block penetrates and slidably connects to the quadcopter drone. A pull bar is fixedly connected to the rear end of the top block, and the pull bar penetrates and slidably connects to the sliding frame. A locking component is provided on the left front end of the cover.

[0007] By adopting the above technical solution, the top block is moved by pulling the pull bar, and then the insert plate is inserted into the insert frame. Then, the top block is pressed tightly by the second spring, so that the top block can be firmly inserted into the top and bottom of the quadcopter drone, thereby installing the quadcopter drone. The quadcopter drone can also be disassembled by following the above steps.

[0008] As a further description of the above technical solution: the locking assembly includes a lock head, the rear end of which is fixedly connected to the box cover, a connecting plate is fixedly connected to the top center of the front end of the lock head, a uniformly distributed first spring is fixedly connected to the bottom of the connecting plate, a top plate is fixedly connected to the bottom of the first spring, a first sliding groove is formed in the middle of the rear end of the lock head, the inner wall of the first sliding groove is slidably connected to the top plate, a mounting plate is fixedly connected to the bottom of the top plate, and a brush plate is slidably connected to the rear end of the mounting plate.

[0009] By adopting the above technical solution, by pulling the top plate, the top plate presses the first spring and moves along the inner wall of the first slide groove. The fingerprint is recognized through the fingerprint recognition area, which opens the box cover for maintenance. Releasing the top plate allows the brush plate to clean the surface of the fingerprint recognition area. The brush plate covers the surface of the fingerprint recognition area to ensure its cleanliness. Pulling the top plate to the appropriate position allows the brush plate to be replaced.

[0010] As a further description of the above technical solution: L-shaped plates are fixedly connected to the bottom left and right sides of the front center of the lock head, one side of the L-shaped plate is slidably connected to the mounting plate, and the top of the L-shaped plate is in contact with the top plate.

[0011] By adopting the above technical solution, the brush plate is prevented from falling off by using an L-shaped plate.

[0012] As a further description of the above technical solution: a fingerprint recognition area is provided at the bottom center of the front end of the brush plate, and the surface of the fingerprint recognition area is in contact with the brush plate.

[0013] By adopting the above technical solution, the box lid can be opened through the fingerprint recognition area.

[0014] As a further description of the above technical solution: omnidirectional wheels are provided at the four bottom corners of the box.

[0015] By adopting the above technical solution, the box is moved by using casters.

[0016] As a further description of the above technical solution: the front top and bottom of the quadcopter drone are fixedly connected with insert plates, which are connected to the main shaft of the electric gyroscope through and slidably.

[0017] By adopting the above technical solution, the quadcopter drone can be stably installed using a plug-in plate.

[0018] As a further description of the above technical solution: the rear end of the electric gyroscope spindle is provided with a frame at the top and bottom, and the inner wall of the frame is slidably connected to the plate.

[0019] By adopting the above technical solution, the insert plate can be stably inserted through the insert frame.

[0020] As a further description of the above technical solution: a second sliding groove is provided at the rear end of the sliding frame, and the inner wall of the second sliding groove is slidably connected to the pull bar.

[0021] By adopting the above technical solution, the pull bar can be moved stably through the second slide groove.

[0022] Compared with the prior art, the beneficial effects of this utility model are as follows: 1. The present invention provides a drone performance testing device, which moves the top block by pulling the pull bar, inserts the insert plate into the insert frame, and then uses the second spring to press the top block firmly, so that the top block can be firmly inserted into the top and bottom of the quadcopter drone, thereby installing the quadcopter drone. The quadcopter drone can also be disassembled by following the above steps.

[0023] 2. The UAV performance testing device provided by this utility model allows the top plate to be pulled, pressing the first spring and moving along the inner wall of the first slide groove. The fingerprint is identified through the fingerprint recognition area, which opens the box cover for maintenance. Releasing the top plate allows the brush plate to clean the surface of the fingerprint recognition area. The brush plate covers the surface of the fingerprint recognition area to ensure its cleanliness. Pulling the top plate to the appropriate position allows the brush plate to be replaced. Attached Figure Description

[0024] Figure 1 This is a perspective view of the present utility model; Figure 2 This is a front perspective view of the present invention; Figure 3 This is a schematic diagram of the lock head of this utility model; Figure 4 This is a schematic diagram of the fingerprint recognition area of ​​this utility model; Figure 5 This is a schematic diagram of the brush plate of this utility model; Figure 6 This is a schematic diagram of the quadcopter drone of this utility model; Figure 7 This is a schematic diagram of the main shaft of the electric gyroscope of this utility model; Figure 8 This is a cross-sectional view of the sliding frame of this utility model.

[0025] In the diagram: 1. Shell; 2. Box body; 3. Caster wheel; 4. Outer ring of electric gyroscope; 5. Cover; 6. Lock; 7. Connecting plate; 8. First spring; 9. Mounting plate; 10. L-shaped plate; 11. Top plate; 12. First slide groove; 13. Fingerprint recognition area; 14. Brush plate; 15. Second slide groove; 16. Quadcopter drone; 17. Pull bar; 18. Inner ring of electric gyroscope; 19. Slide frame; 20. Main spindle of electric gyroscope; 21. Insert plate; 22. Insert frame; 23. Top block; 24. Second spring. Detailed Implementation

[0026] 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.

[0027] To further understand the content of this utility model, a detailed description of this utility model will be provided in conjunction with the accompanying drawings.

[0028] Combination Figures 1-8 This utility model discloses a drone performance testing device, comprising a housing 2 and a quadcopter drone 16. A shell 1 is fixedly connected to the top of the housing 2, securing the shell 1. A cover 5 is rotatably connected to the right front end of the housing 2, covering the housing 2. An electric gyroscope outer ring 4 is rotatably connected between the top center of the inner wall of the shell 1 and the top center of the housing 2. Electric gyroscope inner rings 18 are rotatably connected to the left and right sides of the inner wall of the electric gyroscope outer ring 4. An electric gyroscope spindle 20 is rotatably connected to the top and bottom of the inner wall of the electric gyroscope inner ring 18. Through the interaction of the electric gyroscope outer ring 4, the electric gyroscope inner ring 18, and the electric gyroscope spindle 20, the quadcopter drone 16 can be driven to rotate in different directions. A fingerprint sensor is provided at the bottom center of the front end of the brush plate 14. The surface of the fingerprint recognition area 13 is in contact with the brush plate 14. The cover 5 can be opened by the fingerprint recognition area 13. The bottom four corners of the box body 2 are equipped with universal wheels 3, which drive the box body 2 to move. The front top and bottom of the quadcopter drone 16 are fixedly connected with the insertion plate 21. The insertion plate 21 is connected to the electric gyroscope spindle 20 through and slidingly connected. The quadcopter drone 16 is stably installed by the insertion plate 21. The rear top and bottom of the electric gyroscope spindle 20 are provided with the insertion frame 22. The inner wall of the insertion frame 22 is slidably connected to the insertion plate 21. The insertion plate 21 is stably inserted by the insertion frame 22. The rear end of the sliding frame 19 is provided with the second sliding groove 15. The inner wall of the second sliding groove 15 is slidably connected to the pull bar 17. The pull bar 17 is stably moved by the second sliding groove 15.

[0029] Combination Figures 6-8 The top and bottom of the rear end of the electric gyroscope spindle 20 are fixedly connected to the sliding frame 19. The sliding frame 19 is fixed by the electric gyroscope spindle 20. The inner wall of the sliding frame 19 is slidably connected to the top block 23. One end of the top block 23 is fixedly connected to the second spring 24. One end of the second spring 24 is fixedly connected to the sliding frame 19. The other end of the top block 23 is connected to the quadcopter drone 16 through and slidably. The top block 23 is pressed tightly by the elastic force of the second spring 24, so that the top block 23 can be firmly locked in the top and bottom of the quadcopter drone 16. The rear end of the top block 23 is fixedly connected to the pull bar 17. The pull bar 17 is connected to the sliding frame 19 through and slidably. The top block 23 is moved by pulling the pull bar 17.

[0030] Combination Figures 2-5 A locking assembly is provided on the left front end of the box cover 5. The locking assembly includes a lock head 6. The rear end of the lock head 6 is fixedly connected to the box cover 5. A connecting plate 7 is fixedly connected to the top center of the front end of the lock head 6. A first spring 8 is fixedly connected to the bottom of the connecting plate 7. A top plate 11 is fixedly connected to the bottom of the first spring 8. The top plate 11 is pressed tightly by the elastic force of the first spring 8. A first sliding groove 12 is provided in the middle of the rear end of the lock head 6. The inner wall of the first sliding groove 12 is slidably connected to the top plate 11. The top plate 11 is slidably slidably slid by the first sliding groove 12. An mounting plate 9 is fixedly connected to the bottom of the top plate 11. A brush plate 14 is slidably connected to the rear end of the mounting plate 9. The brush plate 14 is used to clean the fingerprint recognition area 13. L-shaped plates 10 are fixedly connected to the left and right sides of the bottom center of the front end of the lock head 6. One side of the L-shaped plate 10 is slidably connected to the mounting plate 9. The top of the L-shaped plate 10 is in contact with the top plate 11. The brush plate 14 is prevented from falling off by the L-shaped plate 10.

[0031] Working principle: Pulling the top block 23 with the pull bar 17 moves the top block 23, which presses the second spring 24 and moves along the inner wall of the sliding frame 19. Then, the insert plate 21 is inserted into the insert frame 22. After releasing the pull bar 17, the elastic force of the second spring 24 presses the top block 23 firmly, allowing the top block 23 to be firmly inserted into the top and bottom of the quadcopter drone 16, thus installing the quadcopter drone 16. Following the above steps, the quadcopter drone 16 can also be disassembled for inspection of the interior of the housing 2. When inspecting electronic components, by pulling the top plate 11, the top plate 11 presses the first spring 8 and moves along the inner wall of the first slide groove 12. Then, fingerprints are recognized through the fingerprint recognition area 13, and the box cover 5 can be opened for maintenance. Releasing the top plate 11 allows the brush plate 14 to clean the surface of the fingerprint recognition area 13. The brush plate 14 covers the surface of the fingerprint recognition area 13, ensuring its cleanliness. Pulling the top plate 11 to the appropriate position allows the brush plate 14 to be replaced.

[0032] It should be noted that, in this document, relational terms such as "first" and "second" are used only to distinguish one entity or operation from another, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Furthermore, the terms "comprising," "including," or any other variations thereof are intended to cover non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements includes not only those elements but also other elements not expressly listed, or elements inherent to such process, method, article, or apparatus.

[0033] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended claims and their equivalents.

Claims

1. A drone performance testing device, comprising a housing (2) and a quadcopter drone (16), characterized in that: The top of the housing (2) is fixedly connected to the shell (1), and the front right side of the housing (2) is rotatably connected to the cover (5). An electric gyroscope outer ring (4) is rotatably connected between the top middle of the inner wall of the shell (1) and the top middle of the housing (2). An electric gyroscope inner ring (18) is rotatably connected to the left and right sides of the inner wall of the electric gyroscope outer ring (4). An electric gyroscope main shaft (20) is rotatably connected to the top and bottom of the inner wall of the electric gyroscope inner ring (18). The top and bottom of the rear end of the electric gyroscope main shaft (20) are connected to the electric gyroscope main shaft (20). All are fixedly connected to a sliding frame (19), and a top block (23) is slidably connected to the inner wall of the sliding frame (19). A second spring (24) is fixedly connected to one end of the top block (23). One end of the second spring (24) is fixedly connected to the sliding frame (19). The other end of the top block (23) is slidably connected to the quadcopter drone (16). A pull bar (17) is fixedly connected to the rear end of the top block (23). The pull bar (17) is slidably connected to the sliding frame (19). A locking component is provided on the left side of the front end of the box cover (5).

2. The UAV performance testing device according to claim 1, characterized in that: The locking assembly includes a lock head (6), the rear end of which is fixedly connected to the box cover (5), a connecting plate (7) is fixedly connected to the top center of the front end of the lock head (6), a uniformly distributed first spring (8) is fixedly connected to the bottom of the connecting plate (7), a top plate (11) is fixedly connected to the bottom of the first spring (8), a first sliding groove (12) is provided in the middle of the rear end of the lock head (6), the inner wall of the first sliding groove (12) is slidably connected to the top plate (11), a mounting plate (9) is fixedly connected to the bottom of the top plate (11), and a brush plate (14) is slidably connected to the rear end of the mounting plate (9).

3. The UAV performance testing device according to claim 2, characterized in that: The front end of the lock (6) is fixedly connected to the left and right sides of the bottom center of the lock head (6). One side of the L-shaped plate (10) is slidably connected to the mounting plate (9), and the top of the L-shaped plate (10) is in contact with the top plate (11).

4. The UAV performance testing device according to claim 2, characterized in that: A fingerprint recognition area (13) is provided at the bottom center of the front end of the brush plate (14), and the surface of the fingerprint recognition area (13) is in contact with the brush plate (14).

5. The unmanned aerial vehicle (UAV) performance testing device according to claim 1, characterized in that: The box (2) is equipped with casters (3) at the four corners of its bottom.

6. The unmanned aerial vehicle (UAV) performance testing device according to claim 1, characterized in that: The front end of the quadcopter drone (16) is fixedly connected to the top and bottom of the middle section with a plug plate (21), and the plug plate (21) is connected to the electric gyroscope spindle (20) through and slidingly connected.

7. The UAV performance testing device according to claim 1, characterized in that: The electric gyroscope spindle (20) has a frame (22) at the top and bottom of the middle of the rear end, and the inner wall of the frame (22) is slidably connected to the plate (21).

8. The UAV performance testing device according to claim 1, characterized in that: The rear end of the sliding frame (19) is provided with a second sliding groove (15), and the inner wall of the second sliding groove (15) is slidably connected to the pull bar (17).

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