Hanging mechanism for hang-off test

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, and discloses a mounting mechanism for a hang-flight test, which comprises a fixing plate, a fixing mechanism is mounted on the outer side of the fixing plate, a balancing weight is fixedly connected to the outer side of the fixing mechanism, a weight bearing mechanism is mounted at the bottom of the fixing plate, and a supporting mechanism is mounted at the bottom of the weight bearing mechanism. The fixing mechanism comprises a connecting assembly, a telescopic assembly, a positioning assembly and an adjusting assembly, the telescopic assembly comprises a supporting plate, the supporting plate is slidably connected to the interior of the fixing plate, a fixing strip is fixedly connected to the outer side of the supporting plate, and a positioning hole is formed in the outer side of the supporting plate. According to the mounting mechanism, the fixing plate, the supporting plate, the two-way threaded rod, the worm gear, the worm and other structures are matched with one another to drive the sliding block and the arc-shaped block to be adjusted according to the size of the unmanned aerial vehicle support, so that the mounting mechanism is conveniently mounted on the unmanned aerial vehicle, and the mounting mechanism can be mounted on the unmanned aerial vehicle without the support under the cooperation of the connecting plate and the fixing bolt structure.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) technology, and in particular to a mounting mechanism for flight testing. Background Technology

[0002] Drones are unmanned aircraft controlled by radio remote control equipment and their own program control devices, or operated autonomously, either completely or intermittently, by onboard computers. Currently, drones are widely used in aerial photography, agriculture, plant protection, miniature selfies, express delivery, disaster relief, wildlife observation, infectious disease monitoring, surveying, news reporting, power line inspection, disaster relief, film and television shooting, and creating romance, among other fields, by carrying different testing machines.

[0003] After the drone is manufactured, a flight test is required to test whether the drone's performance meets the standards. The flight test is conducted by attaching a mounting mechanism to the bottom of the drone. Existing mounting mechanisms usually consist of structural components such as bolts, connecting plates, fixing blocks, and test accessories. The connecting plate is fixed to the bottom of the drone with bolts, and the test accessories are fixed to the connecting plate with fixing blocks, thereby conducting the flight test of the drone.

[0004] However, the existing mounting mechanism for flight tests is usually fixed to the bottom of the drone without a support frame by bolts. This method cannot be adjusted in time depending on whether the drone has a support frame, resulting in a single fixing method and an inability to adjust the fixing connection in a timely manner. Therefore, a new mounting mechanism for flight tests is proposed to solve the above problems. Utility Model Content

[0005] To overcome the above shortcomings, this utility model provides a mounting mechanism for flight tests, aiming to improve the problem that the existing mounting mechanisms for flight tests have a single fixing method and cannot adjust the fixing connection method according to whether the UAV has a bracket or the size of the bracket.

[0006] To achieve the above objectives, the present invention adopts the following technical solution:

[0007] A mounting mechanism for flight tests includes a fixed plate, a fixing mechanism installed on the outside of the fixed plate, a counterweight block fixedly connected to the outside of the fixing mechanism, a load-bearing mechanism installed at the bottom of the fixed plate, and a support mechanism installed at the bottom of the load-bearing mechanism.

[0008] The fixing mechanism includes a connecting component, a telescopic component, a positioning component, and an adjusting component. The telescopic component includes a support plate, which is slidably connected to the inside of the fixing plate. A fixing strip is fixedly connected to the outside of the support plate, and a slide rail is provided on the outside of the fixing strip. A positioning hole is provided on the outside of the support plate.

[0009] As a further description of the above technical solution:

[0010] The positioning component includes a positioning block, which is slidably connected to the outside of the fixed plate. The positioning block and the positioning hole are engaged with each other. A spring is provided inside the fixed plate.

[0011] As a further description of the above technical solution:

[0012] The adjusting assembly includes a bidirectional threaded rod, which is rotatably connected inside the fixed bar. A worm gear is fixedly connected to the end of the bidirectional threaded rod, and a worm is rotatably connected inside the fixed bar. The worm gear and the worm are interlocked. A handle is fixedly connected to the end of the worm. A slider is threadedly connected to the outside of the bidirectional threaded rod, and an arc-shaped block is connected to the slider by bolts.

[0013] As a further description of the above technical solution:

[0014] The connecting assembly includes a connecting plate, which is fixedly connected to the top of the fixing plate, and a fixing bolt is threaded to the top of the connecting plate;

[0015] As a further description of the above technical solution:

[0016] The load-bearing mechanism includes a load-bearing component, a placement component, and a limiting component. The load-bearing component includes a load-bearing box, which is fixedly connected to the bottom of the fixed plate. A placement box is slidably connected inside the load-bearing box.

[0017] As a further description of the above technical solution:

[0018] The placement assembly includes a partition, which is fixedly connected to the inside of the placement box. A handle is fixedly connected to the outside of the placement box, and a limit hole is provided on the outside of the placement box.

[0019] As a further description of the above technical solution:

[0020] The limiting component includes a retaining seat, which is fixedly connected to the outer side of the load-bearing box. A limiting rod is slidably connected inside the retaining seat, and the limiting rod and the limiting hole are engaged with each other. A spring is provided inside the retaining seat.

[0021] As a further description of the above technical solution:

[0022] The load-bearing mechanism also includes a damping rod, which is fixedly connected to the bottom of the load-bearing box. A silicone block is fixedly connected to the other end of the damping rod, and a compression spring is sleeved on the outer periphery of the damping rod.

[0023] This utility model has the following beneficial effects:

[0024] 1. In this utility model, the sliding block and arc-shaped block can be adjusted according to the size of the drone bracket through the cooperation of structures such as the fixing plate, support plate, bidirectional threaded rod, worm gear, and worm, thus facilitating the installation of the mounting mechanism onto the drone. With the cooperation of the connecting plate and fixing bolt structure, the mounting mechanism can be installed on a drone without a bracket. 2. In this utility model, through the cooperation of structures such as the load-bearing box, placement box, and partition, a fixed weight counterweight can be placed in the placement box, thereby realizing the load test in drone flight experiments. By adding different counterweights, the upper limit of the drone's load capacity can be determined. Attached Figure Description

[0025] Figure 1 This is a three-dimensional schematic diagram of a mounting mechanism for a flight test proposed in this utility model;

[0026] Figure 2 This is a schematic diagram of the counterweight block of the mounting mechanism for a flight test proposed in this utility model;

[0027] Figure 3 This is a cross-sectional schematic diagram of the fixing plate of the mounting mechanism for a flight test proposed in this utility model;

[0028] Figure 4 This is a cross-sectional schematic diagram of the fixing bar of the mounting mechanism for a flight test proposed in this utility model;

[0029] Figure 5 This is a schematic diagram of the placement box for a mounting mechanism in a flight test proposed in this utility model.

[0030] Legend:

[0031] 1. Fixing plate; 2. Connecting plate; 3. Fixing bolt; 4. Support plate; 5. Positioning hole; 6. Positioning block; 7. Spring 1; 8. Fixing strip; 9. Slide rail; 10. Double-sided threaded rod; 11. Worm gear; 12. Worm; 13. Handle; 14. Slider; 15. Arc block; 16. Counterweight block; 17. Load-bearing box; 18. Damping rod; 19. Silicone block; 20. Compression spring; 21. Placement box; 22. Partition plate; 23. Limiting hole; 24. Limiting rod; 25. Card seat; 26. Spring 2. Detailed Implementation

[0032] 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.

[0033] Reference Figures 1-4 This utility model provides an embodiment of a mounting mechanism for flight testing, including a fixed plate 1. A fixing mechanism is installed on the outer side of the fixed plate 1. This fixing mechanism allows for timely adjustment of the fixing method based on whether the drone has a support bracket and the size of the bracket, ensuring better mounting of the mounting mechanism on the drone. A counterweight block 16 is fixedly connected to the outer side of the fixing mechanism. The counterweight block 16 adjusts the weight distribution of the mounting mechanism, preventing one side from being too heavy and affecting the drone's flight. A load-bearing mechanism is installed at the bottom of the fixed plate 1. By adding different counterweights to the load-bearing mechanism, the load capacity of the drone can be tested. A load-bearing mechanism is installed at the bottom of the load-bearing mechanism. The support mechanism reduces the impact force generated when the drone lands. The fixing mechanism includes a connecting component, a telescopic component, a positioning component, and an adjusting component. The telescopic component includes a support plate 4, which is slidably connected to the inside of a fixing plate 1. A fixing strip 8 is fixedly connected to the outside of the support plate 4. The fixing plate 1 provides support for the support plate 4, enabling it to operate stably. The movement of the support plate 4 drives the movement of the fixing strip 8. A slide rail 9 is provided on the outside of the fixing strip 8. A positioning hole 5 is provided on the outside of the support plate 4. The positioning component includes a positioning block 6, which is slidably connected to the outside of the fixing plate 1. The positioning block 6 and the positioning hole 5 are interlocked. The fixing plate 1 is internally equipped with... A spring 7 is provided, and the positioning block 6 is supported by the fixing plate 1 to ensure stable operation. The positioning block 6 and the positioning hole 5 cooperate to fix the support plate 4. The adjustment component includes a bidirectional threaded rod 10, which is rotatably connected inside the fixing bar 8. A worm gear 11 is fixedly connected to the end of the bidirectional threaded rod 10. A worm 12 is rotatably connected inside the fixing bar 8. The worm gear 11 and the worm 12 are interlocked. A handle 13 is fixedly connected to the end of the worm 12. The fixing bar 8 provides support for the bidirectional threaded rod 10 to ensure stable operation. Rotating the handle 13 drives the worm 12 to rotate, and the worm 12 drives the worm gear 11 to rotate. The worm gear 11 drives the bidirectional threaded rod 10 to rotate. The outer side of the bidirectional threaded rod 10 is threaded with a slider 14. The slider 14 is bolted to an arc-shaped block 15. The rotation of the bidirectional threaded rod 10 drives the slider 14 to move inside the slide rail 9. The slider 14 drives the arc-shaped block 15 to move, thereby adjusting the position of the slider 14 according to the size of the drone bracket, so as to facilitate the mounting mechanism to be fixed on the drone. The connecting component includes a connecting plate 2, which is fixedly connected to the top of the fixing plate 1. The top of the connecting plate 2 is threaded with a fixing bolt 3. The connecting plate 2 and the fixing bolt 3 cooperate with each other to fix the mounting mechanism to the bottom of the drone.

[0034] Reference Figure 1 , Figure 3 and Figure 5The load-bearing mechanism includes a load-bearing component, a placement component, and a limiting component. The load-bearing component includes a load-bearing box 17, which is fixedly connected to the bottom of the fixed plate 1. A placement box 21 is slidably connected inside the load-bearing box 17, providing support for the placement box 21 to ensure stable operation. Counterweights are added to the placement box 21 to test the drone's load limit. The placement component includes a partition 22, which is fixedly connected to the inside of the placement box 21. A handle is fixedly connected to the outside of the placement box 21. The partition 22 divides the internal space of the placement box 21, preventing the counterweights from moving freely inside the placement box 21 and affecting the drone's flight status. Limiting holes 23 are provided on the outside of the placement box 21. The limiting component includes a locking seat 25. The seat 25 is fixedly connected to the outside of the bearing box 17. The seat 25 has a sliding limit rod 24 inside, which is engaged with the limit hole 23. The seat 25 has a spring 26 inside, which provides support for the limit rod 24 so that it can run stably. The limit rod 24 and the limit hole 23 cooperate to lock the placement box 21. The spring 26 can reset the limit rod 24 after it is displaced. The load-bearing mechanism also includes a damping rod 18, which is fixedly connected to the bottom of the load box 17. The other end of the damping rod 18 is fixedly connected to a silicone block 19. A compression spring 20 is sleeved on the outer periphery of the damping rod 18. The damping rod 18, the compression spring 20 and the silicone block 19 cooperate to reduce the impact force generated when the UAV lands.

[0035] Working Principle: During use, the fixing method can be selected depending on whether the drone has a support frame. When the drone has no support frame, the mounting mechanism can be fixed to the bottom of the drone using the fixing bolt 3 and connecting plate 2. When the drone has a support frame, pulling the positioning block 6 disengages it from the positioning hole 5, thereby releasing the lock on the support plate 4. Pulling the support plate 4 causes the fixing strip 8 to move. At this time, the position of the fixing strip 8 can be adjusted according to the spacing of the drone support frame. When adjusted to a suitable position, the positioning block 6 is released, and the spring 7 pushes it back to its original position, allowing it to re-engage with the positioning hole 5, thus fixing the support plate 4. By rotating the handle 13, the mounting mechanism can be further secured. The worm gear 12 rotates, which drives the worm wheel 11 to rotate, thereby driving the bidirectional threaded rod 10 to rotate and pushing the slider 14 to move. The slider 14 drives the arc block 15 to move. At this time, the position of the slider 14 can be adjusted according to the size of the drone bracket, so as to facilitate the mounting mechanism to be fixed on the drone. Pull the limit rod 24 to disengage it from the limit hole 23, thereby releasing the lock on the placement box 21. At this time, pull the handle to pull the placement box 21 out of the load-bearing box 17, add different weights of configuration weights into the placement box 21, and put the placement box 21 back into the load-bearing box 17. At this time, the drone load test can be carried out.

[0036] Finally, it should be noted that the above description is only a preferred embodiment of the present utility model and is not intended to limit the present utility model. Although the present utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments or make equivalent substitutions for some of the technical features. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present utility model should be included within the protection scope of the present utility model.

Claims

1. A mounting mechanism for flight tests, comprising a fixing plate (1), characterized in that: A fixing mechanism is installed on the outside of the fixing plate (1), and a counterweight (16) is fixedly connected to the outside of the fixing mechanism. A load-bearing mechanism is installed at the bottom of the fixing plate (1), and a support mechanism is installed at the bottom of the load-bearing mechanism. The fixing mechanism includes a connecting component, a telescopic component, a positioning component and an adjusting component. The telescopic component includes a support plate (4), which is slidably connected inside the fixing plate (1). A fixing strip (8) is fixedly connected to the outside of the support plate (4). A slide rail (9) is provided on the outside of the fixing strip (8). A positioning hole (5) is provided on the outside of the support plate (4).

2. The suspension mechanism of claim 1, wherein: The positioning component includes a positioning block (6), which is slidably connected to the outside of the fixing plate (1). The positioning block (6) and the positioning hole (5) are engaged with each other. A spring (7) is provided inside the fixing plate (1).

3. The mechanism for hanging a test object according to claim 1, wherein: The adjustment assembly includes a bidirectional threaded rod (10), which is rotatably connected inside the fixed bar (8). A worm gear (11) is fixedly connected to the end of the bidirectional threaded rod (10). A worm (12) is rotatably connected inside the fixed bar (8). The worm gear (11) and the worm (12) are interlocked. A handle (13) is fixedly connected to the end of the worm (12). A slider (14) is threadedly connected to the outside of the bidirectional threaded rod (10). An arc block (15) is bolted to the slider (14).

4. The mounting mechanism for flight testing according to claim 1, characterized in that: The connecting assembly includes a connecting plate (2), which is fixedly connected to the top of the fixing plate (1), and a fixing bolt (3) is threadedly connected to the top of the connecting plate (2).

5. The mechanism for hanging a test object according to claim 1, wherein: The load-bearing mechanism includes a load-bearing component, a placement component, and a limiting component. The load-bearing component includes a load-bearing box (17), which is fixedly connected to the bottom of the fixed plate (1). A placement box (21) is slidably connected inside the load-bearing box (17).

6. The mounting mechanism for flight testing according to claim 5, characterized in that: The placement assembly includes a partition (22), which is fixedly connected to the inside of the placement box (21). A handle is fixedly connected to the outside of the placement box (21), and a limit hole (23) is opened on the outside of the placement box (21).

7. The mounting mechanism for flight testing according to claim 6, characterized in that: The limiting component includes a card holder (25), which is fixedly connected to the outside of the load-bearing box (17) and a limiting rod (24) is slidably connected inside the card holder (25). The limiting rod (24) and the limiting hole (23) are engaged with each other, and a spring (26) is provided inside the card holder (25).

8. The mechanism for hanging a test according to claim 5, characterized in that: The load-bearing mechanism also includes a damping rod (18), which is fixedly connected to the bottom of the load-bearing box (17). A silicone block (19) is fixedly connected to the other end of the damping rod (18), and a compression spring (20) is sleeved on the outer periphery of the damping rod (18).

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