一种无人机前轮转弯舵机测试装备

Abstract

本实用新型涉及机械工程与自动化控制技术领域，公开了一种无人机前轮转弯舵机测试装备，包括收纳盒，所述收纳盒的内壁滑动连接有测试器，所述测试器的外壁固定连接有多个限位条，所述测试器的内壁固定连接有两个滑轨，所述滑轨的外壁滑动连接有连接块，两个所述连接块的相近一侧固定连接有电子元件，所述连接块的外壁固定连接有两个阻尼器，所述阻尼器的外壁套设有弹簧，所述电子元件的外壁固定连接有两个连接板一，两个所述连接板一的相远一侧均固定连接有两个转动座一。本实用新型中，从而实现对电子元件的有效减震，缓冲外力冲击，减少震动对电子元件的影响，保护其稳定工作。

Claims

1. A test equipment for unmanned aerial vehicle front wheel turning servo, comprising a storage box (1), characterized in that: The inner wall of the storage box (1) is slidably connected to a tester (2). Multiple limiting strips (3) are fixedly connected to the outer wall of the tester (2). Two slide rails (4) are fixedly connected to the inner wall of the tester (2). Connecting blocks (5) are slidably connected to the outer walls of the slide rails (4). Electronic components (6) are fixedly connected to the adjacent sides of the two connecting blocks (5). Two dampers (7) are fixedly connected to the outer walls of the connecting blocks (5). Springs (8) are sleeved on the outer walls of the dampers (7). The outer walls of the electronic components (6) are fixedly connected to... Two connecting plates (9) are fixedly connected to two rotating seats (10) on opposite sides of each connecting plate (9). A rotating arm (11) is rotatably connected to the outer wall of the rotating seat (10). A rotating arm (12) is rotatably connected to the outer wall of the rotating arm (11). A rotating seat (13) is rotatably connected to the outer wall of the rotating arm (12). A connecting plate (14) is fixedly connected to the outer wall of the two rotating seats (13). A fixing component is provided at the bottom of the storage box (1) to prevent the tester (2) from shaking. 2.The unmanned aerial vehicle front wheel turning rudder machine test equipment according to claim 1, wherein: The fixing component includes a positioning block (15), the top of which is fixedly connected to the bottom of the tester (2), and a positioning frame (16) is slidably connected to the outer wall of the positioning block (15). 3.The unmanned aerial vehicle front wheel turning rudder machine test equipment according to claim 1, wherein: The outer walls of the multiple limiting strips (3) are slidably connected to the inner wall of the storage box (1), and the two dampers (7) are fixedly connected to the inner wall of the tester (2) on opposite sides.

4. The unmanned aerial vehicle front wheel turning rudder machine test equipment according to claim 1, wherein: The outer walls of the two connecting plates (14) are fixedly connected to the inner wall of the tester (2), the two springs (8) are fixedly connected to the outer wall of the connecting block (5) on their adjacent sides, and the outer walls of the multiple springs (8) are fixedly connected to the inner wall of the tester (2).

5. The unmanned aerial vehicle front wheel turning rudder machine test equipment according to claim 2, characterized in that: A motor (17) is fixedly connected to the inner wall of the positioning frame (16), and a gear (18) is fixedly connected to the drive end of the motor (17).

6. The unmanned aerial vehicle front wheel turning rudder machine test equipment according to claim 5, characterized in that: The inner wall of the positioning frame (16) is fixedly connected to a limiting ring (19), and the inner wall of the limiting ring (19) is slidably connected to a limiting post (20).

7. The unmanned aerial vehicle front wheel turning rudder machine test equipment according to claim 6, characterized in that: A rack (21) is fixedly connected to the outer wall of the limiting post (20), and the outside of the rack (21) is meshed with the outside of the gear (18). 8.The unmanned aerial vehicle front wheel turning rudder machine test equipment according to claim 7, characterized in that: The outer wall of the limiting post (20) is slidably connected to the inner wall of the positioning block (15), and the outer wall of the limiting post (20) is slidably connected to the inner wall of the positioning frame (16).

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