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Unmanned aerial vehicle aging test platform

An aging test, UAV technology, applied in the field of UAV, can solve the problems of time-consuming and laborious, complicated manual take-off test operation, low test accuracy, etc., to achieve the effect of high efficiency, accurate aging and performance.

Inactive Publication Date: 2021-04-27
北京共创晶桔科技服务股份有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to provide a UAV aging test platform to solve the problems in the prior art that the manual take-off test operation is complex, time-consuming and labor-intensive, and the accuracy of the test is low

Method used

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  • Unmanned aerial vehicle aging test platform
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  • Unmanned aerial vehicle aging test platform

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Embodiment

[0019] see Figure 1-3 , the present invention provides a technical solution: a UAV aging test platform, including a platform base 1, the two ends of the top surface of the platform base 1 are provided with a vertically upward side shell 2, and a guide cavity 3 is opened in the side shell 2 Specifically, the guide cavities 3 of the two side shells 2 are arranged oppositely, and the top of the guide cavities 3 is provided with a top cover 4 detachably connected with the side shells 2. Specifically, the top cover 4 and the top of the side shells 2 are connected by bolts , a mount 8 is provided between the side shells 2, and the top surface of the mount 8 is detachably connected to the drone body 9. Specifically, the bottom surface of the drone body 9 is connected to the mount 8 by bolts, and the two sides of the mount 8 A support seat 5 is provided, and a torque sensor 11 is connected between the support seat 5 and the mounting seat 8. Specifically, one end of the torque sensor ...

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Abstract

The invention relates to an unmanned aerial vehicle aging test platform which comprises a platform base, vertically upward side shells are arranged at the two ends of the top surface of the platform base, guide cavities are formed in the side shells, top covers detachably connected with the side shells are arranged at the top ends of the guide cavities, and a mounting base is arranged between the side shells. A test mechanism is used for supporting a supporting seat, a stop table is used for positioning a spring, and the spring is used for carrying out bidirectional elastic supporting on the supporting seat, so that an unmanned aerial vehicle body moves upwards and downwards to compress the springs above and below respectively, and power can act on a guide cylinder through the stop table; the power and the change of the power in the ascending and descending processes are tested through pressure sensors above and below respectively, the mounting base is positioned and mounted through a torque sensor, and then the power of lateral flight and steering of the unmanned aerial vehicle body is tested through the torque sensor. Therefore, the aging and use performance of the unmanned aerial vehicle body can be tested more efficiently and accurately.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to an aging test platform for unmanned aerial vehicles. Background technique [0002] Unmanned aircraft, referred to as "UAV", is an unmanned aircraft controlled by radio remote control equipment and its own program control device. There is no cockpit on board, but equipment such as autopilot and program control device are installed. The personnel on the ground, on the ship, or at the remote control station of the parent aircraft track, locate, remotely control, telemeter and digitally transmit it through radar and other equipment. Under the radio control, it can take off like an ordinary aircraft or be launched into the air with a booster rocket, and it can also be taken into the air by the parent aircraft for flight. When recovering, it can automatically land in the same way as the common aircraft landing process, and can also be recovered by remote control with...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F5/60
CPCB64F5/60
Inventor 吴海涛
Owner 北京共创晶桔科技服务股份有限公司