Wind resistance simulation equipment for unmanned aerial vehicle

By integrating the testing mechanism with the tracked intelligent vehicle, the drone and the equipment can move synchronously along the same trajectory and at the same speed. This solves the problem that existing equipment cannot cover all working conditions and enables comprehensive wind resistance performance testing of drones in real environments, improving safety and the comprehensiveness of the testing.

CN122059097APending Publication Date: 2026-05-19BEIJING LINGYUN FLIGHT CONTROL TECHNOLOGY CO LTD
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Patent Information

Application Number
CN202610493195.0
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2026-04-15
Publication Date
2026-05-19

AI Technical Summary

Technical Problem

Existing drone wind resistance testing equipment cannot fully cover all working conditions during actual drone operations, leading to misleading test data that fails to reflect the drone's wind resistance performance in real-world environments, posing a safety hazard.

Method used

Design a wind resistance simulation device for unmanned aerial vehicles (UAVs). By integrating the testing mechanism onto a track-guided intelligent vehicle, the device enables the UAV and the testing mechanism to move synchronously along the same trajectory and at the same speed. It covers all-directional flight scenarios, including flight path cruising, maneuvering flight, crosswind, headwind, and tailwind. It can also simulate complex environments, such as wind, rain, and debris scenarios. The device employs a multi-wind turbine array and a dynamic wind field control system.

Benefits of technology

It enables real-world wind resistance performance testing of drones under fully dynamic operating conditions, avoiding safety accidents caused by misleading data, improving the safety and comprehensiveness of the test, and adapting to the operational needs of drones in complex environments.

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Abstract

The invention belongs to the technical field of unmanned aerial vehicle testing, and particularly relates to unmanned aerial vehicle wind resistance simulation equipment. Comprising a testing mechanism; the testing mechanism comprises a top frame and a bottom frame; the top frame and the bottom frame are fixed through two stand columns. First mounting frames are uniformly arranged between the two stand columns on the same side; first fans which are uniformly arranged are mounted in the first mounting frame; an arc plate is mounted on the left side of the stand column on the left side; second mounting frames are uniformly arranged between the two arc plates; second fans which are uniformly arranged are mounted in the second mounting frame; a platform is arranged in the middle of the bottom frame, and an unmanned aerial vehicle needing to be tested is placed on the platform; an electric push rod is mounted at the bottom of the platform, and the other side of the electric push rod is mounted at the top of the rail intelligent trolley; by arranging the testing mechanism, all-working-condition scenes such as route cruise, maneuvering flight, crosswind, headwind and downwind all-directional flight and the like in the real operation process of the unmanned aerial vehicle can be completely covered.
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