Flight control damping structure of unmanned aerial vehicle
Flight control damping structure of unmanned aerial vehicle
The invention relates to an unmanned aerial vehicle flight control damping structure which comprises a lower shell, a lower damping sponge positioning piece, a lower damping sponge, a flight control balancing weight, a flight control plate, an upper damping sponge, an upper damping sponge positioning piece and an upper shell. The device is scientific and reasonable in design, high in structural firmness, capable of being integrally fixed to a main control board, capable of being rapidly assembled, time-saving and labor-saving in installation and suitable for mass production; the influence of vibration of the unmanned aerial vehicle in the horizontal direction and the vertical direction on flight control can be effectively reduced, the damping effect is good, and stable and accurate flight of the unmanned aerial vehicle is guaranteed.
本发明涉及一种无人机飞控减震结构，包括下壳体、下减震海绵定位片、下减震海绵、飞控配重块、飞控板、上减震海绵、上减震海绵定位片及上壳体。本发明设计科学合理，结构牢靠性强，能够整体固定到主控板上，且可快速完成组装，安装省时省力，适合量产；能够时有效降低无人机水平方向和垂直方向的振动对飞控的影响，减震效果良好，保证无人机的稳定精确飞行。
Dokumentinformationen
Flight control damping structure of unmanned aerial vehicle
一种无人机飞控减震结构
2022-11-15
Patent
Elektronische Ressource
Chinesisch
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