The invention discloses a scissor-type folding airfoil without a power source, an unfolding method of the scissor-type folding airfoil and an aircraft, belongs to the technical field of aircraft design, and aims to simplify the structure of the folding airfoil and improve the unfolding speed and stability of the airfoil. A first airfoil of the folding airfoil has a first centroid offset by a predetermined distance with respect to an axis passing through a center of the rotating shaft in a length direction of the first airfoil; a second airfoil of the folding airfoil has a second centroid offset by a predetermined distance with respect to an axis passing through the center of the rotating shaft in the length direction of the second airfoil such that when the upper airfoil and the lower airfoil are in a folded state, the first centroid and the second centroid are arranged substantially symmetrically on both sides of an axis passing through the center of the rotating shaft in the length direction of the two airfoils. Overload force of the launching initial section is fully utilized, and the folding airfoil has the advantages of being simple in structure and light in weight.
本发明公开了一种无动力源剪刀式折叠翼面及其展开方法、飞行器,属于飞行器设计技术领域,旨在简化折叠翼面结构,提高翼面展开速度和稳定性。折叠翼面的第一翼面具有第一质心,该第一质心相对于沿第一翼面长度方向经过转轴中心的轴线偏移预定距离;第二翼面具有第二质心,该第二质心相对于沿第二翼面长度方向且经过转轴中心的轴线偏移预定距离,使得上翼面与下翼面处于折叠状态时,第一质心与第二质心基本对称地布置在沿两翼面长度方向经过转轴中心的轴线两侧。本发明充分利用发射初段的过载力,具有结构简单、重量轻的特点。
Scissor type folding airfoil without power source, unfolding method of scissor type folding airfoil and aircraft
一种无动力源剪刀式折叠翼面及其展开方法、飞行器
2020-05-08
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
European Patent Office | 2022
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