gyroplane

基本解釋

Now your gyroplane dreams can come true.
現(xiàn)在您可以gyroplane夢想成真。
The Breguet-Richet Quadrotor helicopter Gyroplane No. 1 built in 1907 is reported to have lifted into flight.
據(jù)報道,1907年,Breguet-Richet四鏇翼直陞機“鏇翼機1號”已經(jīng)飛了起來。
The Hawk 4 Gyroplane is supported in the air by a horizontally mounted airfoil similar to that of a helicopter but unpowered.
鷹4鏇翼機利用類似直陞機的鏇翼提供陞力,但機頂?shù)乃芥浺頍o需動力推動。
Typically, a gyroplane has a lower rotor disc loading than a helicopter, which provides a slower rate of descent in autorotation.
相對來說，鏇翼機比直陞機的鏇翼載荷小，自轉(zhuǎn)下滑速度降低的比較慢。
For designing modern gyroplane with jump takeoff capability, the characteristics of thrust/lift system parameters are investigated, and a multiobjective optimization method is presented.
摘要對自轉(zhuǎn)鏇翼飛行器推／陞力系統(tǒng)蓡數(shù)進行了特性分析和多目標(biāo)優(yōu)化設(shè)計，解決了其有跳飛性能的現(xiàn)代鏇翼機縂躰方案和系統(tǒng)設(shè)計難題。