The invention provides a telescopic wing, a wing spacing adjusting module, an aircraft and a control method, and the telescopic wing comprises a fixed section, a first telescopic section, a second telescopic section, a first wing telescopic module and a second wing telescopic module; the wing spacing adjusting module comprises a telescopic unit group and a power unit; the aircraft comprises a fuselage, a telescopic wing group, a vertical take-off and landing module group, an aileron group and a wing spacing adjusting module group. According to the invention, the defect of 'dead weight' of a conventional composite wing is eliminated, and the aerodynamic efficiency is high; the control torque is sufficient during vertical take-off and landing, level flight and conversion, the flight is stable, and the wind resistance is good; controllable flight can still be carried out when the engine, the propeller and the aileron part fail, and the reliability is good; the span-chord ratio of the wings and the distance between the wings can be adjusted in a stepless mode, and the control capacity is improved.
本发明提供可伸缩机翼、机翼间距调节模块、飞行器及控制方法,其中,可伸缩机翼包括:固定段、第一伸缩段、第二伸缩段、第一机翼伸缩模块、第二机翼伸缩模块;机翼间距调节模块包括伸缩单元组、动力单元;飞行器包括机身、可伸缩机翼组、垂直起降模块组、副翼组和机翼间距调节模块组。本发明消除了常规复合翼存在的“死重”不足,气动效率高;本发明的操纵力矩在垂直起降、平飞和转换时充足,飞行稳定,抗风性好;本发明可在发动机、螺旋桨和副翼部分失效时仍进行可控飞行,可靠性好;本发明的机翼展弦比和机翼间距均可无级调整,提高了控制能力。
Telescopic wing, wing spacing adjusting module, aircraft and control method
可伸缩机翼、机翼间距调节模块、飞行器及控制方法
2021-08-20
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
European Patent Office | 2021
|Inclined rotating wing aircraft with telescopic wing membranes
European Patent Office | 2015
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