The invention provides a wing spacing adjusting module, an aircraft comprising the wing spacing adjusting module and an aircraft control method. The wing spacing adjusting module comprises a telescopic unit group and a power unit, the aircraft comprises a wing spacing adjusting module group consisting of wing spacing adjusting modules, a first wing, a second wing, a fuselage, a vertical take-off and landing module group and an aileron group, the flight control method comprises steps that the aircraft is controlled in the processes of vertical take-off and landing, level flight, hovering, conversion from vertical take-off to level flight and conversion from vertical take-off to level flight. According to the method, the defect of dead weight of a conventional composite wing is eliminated, and aerodynamic efficiency is high; the control torque is sufficient during vertical take-off and landing, level flight and conversion, the flight is stable, and good wind resistance is achieved; controllable flight can still be carried out when the engine, the propeller and the aileron part fail, and good reliability is achieved; a distance between the wings can be adjusted in a stepless mode, and the control capacity of the vertical take-off and landing process, the level flight process and the conversion whole flight process is improved.
本发明提供机翼间距调节模块、包含其的飞行器及飞行器控制方法,其中,机翼间距调节模块包括伸缩单元组、动力单元;飞行器包括由机翼间距调节模块组成的机翼间距调节模块组、第一机翼、第二机翼、机身、垂直起降模块组、副翼组;飞行控制方法包括对飞行器垂直起降、平飞、悬停、从垂直起飞转换至平飞和从垂直起飞转换至平飞过程中对飞行器进行控制。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;本发明的机翼间距可无级调整,提高了垂直起降、平飞及转换全飞行过程的控制能力。
Wing spacing adjusting module, aircraft comprising wing spacing adjusting module and aircraft control method
机翼间距调节模块、包含其的飞行器及飞行器控制方法
2021-09-21
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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