The invention discloses an aircraft aerodynamic layout efficiency risk coping method and application, and relates to the field of aircraft manufacturing. Wherein the aerodynamic layout of the aircraft comprises wing layout, fuselage layout, engine types, engine layout and aerodynamic layout of the aircraft; the aerodynamic layout efficiency method of the aircraft comprises the steps of engine hanging limit, flight aerodynamic balance and efficiency maximization, wherein the wing roots are in front, the two sides of the wing roots, the belly is in back and the belly is in front; the aircraft aerodynamic layout efficiency coping method comprises the steps of flight speed limitation, flight speed control, a coping method and pilot operation rule guidance. According to the coping method, an artificial mechanical driving system is immediately used, the flight speed of the aircraft is reduced, an operating rod is pressed downwards, the aircraft achieves pneumatic balance again, accordingly, wings generate lift force, the aircraft is balanced, then the operating rod is pulled, the aircraft enters a horizontal flight state, and the aircraft enters a normal flight state.
本发明公开了一种飞机气动布局效率风险的应对方法与应用,涉及到飞机制造领域。其中,飞机气动布局包括机翼布局,机身布局,发动机种类,发动机布局,飞机气动布局;飞机气动布局效率方法包括翼根靠前,翼根两侧,腹部靠后,腹部靠前的发动机吊挂极限,飞行气动平衡,效率最大化;飞机气动布局效率应对方法包括飞行速度限制,飞行速度控制,应对方法,飞行员操作守则指引;所述应对方法是立即使用人工机械驾驶系统,降低飞机飞行速度,把操纵杆往下压,让飞机重新实现气动平衡,从而让机翼产生升力,使飞机平衡,然后拉操纵杆让飞机进入水平飞行状态,飞机进入正常飞行。
Aircraft aerodynamic layout efficiency risk coping method and application
飞机气动布局效率风险的应对方法与应用
2023-12-08
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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