The invention provides a backpack type layout low-noise supersonic aircraft, and belongs to the technical field of aircraft structure design, the supersonic aircraft comprises a fuselage, the front section of the fuselage is sequentially provided with a telescopic nose used for reducing noise, a nose motor used for controlling the telescopic nose, an avionics cabin used for containing an avionics system, and a cockpit, a passenger cabin is arranged at the middle section part of the fuselage, and a luggage compartment is arranged at the rear section part of the fuselage; the wings are lambda wings with large sweepback angles, and the lambda wings are arranged at the middle rear section of the fuselage; the engines are installed on wings on the two sides of a fuselage on the back of the aircraft through supporting frames, and gaps are formed between the engines and the wings; and the empennage is mounted on the engine and is of a triangular structure which is swept backwards.
本申请提供了一种背负式布局的低噪声超音速飞机,属于飞行器结构设计技术领域,该超音速飞机包括:机身,所述机身的前段依次设置有用于降噪的可伸缩机头、用于控制所述可伸缩机头的机头电机、用于容纳航电系统的航电舱及驾驶舱,所述机身的中段部分设有客舱,所述机身的后段部分设有行李舱;机翼,所述机翼为大后掠角的λ机翼,所述λ机翼设置在机身的中后段;发动机,所述发动机通过支撑架安装在飞机背部机身两侧的机翼上,且所述发动机与机翼之间具有间隙;尾翼,所述尾翼安装在所述发动机上且呈向后掠的三角形结构。
Backpack layout low-noise supersonic aircraft
一种背负式布局的低噪声超音速飞机
2025-01-14
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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