The invention discloses a double-nose wing body fusion low detectable layout, and belongs to the field of aircraft aerodynamic layouts. The layout comprises a fuselage and wings, the wings are arranged on the two sides of the fuselage, and the layout of a wing body fusion body is formed; the fuselage comprises double heads, a propulsion system, a cabin/satellite penetration cabin, a fuselage rear edge, a fuselage tail, a lifting body fuselage rear edge pitching control surface, a fuselage side edge and a strake wing; the propelling system comprises an engine, an engine air inlet, an engine tail nozzle, an inner pipeline and an infrared signal shielding groove, and the engine air inlet is formed between the double machine heads; the engine tail nozzle is arranged on the upper portion of the rear edge of the fuselage and installed in the infrared signal shielding groove, and the infrared signal shielding groove is used for shielding the engine tail nozzle 24. Radar waves in the range of plus or minus 30 degrees in front of the machine heads are reflected to several non-important directions through arrangement of radar reflecting surfaces and edges between the double machine heads.

    本发明一种双机头翼身融合低可探测布局,属于飞机气动布局的领域;包括机身和机翼,所述机翼设置于机身的两侧,形成翼身融合体的布局;所述机身包括双机头、推进系统、座舱/卫通舱、机身后缘、机身尾部、升力体机身后缘俯仰控制舵面、机身侧缘和边条翼;推进系统包括发动机、发动机进气口、发动机尾喷口、内管道和红外信号屏蔽槽,发动机进气口设置于双机头之间;发动机尾喷口设置于机身后缘的上部,并安装于红外信号屏蔽槽内,红外信号屏蔽槽用于发动机尾喷口24的屏蔽。通过对双机头之间各雷达反射面和棱边的布置将机头正前方正负30°范围内的雷达波反射到几个非重要方向上去。


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    Titel :

    Double-nose wing body fusion low detectable layout


    Weitere Titelangaben:

    一种双机头翼身融合低可探测布局


    Beteiligte:
    MA XIAOHUI (Autor:in) / CAI JINSHENG (Autor:in) / LI WENFENG (Autor:in)

    Erscheinungsdatum :

    2021-07-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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