The invention provides an engine conformal jet aircraft, and relates to the technical field of jet aircrafts. The jet aircraft comprises an aircraft body, wings and a multi-branch convergence type turbocharged engine. The engine comprises a plurality of pressurizing pipes and a multi-way pipe. The pressurizing pipes are converged and communicated step by step through a multi-way pipe, and a turbocharging fan is arranged in each pressurizing pipe; an air inlet is formed in the head end of the primary-stage pressurizing pipe, and an air outlet is formed in the tail end of the final-stage pressurizing pipe; the air inlet is located at the front end of the wing, and the air outlet is located at the rear end of the wing; air inlet holes are formed in the front ends of the wings; air outlet holes are formed in the rear ends of the wings; the aircraft is provided with a pressurized turbine duct power system, the speed of airflow jetted by the tail of the aircraft is higher and is far higher than the jet speed of a traditional engine, and the limit flight speed of the aircraft is higher; and the engines are conformally arranged in the wings, so that the aircraft can fully cover the stealth coating, and the stealth and high-speed flight functions of the aircraft are realized.

    本发明提供了一种发动机共形喷气式飞机,涉及喷气式飞机技术领域。所述喷气式飞机包括:机身、机翼和多支路汇合式涡轮增压的发动机;发动机包括:若干增压管和多通管;增压管通过多通管逐级汇合连通,每根增压管内都设置有涡轮增压风扇;初级的增压管头端开设进气口,末级的增压管末端开设有出气口;增压管和多通管平铺在机翼内,进气口位于机翼前端,出气口位于机翼后端;机翼前端开设有进气孔,机翼后端开设有出气孔;所述飞机装备了加压式涡轮涵道动力系统,其尾部喷射的气流速度更快,远高于传统发动机的喷流速度,使得飞机的极限飞行速度更快;且发动机共形设置在机翼内,使得飞机能够全面覆盖隐身涂层,实现了飞机的隐身和高速飞行功能。


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    Titel :

    Engine conformal jet aircraft


    Weitere Titelangaben:

    发动机共形喷气式飞机


    Beteiligte:
    ZHANG YAN (Autor:in) / CHENG XIANGYU (Autor:in)

    Erscheinungsdatum :

    2023-05-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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