The invention discloses a combined power aircraft, relates to the technical field of power aircrafts, and aims to solve the problem that in the prior art, a power system of a high-speed aircraft cannot instantly obtain large longitudinal acceleration, so that strike to an air missile weapon system cannot be effectively escaped, or the speed of sound cannot be quickly spanned. The power system comprises an engine and a rocket booster; the rocket booster is used for assisting an aircraft in obtaining large short-time longitudinal acceleration and normal acceleration. The rocket booster is applied to the aircraft, so that the aircraft can obtain instantaneous large longitudinal acceleration, and the aircraft can avoid strike of air defense weapons or achieve short-time supersonic speed.

    本发明公开了一种组合动力飞机,涉及动力飞机技术领域,用于解决现有技术中高速飞机的动力系统不能瞬时获得较大的纵向加速度,从而不能有效逃脱对空导弹武器系统的打击,或者快速的跨越声速的问题,本发明包括动力系统,所述动力系统包括发动机和火箭助推器;所述火箭助推器用于辅助飞机获得较大的短时纵向加速度和法向加速度。本发明通过将火箭助推器运用于飞机上,可以使飞机获得瞬时很大的纵向加速度,从而可以让飞机躲避防空武器的打击或者实现短时超音速。


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    Title :

    Combined power aircraft


    Additional title:

    一种组合动力飞机


    Contributors:
    YU HONGYONG (author) / SONG YONG (author) / LIU FUPING (author) / LI SHIQIU (author) / TONG KAI (author) / LI XIAOFEI (author) / LIU BO (author) / RAO LUO (author)

    Publication date :

    2022-03-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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