The invention discloses an aircraft system based on missile power propulsion. A missile power propulsion aircraft is composed of an aircraft body, wings, an aircraft flight control system, a missile power system, a missile flight control system and a switcher, wherein the aircraft flight control system, the missile power system, the missile flight control system and the switcher are arranged in the aircraft body. When an aircraft flight power control network of the aircraft flight control system is connected with the missile power system, and when the aircraft flight power control network of the aircraft flight control system is connected to the missile power system, the whole system works in a missile power propulsion state; the aircraft flight control system controls the power of the missile, the power of the missile is used for helping the aircraft to take off quickly, and when the power of the aircraft breaks down, the power of the missile can help the aircraft to keep the flight height emergently. Through reuse of the thrust of the missile, the aircraft is helped to achieve power backup, and when the main engine of the aircraft breaks down, the aircraft is helped to break awayfrom a dangerous stall state, and the thought of reuse of missile power is achieved.

    本发明公开了一种基于导弹动力推进的飞机系统,所述导弹动力推进飞机由机身、机翼和机身内部的飞机飞行控制系统、导弹动力系统、导弹飞行控制系统以及切换器组成。当飞机飞行控制系统的飞机飞行动力控制网络和导弹动力系统连接,当飞机飞行控制系统的飞机飞行动力控制网络连入到导弹动力系统时,整个系统工作在导弹动力推进状态;飞机飞行控制系统控制导弹的动力,利用导弹的动力帮助飞机实现快速的起飞,在飞机本身动力发生故障时,导弹的动力还可以应急帮助飞机保持飞行高度。本发明通过导弹的推力的复用,帮助飞机实现动力备份,在飞机主发动机故障时,帮助飞机脱离危险的失速状态,实现导弹动力的复用的思想。


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    Titel :

    Aircraft system based on missile power propulsion


    Weitere Titelangaben:

    一种基于导弹动力推进的飞机系统


    Beteiligte:
    LI CHANGQI (Autor:in)

    Erscheinungsdatum :

    2021-02-12


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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