The invention provides a composite brake parachute for an aircraft, and belongs to the technical field of aircraft landing deceleration, the composite brake parachute specifically comprises a first parachute body, a plurality of second parachute bodies, a first connecting rope and a plurality of second connecting ropes, the first parachute body is connected with the tail of the aircraft through the first connecting rope, and the second parachute bodies are mutually connected through the second connecting ropes; the umbrella cloth of the first umbrella body is connected with the umbrella rope of the second umbrella body through a second connecting rope. According to the treatment scheme, the requirement for the structural strength of a single brake parachute material is lowered while the speed reduction effect and reliability of the brake parachute are improved.

    本申请提供了一种飞机用复合减速伞,属于飞机降落减速的技术领域,具体包括第一伞体、多个第二伞体、第一连接绳和多个第二连接绳,所述第一伞体通过第一连接绳连接飞机的尾部,多个第二伞体通过第二连接绳相互连接,所述第一伞体的伞布通过第二连接绳连接一个所述第二伞体的伞绳。通过本申请的处理方案,提高减速伞的减速效果和可靠性的同时,降低对单个减速伞材料结构强度的要求。


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    Title :

    Composite brake parachute for airplane


    Additional title:

    一种飞机用复合减速伞


    Contributors:
    WEI MINGHU (author) / ZHU GUOQIANG (author) / WU JIABIN (author)

    Publication date :

    2025-03-18


    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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