An aircraft defining a longitudinal direction and a transverse direction is provided. The aircraft comprises: a fuselage; an engine mounted at a position spaced apart from a fuselage of the aircraft, the engine including rotor blades; and at least one fuselage shroud removably coupled to the fuselage at a location aligned with the rotor blade in the lateral direction.

    提供一种限定纵向方向和横向方向的飞行器。该飞行器包括:机身;发动机,该发动机安装在与飞行器的机身间隔的位置处,该发动机包括转子叶片;以及至少一个机身护罩,该至少一个机身护罩在沿横向方向与转子叶片对准的位置处可去除地联接到机身。


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    Title :

    Removable fuselage shroud for aircraft


    Additional title:

    用于飞行器的可去除机身护罩


    Contributors:
    D W CLARR (author) / N J CARRE (author) / D D WORDE (author) / B W MILLER (author)

    Publication date :

    2021-04-16


    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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