The propulsion system includes at least one conduit configured to carry and distribute motive fluid, the conduit further configured to contract when no motive fluid is supplied from the compressor and inflate when motive fluid is supplied from the compressor; and at least one ejector in fluid communication with the at least one conduit, where the compressor supplies compressed air to the at least one ejector to generate thrust, and where, when not in use, the at least one ejector is retractable into the volume of the wing to streamline the exterior of the wing.

    推进系统包括:至少一个导管,所述导管配置为承载和分配原动流体,所述导管还配置为当未从压缩机供应原动流体时收缩而当从压缩机供应原动流体时充胀;至少一个引射器,其与至少一个导管流体连通,其中,压缩机向至少一个引射器供应压缩空气以产生推力,并且其中,在不使用时,至少一个引射器可缩回到翼部的体积中,从而使所述翼部的外部流线型化。


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    Title :

    Pneumatic collapsible ejector supply system for aircraft propulsion


    Additional title:

    飞行器推进用气动可折叠引射器供应系统


    Contributors:

    Publication date :

    2025-02-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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