An injector system for propelling an aircraft. The system includes a diffusion structure and a conduit coupled to the diffusion structure. The duct includes a wall having an opening formed therethrough and configured to introduce a primary fluid generated by the aircraft into the diffusion structure. The airfoil is located in a flow of the primary fluid through the opening to the diffusion structure.

    用于推进飞行器的喷射器系统。该系统包括扩散结构和联接至该扩散结构的管道。该管道包括壁,该壁具有穿过其形成的开口,并构造成将由飞行器产生的主要流体引入扩散结构。翼型位于通过开口到达扩散结构的主要流体的流中。


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    Title :

    Winglet injector configuration


    Additional title:

    小翼喷射器构造


    Contributors:

    Publication date :

    2024-06-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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