The invention belongs to the field of aircraft design, and relates to an embedded air inlet channel. In order to solve the problems that an existing embedded air inlet channel is affected by side edgevortexes, and the performance of the air inlet channel is poor, the invention provides an embedded air inlet channel with a main flow channel and a side edge rotational flow channel, and the embeddedair inlet channel is used for improving the performance of the embedded air inlet channel and the performance of an aircraft using the embedded air inlet channel.

    本发明属于飞行器设计领域,涉及一种埋入式进气道。针对当前埋入式进气道受侧棱漩涡影响,进气道性能差的问题,本发明提出一种主流加侧棱旋流两通道的埋入式进气道,用于改善埋入式进气道的性能以及使用埋入式进气道的飞行器的性能。


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    Titel :

    Embedded air inlet channel and aircraft


    Weitere Titelangaben:

    一种埋入式进气道及飞行器


    Beteiligte:
    WAN LIYING (Autor:in) / AN PING (Autor:in) / LU JIE (Autor:in) / REN ZHIWEN (Autor:in) / ZHAO SHENGHAI (Autor:in) / WANG CHUNLI (Autor:in) / CHEN ZUNJING (Autor:in) / YANG JIABI (Autor:in) / WAN ZHIMING (Autor:in) / XIAO YI (Autor:in)

    Erscheinungsdatum :

    05.02.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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