The invention provides an aero-engine and an aircraft. The aero-engine comprises a body with an air compression device; the annular installation part is arranged at the end of the body, an installation cavity is formed in the installation part, an air inlet channel is formed in an inner hole of the installation part, the air outlet side of the air inlet channel is communicated with the air inlet side of the air compression device, an air injection through hole is formed in the side, facing the air inlet channel, of the installation part, and an auxiliary through hole is formed in the side, back to the air inlet channel, of the installation part. The air injection through hole is communicated with the auxiliary through hole through the mounting cavity; and the control device is arranged in the mounting cavity. The aero-engine not only is simple in structure, but also is applied to an aircraft, and the control device can be well cooled in a ground test run mode and a flight mission mode.

    本文提供一种航空发动机及飞行器。航空发动机包括:具有压气装置的本体;环形的安装件,设于本体的端部,安装件的内部具有安装腔,安装件的内孔形成进气通路,进气通路的出气侧与压气装置的进气侧连通,安装件的朝向进气通路的一侧设有空气引射通孔、背向进气通路的一侧设有辅助通孔,空气引射通孔和辅助通孔通过安装腔相连通;和控制装置,设于安装腔内。该航空发动机,不仅结构简单,而且应用于飞行器,地面试车模式和飞行任务模式均能够实现对控制装置进行很好地散热。


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    Titel :

    Aero-engine and aircraft


    Weitere Titelangaben:

    一种航空发动机及飞行器


    Beteiligte:
    FAN PING (Autor:in) / DONG KUN (Autor:in) / HOU XIAOCHUN (Autor:in) / DONG TIANLONG (Autor:in) / JING MINGMING (Autor:in)

    Erscheinungsdatum :

    30.12.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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