A propulsion system for an aircraft includes an engine having a central axis. The cover surrounds the engine and includes a cover lip. A compression ramp is spaced from the cover lip. And an inlet is formed by the cover lip part and the compression slope. The compression ramp is non-planar. The compression ramp may move relative to the shroud lip to vary compression of the inlet airflow through the inlet.

    一种用于飞机的推进系统,其包括具有中心轴线的发动机。罩环绕发动机并且包括罩唇部。压缩斜坡与该罩唇部间隔开。由罩唇部和压缩斜坡形成一入口。压缩斜坡是非平面的。压缩斜坡可以相对于罩唇部移动,以改变通过入口的入口气流的压缩。


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    Title :

    Variable compression air inlet channel of aircraft propulsion system and method for variable compression of air inlet channel


    Additional title:

    飞机推进系统的可变压缩进气道及进气道可变压缩的方法


    Contributors:

    Publication date :

    2024-07-26


    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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