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。
Variable compression air inlet channel of aircraft propulsion system and method for variable compression of air inlet channel
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
2024-07-26
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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