Invention Grant
US09046035B2 Compression ramp boundary layer removal 有权
压缩斜坡边界层去除

Compression ramp boundary layer removal
Abstract:
An inlet for removal of a boundary layer from an incoming air flow of an engine is disclosed. The inlet includes at least one compression element proximate to an inlet aperture of the engine. The compression element is selectably moveable between a first position and a second position along an axis. A boundary layer removal aperture is open when the compression element is in the first position and the boundary layer removal aperture is closed when the compression element is in the second position.
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