公开(公告)号：US20120260661A1

公开(公告)日：2012-10-18

申请号：US13088270

申请日：2011-04-15

Applicant: Sevan Megerian ,  Chandler Clifton

Inventor： Sevan Megerian ,  Chandler Clifton

IPC: F02C7/057

CPC classification number: F02C7/057 ,  F02K7/10 ,  F05D2270/17 ,  Y10T137/0536

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.

Abstract translation: 公开了用于从引擎的进入空气流中移除边界层的入口。 入口包括靠近发动机的入口孔的至少一个压缩元件。 压缩元件可选地沿着轴线在第一位置和第二位置之间移动。 当压缩元件处于第一位置时，边界层去除孔开放，并且当压缩元件处于第二位置时，边界层去除孔关闭。

公开(公告)号：US09046035B2

公开(公告)日：2015-06-02

申请号：US13088270

申请日：2011-04-15

Applicant: Sevan Megerian ,  Chandler Clifton

Inventor： Sevan Megerian ,  Chandler Clifton

IPC: F02B27/00 ,  F02K99/00 ,  F02C7/057 ,  F02K7/10

CPC classification number: F02C7/057 ,  F02K7/10 ,  F05D2270/17 ,  Y10T137/0536

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.

Abstract translation: 公开了用于从引擎的进入空气流中移除边界层的入口。 入口包括靠近发动机的入口孔的至少一个压缩元件。 压缩元件可选地沿着轴线在第一位置和第二位置之间移动。 当压缩元件处于第一位置时，边界层去除孔开放，并且当压缩元件处于第二位置时，边界层去除孔关闭。