Invention Grant
- Patent Title: Compression ramp boundary layer removal
- Patent Title (中): 压缩斜坡边界层去除
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Application No.: US13088270Application Date: 2011-04-15
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Publication No.: US09046035B2Publication Date: 2015-06-02
- Inventor: Sevan Megerian , Chandler Clifton
- Applicant: Sevan Megerian , Chandler Clifton
- Applicant Address: US MD Bethesda
- Assignee: Lockheed Martin Corporation
- Current Assignee: Lockheed Martin Corporation
- Current Assignee Address: US MD Bethesda
- Agency: McDermott Will & Emery LLP
- Main IPC: F02B27/00
- IPC: F02B27/00 ; F02K99/00 ; F02C7/057 ; F02K7/10

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.
Public/Granted literature
- US20120260661A1 COMPRESSION RAMP BOUNDARY LAYER REMOVAL Public/Granted day:2012-10-18
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