Invention Grant
- Patent Title: Establishment of laminar boundary layer flow on an aerofoil body
- Patent Title (中): 在机翼上建立层流边界层流
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Application No.: US12448437Application Date: 2007-12-20
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Publication No.: US08172185B2Publication Date: 2012-05-08
- Inventor: Micheal Gaster
- Applicant: Micheal Gaster
- Applicant Address: GB Surrey
- Assignee: Gaster Consultants Ltd
- Current Assignee: Gaster Consultants Ltd
- Current Assignee Address: GB Surrey
- Agency: Carmody & Torrance LLP
- Priority: GB0625612.7 20061221
- International Application: PCT/GB2007/050773 WO 20071220
- International Announcement: WO2008/075106 WO 20080626
- Main IPC: B64C23/06
- IPC: B64C23/06

Abstract:
In order to establish laminar flow on the attachment line (18) of an aerofoil body, a duct entrance (27) is provided on the leading edge of the aerofoil body for receiving spanwise boundary layer flow BLt. The exit (23) of the duct is located spanwise downstream of the duct entrance (27). The boundary layer flow BLt enters the duct (23) and is discharged downstream. The height of the duct entrance (27) above the leading edge of the aerofoil body is greater than the depth of the boundary layer BLt and thus a fresh laminar boundary layer is established on the outer surface (20) of the duct which propagates spanwise along the surface to rejoin the leading edge of the aerofoil body.
Public/Granted literature
- US20100044520A1 Establishment of laminar boundary layer flow on an aerofoil body Public/Granted day:2010-02-25
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