Invention Grant
- Patent Title: Vernier active flow control effector
- Patent Title (中): 游标主动流量控制效应器
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Application No.: US11736721Application Date: 2007-04-18
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Publication No.: US08128036B2Publication Date: 2012-03-06
- Inventor: Clete M. Boldrin , Ahmed A. Hassan
- Applicant: Clete M. Boldrin , Ahmed A. Hassan
- Applicant Address: US IL Chicago
- Assignee: The Boeing Company
- Current Assignee: The Boeing Company
- Current Assignee Address: US IL Chicago
- Agency: Harness, Dickey & Pierce, P.L.C.
- Main IPC: B64C21/04
- IPC: B64C21/04 ; B64C21/06

Abstract:
Methods and apparatus for controlling the attitude of a mobile platform with a resolution suitable for vernier attitude control. In one embodiment a method includes flowing fluid through an orifice of an aerodynamic surface. The method also includes modifying a boundary layer of the aerodynamic surface with the flowing fluid. Another embodiment provides an aerodynamic member of a mobile platform. The aerodynamic member includes an aerodynamic surface, an orifice, an actuator, and a fluid moving member. The orifice is in the aerodynamic surface and the actuator is subject to friction and backlash. The fluid moving member communicates with the orifice and causes the fluid to flow through the orifice to modify the boundary layer of aerodynamic surface.
Public/Granted literature
- US20090321580A1 VERNIER ACTIVE FLOW CONTROL EFFECTOR Public/Granted day:2009-12-31
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