发明名称 Vernier active flow control effector
摘要 Methods and apparatus for controlling the attitude of a mobile platform with a resolution suitable for vernier attitude control. In a preferred 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 preferred 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.
申请公布号 US7255309(B2) 申请公布日期 2007.08.14
申请号 US20040890639 申请日期 2004.07.14
申请人 THE BOEING COMPANY 发明人 BOLDRIN CLETE M.;HASSAN AHMED A.
分类号 B64C21/04 主分类号 B64C21/04
代理机构 代理人
主权项
地址