公开(公告)号：US07984879B2

公开(公告)日：2011-07-26

申请号：US11995233

申请日：2007-08-31

申请人： Michael Victor Cook ,  Clyde Warsop

发明人： Michael Victor Cook ,  Clyde Warsop

IPC分类号： B64C21/04

CPC分类号： B64C9/38 ,  B64C15/14

摘要： A flow control actuator 10 for a body exposed to fluid flow comprises first and second flow surfaces 14, 16 spaced to define an elongate gap 20 therebetween. An elongate control element is disposed in or adjacent the gap and has an externally facing arcuate surface and defines a first slot 24 between the control element and said first flow surface and a second slot between said control element and said second flow surface 26. The control element 22 is moveable to allow the width of said slots to be adjusted generally proportionally. The flow of pressurized flow control fluid passes from a plenum chamber 30 out through one or both slots 24, 26 to be deflected around the arcuate surface under the influence of the Coanda effect. The flow control actuator 10 may be provided in the trailing or leading edge of an aerofoil; alternatively it may be provided between two surfaces spaced to provide said gap but otherwise providing a generally continuous surface.

摘要翻译： 用于暴露于流体流动的主体的流量控制致动器10包括间隔开的第一和第二流动表面14,16，以在其间限定细长间隙20。 细长的控制元件设置在间隙中或邻近间隙并且具有外部面对的弓形表面并且在控制元件和所述第一流动表面之间限定第一槽24和在所述控制元件和所述第二流动表面26之间的第二槽。控制 元件22可移动以允许所述槽的宽度大致成正比地调节。 加压流量控制流体的流动从通风室30通过一个或两个狭槽24,26，在柯恩达效应的影响下绕弧形表面偏转。 流量控制致动器10可以设置在机翼的后缘或前缘中; 或者可以在间隔开的两个表面之间提供以提供所述间隙，但是另外提供大致连续的表面。

公开(公告)号：US20090050734A1

公开(公告)日：2009-02-26

申请号：US11995233

申请日：2007-08-31

申请人： Michael Victor Cook ,  Clyde Warsop

发明人： Michael Victor Cook ,  Clyde Warsop

IPC分类号： B64C13/00

CPC分类号： B64C9/38 ,  B64C15/14

摘要： A flow control actuator 10 for a body exposed to fluid flow comprises first and second flow surfaces 14, 16 spaced to define an elongate gap 20 therebetween. An elongate control element is disposed in or adjacent the gap and has an externally facing arcuate surface and defines a first slot 24 between the control element and said first flow surface and a second slot between said control element and said second flow surface 26. The control element 22 is moveable to allow the width of said slots to be adjusted generally proportionally. The flow of pressurised flow control fluid passes from a plenum chamber 30 out through one or both slots 24, 26 to be deflected around the arcuate surface under the influence of the Coanda effect. The flow control actuator 10 may be provided in the trailing or leading edge of an aerofoil; alternatively it may be provided between two surfaces spaced to provide said gap but otherwise providing a generally continuous surface.

摘要翻译： 用于暴露于流体流动的主体的流量控制致动器10包括间隔开的第一和第二流动表面14,16，以在其间限定细长间隙20。 细长的控制元件设置在间隙中或邻近间隙并且具有外部面对的弓形表面并且在控制元件和所述第一流动表面之间限定第一槽24和在所述控制元件和所述第二流动表面26之间的第二槽。控制 元件22可移动以允许所述槽的宽度大致成正比地调节。 加压流量控制流体的流动从通风室30通过一个或两个狭槽24,26，在柯恩达效应的影响下绕弧形表面偏转。 流量控制致动器10可以设置在机翼的后缘或前缘中; 或者可以在间隔开的两个表面之间提供以提供所述间隙，但是另外提供大致连续的表面。