发明名称 Improvements in or relating to aerofoils
摘要 An aerofoil has a body (14), and at least one flow control device, the flow control device including a passage (22) within the body (14) of the aerofoil, and a passage outlet (21) at an upper aerofoil surface (18) of the aerofoil, whereby in use, air from the passage (22) passes through the passage outlet (21) to affect airflow over the upper surface (18) of the aerofoil over at least a range of incidence angles, wherein the passage outlet (21) is provided by an outlet fitting (24) which is secured relative to the upper surface (18) of the aerofoil, the outlet fitting including a surface part (25) which lies contiguously with the surrounding upper aerofoil surface (18) so there is no or only a minimal discontinuity where the surface part (25) and the surrounding upper aerofoil surface (18) interface, the surface part (25) of the fitting further including an opening (21) which communicates with the passage (22) within the body (14) of the aerofoil. <IMAGE>
申请公布号 EP1577212(A3) 申请公布日期 2005.12.21
申请号 EP20040022521 申请日期 2004.09.22
申请人 WESTLAND HELICOPTERS LIMITED 发明人 DUNN, SHAUN STEPHEN
分类号 B64C27/467;B64C21/02;B64C21/04;B64C23/06;B64C27/46 主分类号 B64C27/467
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