发明名称 Laminar flow skin.
摘要 <p>Apparatus for the control of boundary layer fluids by a suction technique, the said apparatus being adapted to form part of or attach to a fluid dynamic surface and comprising; a sandwich skin material (2) consisting of at least two layers, an outer layer of which is in use positioned adjacent to the boundary layer fluid, the said layers of material bounding internal intercommunicating passageways to allow in use the movement of fluid to substantially all areas within the material, the outer layer being provided with a plurality of holes (4) communicating with the internal passageways (6) of the said sandwich skin material and a plurality of hoods (8) or steps being fixedly attached to the outer layer of the material located such that in use said hoods (8) or steps are downstream of said plurality of holes (4) and each upstream of and shielding an opening in said outer layer and communicating with at least one of said internal intercommunicating passageways (6).</p>
申请公布号 EP0679572(A2) 申请公布日期 1995.11.02
申请号 EP19950302749 申请日期 1995.04.26
申请人 BRITISH AEROSPACE PUBLIC LIMITED COMPANY 发明人 SEYFANG, GEORGE R., BRIT. AEROSPACE DEF. LTD.
分类号 B64C21/02;B64C21/06;B64C21/08;B64C23/00;(IPC1-7):B64C21/06 主分类号 B64C21/02
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