发明名称 |
LAMINAR FLOW CONTROL SYSTEM AND SUCTION PANEL FOR USE THEREWITH |
摘要 |
A laminar flow control system for incorporation in, for example, an aircraft flying surface includes a suction panel comprising a perforated skin (20, 40) mounted on a base member (60), a plenum chamber (30) being in communication with a plurality of micro channels (90) formed in the top surface of the base member (60), the micro channels (90) being in communication with the holes (40) in the skin (20). |
申请公布号 |
WO0100488(A1) |
申请公布日期 |
2001.01.04 |
申请号 |
WO2000GB02210 |
申请日期 |
2000.06.07 |
申请人 |
BAE SYSTEMS PLC;WILLIAMS, STEWART, WYNN;TURNER, BRIAN, JOHN |
发明人 |
WILLIAMS, STEWART, WYNN;TURNER, BRIAN, JOHN |
分类号 |
B64C1/12;B64C3/26;B64C21/06;F15D1/12 |
主分类号 |
B64C1/12 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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