发明名称 Wing unit airfoil structure
摘要 <p>The wing unit (12) has a ridge (6) bulging outwardly in a top skin (4), and a ridge (7) bulging in a bottom skin (5). The ridges begin in an area (9) of a trailing edge (2), and extend toward the leading edge (1) in the direction of a depth axis (8). Each ridge has a height that is largest in the trailing edge area, and diminishing from the trailing edge area toward the leading edge. The top skin and bottom skin are supported by an inner structure between the trailing and leading edges. The depth axis extends perpendicularly to and between the leading and trailing edges.</p>
申请公布号 EP1522492(A1) 申请公布日期 2005.04.13
申请号 EP20030025295 申请日期 2003.11.06
申请人 AIRBUS DEUTSCHLAND GMBH 发明人 BURCHARD, ALEXANDER, DIPL.-ING.
分类号 B64C1/00;B64C3/26;B64C9/00;(IPC1-7):B64C9/00 主分类号 B64C1/00
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