发明名称 Drain in particular for engine pylon support
摘要 The drain has a rectangular section placed in a plane parallel to a trailing edge (6) of a rear secondary structure (RSS) of a strut. The drain is closed at one of its outer end by a terminal part (19). The drain is symmetrical with respect to a vertical plane containing the trailing edge. A draining opening (12) is elongated on one of its opposite lateral walls (11a, 11b).
申请公布号 EP1544106(A1) 申请公布日期 2005.06.22
申请号 EP20040106283 申请日期 2004.12.03
申请人 AIRBUS FRANCE 发明人 BONNAUD, CYRIL
分类号 B64C1/14;B64D27/00;B64D29/02;(IPC1-7):B64D27/00 主分类号 B64C1/14
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