发明名称 METHOD FOR FIXING AN ENGINE STRUT TO AN AIRPLANE WING
摘要 The inventive fixing system comprises a front attachment (6), a rear attachment (7) and an intermediate attachment (8) connecting a strut (1) to a wing (2), wherein the lower fitting (17) of the rear attachment (7) is fixedly connected to the transversal rear face (1G) of said strut on the extension thereof and said lower fitting (17) is substantially in flush with the top face of the strut.
申请公布号 US2009108127(A1) 申请公布日期 2009.04.30
申请号 US20050719891 申请日期 2005.11.17
申请人 AIRBUS FRANCE 发明人 CAZALS OLIVIER
分类号 B64D27/26 主分类号 B64D27/26
代理机构 代理人
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