发明名称 ENGINE MOUNTING STRUCTURE FOR AN AIRCRAFT ENGINE
摘要 The invention concerns a structure for mounting (4) the engine (2) of an aircraft, comprising a rigid structure (10) provided with a structure box (24), said structure further comprising a mounting system (11) interposed between the engine and the rigid structure, said system (11) including in particular a rear engine attachment (8). The invention is characterized in that the rigid structure further comprises a structural block (34) mounted fixedly on the structure box (24) between the latter and the engine, and including an interface for fixing (36) the rear engine attachment (8).
申请公布号 WO2007036520(A2) 申请公布日期 2007.04.05
申请号 WO2006EP66737 申请日期 2006.09.26
申请人 AIRBUS FRANCE;LAFONT, LAURENT;JOURNADE, FREDERIC;DIOCHON, LIONEL 发明人 LAFONT, LAURENT;JOURNADE, FREDERIC;DIOCHON, LIONEL
分类号 F02C7/20;F02C7/14;F02C7/24 主分类号 F02C7/20
代理机构 代理人
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