发明名称 Aircraft jet engine suspension system has bars extended beyond beam and connected to master component by articulated joints
摘要 The suspension system, comprising a fixed structure with a pair of bars (9, 10) between front and rear couplings, the rear coupling being in the form of a master component (17) and a pivoted beam (15), has the bars extended beyond the beam and connected to the master component by articulated joints (20, 21). The joints have sufficient clearance to remain inactive until their is a failure in one of the bars or in the rear coupling. In addition, the master component and fixed structure are connected by a vertical stud with a shoulder and top and bottom nuts.
申请公布号 FR2830515(A1) 申请公布日期 2003.04.11
申请号 FR20010012735 申请日期 2001.10.04
申请人 SNECMA MOTEURS 发明人 HUET PATRICK;BREFORT FRANCOIS;PASQUER FELIX JEAN CLAUDE
分类号 B64D27/26;(IPC1-7):B64D27/26 主分类号 B64D27/26
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