发明名称 Mounting device for a turbojet engine
摘要 The turbojet engine suspension system includes a coupling with a main plate (17) connected to a fixed structure, incorporating a vertical stud (26) with an intermediate shoulder (28) set on the main plate, an upper shoulder (35) located above a component (29) of the fixed structure, and a lower shoulder (34) which presses the main plate against the intermediate shoulder. The lower and upper shoulders are formed by nuts on the threaded ends of the stud, the upper nut being fitted with a stop (36). The suspension system can incorporate a second vertical stud connecting the main plate to the fixed structure.
申请公布号 EP1300337(A1) 申请公布日期 2003.04.09
申请号 EP20020292424 申请日期 2002.10.03
申请人 SNECMA MOTEURS 发明人 HUET, PATRICK;PASQUER, FELIX - JEAN-CLAUDE;BREFORT, FRANCOIS
分类号 B64D27/26;(IPC1-7):B64D27/26 主分类号 B64D27/26
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