发明名称 NUT SYSTEM AND AIRCRAFT ENGINE MOUNTING STRUCTURE COMPRISING SAME
摘要 The invention concerns a nut system (100) comprising a nut (104) provided with a main thread (106) of pitch p1 and arranged along a screwing axis (108) of the nut. The invention is characterized in that it further comprises a threaded member (116) coupled in rotation with the screw, said threaded member including a secondary thread (122) not screwed on the main thread (106) from which it is spaced apart, the secondary thread being arranged along the screwing axis and being provided with a pitch p2 different from p1. The invention is applicable to a device for absorbing thrust loads generated by an aircraft engine.
申请公布号 CA2624476(A1) 申请公布日期 2007.04.19
申请号 CA20062624476 申请日期 2006.10.10
申请人 AIRBUS FRANCE 发明人 LEVERT, STEPHANE
分类号 B64D27/26 主分类号 B64D27/26
代理机构 代理人
主权项
地址