发明名称 Attachment of a helicopter landing gear
摘要 The invention is related to a bracket (24) for connecting a traverse (20) of a landing gear to a cabin of a helicopter. A landing gear retainer (5) is fixed around the traverse (20) coaxially to the longitudinal direction of the traverse (20) and at least one cabin clamp mount (7) is fixed to the cabin. The landing gear retainer (5) is in between the cabin and upper and lower pendulum bolts (12, 13) and upper and lower pendulum bearings (18, 19). A pendulum (9) is in longitudinal direction of the traverse (20) hinged to the landing gear retainer (5). The invention is further related to an application of such brackets (24).
申请公布号 EP2853488(A1) 申请公布日期 2015.04.01
申请号 EP20130400020 申请日期 2013.09.30
申请人 AIRBUS HELICOPTERS DEUTSCHLAND GMBH 发明人 VON-WILMOWSKY, KASPAR;MARKMILLER, JOHANNES
分类号 B64C25/52 主分类号 B64C25/52
代理机构 代理人
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