发明名称 Auxiliary nose landing gear, support structure and rotorcraft
摘要 <p>The gear has a wheel (4) rotating around a rolling axle (47) of a rolling assembly (46), where the axle is arranged on an oscillatory system (13) via an intermediary of a turning pivot (54). The pivot has a bearing axle (53) intersecting with the rolling axle and turns the wheel on both sides of a position corresponding to the rolling of a rotorcraft in a straight line using a turning actuator (55). A shock absorbing jack (9) has a retraction unit of the oscillatory system above the position of an end stop of a damping displacement.</p>
申请公布号 EP1714870(A1) 申请公布日期 2006.10.25
申请号 EP20060008040 申请日期 2006.04.19
申请人 EUROCOPTER 发明人 BIETENHADER, CLAUDE
分类号 B64C25/14;B64C25/04 主分类号 B64C25/14
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