发明名称 SEMI-LEVERED LANDING GEAR AND ASSOCIATED METHOD
摘要 A semi-levered landing gear is provided that includes a shock strut, a truck beam pivotally connected to the shock strut and a semi-levered landing gear mechanism including at least three links configured to angularly orient the truck beam and a truck pitch actuation system operatively connected to at least one of the three links. The landing gear mechanism may be configured to cooperate with an extension of a shock strut by positioning the truck pitch actuator in a retracted position, thereby positioning a forward end of the truck beam in a raised position relative to the aft end of the truck beam. The landing gear mechanism may also be configured to cooperate with a retraction of the shock strut into the wheel well by extending the truck pitch actuator to position a forward end of the truck beam in a lower position relative to the aft end of the truck beam.
申请公布号 KR20130006599(A) 申请公布日期 2013.01.17
申请号 KR20127021625 申请日期 2011.02.23
申请人 THE BOEING COMPANY 发明人 MELLOR MITCHELL L.;LONG MICHAEL A.;ODELL RICHARD B.
分类号 B64C25/34 主分类号 B64C25/34
代理机构 代理人
主权项
地址