发明名称 SEMI-LEVERED LANDING GEAR AND ASSOCIATED METHOD
摘要 <p>A semi -levered landing gear (10) is provided that includes a shock strut (12), a truck beam (18) pivotally connected to the shock strut and a semi -levered landing gear mechanism including at least three links (24, 30a, 30b) configured to angularly orient the truck beam and a truck pitch actuation system (40) 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 (18a) of the truck beam in a lower position relative to the aft end (18b) of the truck beam.</p>
申请公布号 CA2793734(C) 申请公布日期 2015.09.08
申请号 CA20112793734 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
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