发明名称 Landing gear
摘要 An auxiliary actuator mechanism includes a lever, a spring unit and a control linkage. The lever is pivotally connected to the upper portion of a main shock absorber strut, and pivotable between an upper position for take-off, and a lower position. The spring unit is pivotally connected at an upper end to the lever and at a lower end to the bogie at an auxiliary pivot forward of the main pivot. The control linkage is connected between the lever and the upper portion of the main shock absorber strut to define the upper predetermined position of the lever. The control linkage is connectable to an anchor point that moves relative to the upper portion of the main shock absorber strut during stowing, and is operated by initial stowing movement of the stowing mechanism to lower the lever from the upper position to a stowing position.
申请公布号 US8376272(B2) 申请公布日期 2013.02.19
申请号 US201113333138 申请日期 2011.12.21
申请人 MESSIER-DOWTY LIMITED;BENNETT IAN;LANG RICHARD CHARLES;MENEZES ROBERT ANTHONY 发明人 BENNETT IAN;LANG RICHARD CHARLES;MENEZES ROBERT ANTHONY
分类号 B64C25/26;B64C25/22;B64C25/34;B64C25/58;B64C25/60;B64C25/62 主分类号 B64C25/26
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