发明名称 Actuating mechanism for use in aircraft electrically-driven seat for moving an offset organ between two positions, has control cable connected to operating arm by a linking mechanism consisting in screw shank sliding in elongated slot
摘要 -NOVELTY : The actuating mechanism includes a control lever (40) consisting in an operating arm (54) and a control arm (46). A control cable (24) is connected, at one end, to the offset organ and, at another end, to the operating arm using a linking mechanism (42). This linking mechanism includes a sliding system consisting in a screw shank (102) sliding in an elongated slot (100) running along the operating arm. The screw is held in place by a nut. -USE : Actuating mechanism for use in an aircraft seat with electric drive for moving an offset organ between two positions. -ADVANTAGE : Allows manual control during power cut or faulty actuator. The offset organ can be actuated without moving the lever by a large distance, and without accidentally disconnecting the actuator.
申请公布号 FR2811393(A1) 申请公布日期 2002.01.11
申请号 FR20000008694 申请日期 2000.07.04
申请人 LABINAL 发明人 GUARALDO DENIS
分类号 F16C1/16;F16C1/22;F16C1/26;F16H61/36;(IPC1-7):F16H21/16;B60N2/44 主分类号 F16C1/16
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