发明名称 LEVIER DE COMMANDE D'UNE VOILURE TOURNANTE, SYSTEME DE COMMANDE MECANIQUE MUNI DUDIT LEVIER, ET AERONEF
摘要 A control lever (10) provided with a stick (11) extending axially from a stand (11′) towards grip means (11″) and with a carrier structure (20) for said stick (11) that is hinged about a first hinge axis (AX1) and about a second hinge axis (AX2). The control lever (10) includes phasing means (30) constrained to move in rotation with said stick (11) about said first hinge axis (AX1) and about said second hinge axis (AX2), said phasing means (30) comprising at least three main arms (31, 32, 33), each for controlling a respective power member (8′, 8″, 8″′) that is connected to a set (6) of swashplates for controlling a rotary wing (2).
申请公布号 FR2973775(B1) 申请公布日期 2014.01.10
申请号 FR20110001031 申请日期 2011.04.06
申请人 EUROCOPTER 发明人 COUDERC GERARD;BIEST ROMUALD
分类号 B64C13/04;G05G9/047 主分类号 B64C13/04
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