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).
Control lever for controlling a rotary wing, a mechanical control system including said control lever, and an aircraft
06.10.2015
Patent
Elektronische Ressource
Englisch
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