Airbus Helicopters

Florian Feugas

Bernard Gemmati

Christophe Pujol

An adjustable and rotary rudder bar for a rotary wing aircraft. The rudder bar comprises a pedal bar, a main body, two pedals connected to the pedal bar on either side of the main body, a slider device enabling the pedal bar to slide relative to the main body, a structure fastened to a floor of the aircraft, and a shaft having a first axis (A). The shaft is secured to the main body, and the main body is movable in turning relative to the structure about the first axis (A) thus causing the main body, the pedal bar, and the pedals to turn simultaneously.

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Chateauneuf Les Martigues, France

Florian Feugas