Ratier-figeac Sas

Ratier Figeac

Arnaud Soulié

Cedric Antraygue

Patrick Moulènes

A control lever assembly for controlling an aircraft system. The lever includes: a housing having an outer side and an aperture defined by a rim; and a control lever extending through the aperture and movable in the aperture; the control lever having an outer cover member arranged to slide over the outer side of the housing and cover the rim throughout the range of movement of the control lever.

Control lever assembly for controlling an aircraft system

A piloting device () for piloting a vehicle, in particular an aircraft, has a frame (), a cradle () pivoting with respect to the frame on a first pivot axis (R), a piloting member, called a stick (), pivoting with respect to the cradle () on a second axis (T) orthogonal to and intersecting the first axis, first return elements () for returning the cradle to a predetermined position with respect to the frame, called the neutral position of the cradle, second return elements () for returning the stick to a predetermined position with respect to the cradle, called the neutral position of the stick, wherein at least one of the second return elements, called a stick jack (), is arranged between the stick and the frame.

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Figeac, France

Arnaud Soulié