Flight control device for an aircraft

Abstract

The invention concerns a flight control device (1) for an aircraft, comprising: —a housing (2), —a handle (4) mounted rotating relative to the housing (2) about a center of rotation (O), —a first drive shaft (31), a second drive shaft (32) and a third drive shaft (33), the drive shafts (31-33) being mounted rotating relative to the housing (2) about a same axis of rotation (X), —a first connecting part (34) mounted pivoting on the first shaft (31) about a first axis of rotation (A1), and on the handle (4) about a fourth axis of rotation (B1), —a second connecting part (35) mounted pivoting on the second shaft (32) about a second axis of rotation (A2), and on the handle (4) about a fifth axis of rotation (B2), —a third connecting part (36) mounted pivoting on the third shaft (33) about a third axis of rotation (A3), and on the handle (4) about a sixth axis of rotation (B3), the first axis of rotation (A1), the second axis of rotation (A2) and the third axis of rotation (A3) intersecting at the center of rotation (O) of the handle (4).

Dependencies are inferred from the claim text.