Patent ID: 8408500

Claim:
Aircraft wing ( 4 ) comprising a wing fixed central body ( 8 ), and a leading edge mobile slat ( 16 ) designed to be moved in rotation relative to said fixed central body along a circular trajectory ( 48 ) inscribed on a sphere ( 50 ) with centre (C), located on a rotation axis ( 42 ) of the leading edge mobile slat ( 16 ) relative to said wing fixed central body ( 8 ); wherein said wing also comprises an assembly ( 100 ) comprising a chain ( 30 ) and at least one cable ( 32 ) supported by said chain connected rigidly at its two ends to the fixed central body ( 8 ) and to the leading edge mobile slat ( 16 ) respectively, said chain comprising links ( 34 , 36 , 38 ) articulated to each other through articulation axes ( 44 ) that converge towards the centre (C).