AIRCRAFT WING COMPRISING A MOVABLE TRAILING-EDGE FLAP DRIVEN BY A LINEAR ELECTRIC MOTOR

The invention relates to an aircraft wing comprising a mobile trailing edge flap (16), the wing comprising a device (50) for moving said flap, the device being provided with: a beam (51) supporting a guide rail; a carriage (52a) movably mounted on the rail (20); a rotary joint (40a) between the carriage (52a) and a bracket (30) rigidly connected to the flap; a tilt member (29) for tilting the mobile flap; a rotary joint (40b) between the bracket (30) and the tilt member (29); and a rotary joint (40c) between the tilt member (29) and the beam (51). According to the invention, the device (50) comprises a linear electric motor (22) including: a primary assembly (52) provided with the carriage (52a), which includes coils (55); and a secondary assembly (54) including a magnetic track arranged on the rail (20). L'invention concerne une aile d'aéronef comprenant un volet mobile de bord de fuite (16), l'aile comprenant un dispositif (50) de mise en mouvement de ce volet, le dispositif étant équipé : - d'une poutre (51) portant un rail de guidage; - d'un chariot (52a) monté mobile sur le rail (20); - d'une liaison articulée (40a) entre le chariot (52a) et une ferrure (30) solidaire du volet; - d'un organe de basculement (29) du volet mobile; - d'une liaison articulée (40b) entre la ferrure (30) et l'organe de basculement (29); et - d'une liaison articulée (40c) entre l'organe de basculement (29) et la poutre (51). Selon l'invention, le dispositif (50) comprend un moteur électrique linéaire (22) comportant un ensemble primaire (52) équipé du chariot (52a) qui intègre des bobines (55), et un ensemble secondaire (54) comportant une voie magnétique agencée sur le rail (20).