首页> 外国专利> AIRCRAFT WING COMPRISING A MOVABLE TRAILING-EDGE FLAP DRIVEN BY A LINEAR ELECTRIC MOTOR

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

机译:飞机机翼由直线电机驱动的活动式尾翼襟翼

摘要

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).
机译:本发明涉及一种飞机机翼,其包括可移动的后缘襟翼(16),所述机翼包括用于移动所述襟翼的装置(50),该装置设置有:支撑导轨的梁(51);以及支撑所述导轨的梁(51)。可移动地安装在导轨(20)上的托架(52a);滑架(52a)与刚性连接到襟翼的托架(30)之间的旋转接头(40a);倾斜构件(29),用于使活动挡板倾斜。支架(30)和倾斜构件(29)之间的旋转接头(40b);倾斜构件(29)与梁(51)之间具有旋转接头(40c)。根据本发明,装置(50)包括线性电动机(22),该线性电动机包括:初级组件(52),该初级组件设置有滑架(52a),该初级组件包括线圈(55);初级组件(52)。次级组件(54)包括布置在轨道(20)上的磁轨。

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