公开(公告)号：US09527582B2

公开(公告)日：2016-12-27

申请号：US14447825

申请日：2014-07-31

Applicant: MESSIER-BUGATTI-DOWTY

Inventor： Thierry Blanpain ,  Edouard Campbell ,  Yann Simonneaux ,  Martial Monseu ,  Remi Finet

IPC: B64C25/40 ,  B64C25/18

CPC classification number: B64C25/18 ,  B64C25/405 ,  Y02T50/823

Abstract: Aircraft undercarriage leg including an axle (3) that bears at least one wheel (4), the undercarriage leg being equipped with a unit (6) for driving rotation of the wheel, wherein the drive unit is rigidly fixed to the axle and a deformable support (12) extends between a cantilevered portion of the drive unit and a portion of the undercarriage leg not including the axle to support the cantilevered portion of the drive unit.

Abstract translation: 飞机起落架腿包括具有至少一个轮（4）的轴（3），起落架腿配备有用于驱动车轮旋转的单元（6），其中驱动单元刚性地固定到车轴上，并且可变形 支撑件（12）在驱动单元的悬臂部分和不包括轴的起落架腿部的一部分之间延伸，以支撑驱动单元的悬臂部分。