公开(公告)号：US09650131B2

公开(公告)日：2017-05-16

申请号：US14817295

申请日：2015-08-04

Applicant: MESSIER-BUGATTI-DOWTY

Inventor： Sylvain Jaber ,  Raffi Cekic

IPC: B60K1/00 ,  B64C25/40 ,  B60B3/08 ,  B60B37/10 ,  B60B25/00

CPC classification number: B64C25/405 ,  B60B3/08 ,  B60B25/004 ,  B60B37/10 ,  B60Y2200/51 ,  Y02T50/823

Abstract: A method for rotationally driving an aircraft wheel, the wheel being equipped with a rim comprising two half-rims assembled by bolts (5). According to the method, a drive member for generating a torque for driving the wheel is controlled. The transfer of the drive torque to the wheel is accomplished via the rim assembly bolts.

公开(公告)号：US09630707B2

公开(公告)日：2017-04-25

申请号：US14746953

申请日：2015-06-23

Applicant: MESSIER-BUGATTI-DOWTY

Inventor： Sylvain Jaber ,  Raffi Cekic

IPC: H03K5/00 ,  B64C25/40 ,  H02P9/00 ,  H02P3/22 ,  H02P3/12

CPC classification number: B64C25/405 ,  H02P3/12 ,  H02P3/22 ,  H02P9/008 ,  Y02T50/823

Abstract: The invention relates to a method for managing an electric motor (6) intended to drive rotationally a wheel (4) of an aircraft (1), the method comprising the step of short-circuiting the phases of the electric motor (6) when the aircraft (1) is in a period of deactivation of the motor (6) during which it is envisaged not using the electric motor (6).