公开(公告)号：US20150375855A1

公开(公告)日：2015-12-31

申请号：US14746953

申请日：2015-06-23

Applicant: MESSIER-BUGATTI-DOWTY

Inventor： Sylvain JABER ,  Raffi CEKIC

IPC: B64C25/40 ,  H02P3/22

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).

Abstract translation: 本发明涉及一种用于管理旨在旋转地驱动飞行器（1）的车轮（4）的电动机（6）的方法，所述方法包括以下步骤：当电动机（6）的相位短路时， 飞机（1）处于停止使用电动机（6）的期间，在此期间，设想不使用电动机（6）。

公开(公告)号：US20160039518A1

公开(公告)日：2016-02-11

申请号：US14817295

申请日：2015-08-04

Applicant: MESSIER-BUGATTI-DOWTY

Inventor： Sylvain JABER ,  Raffi CEKIC

IPC: B64C25/40 ,  B60B37/10 ,  B60B3/08

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

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

Abstract translation: 本发明涉及一种用于旋转驾驶飞行器轮的方法，所述车轮配备有包括由螺栓（5）组装的两个半轮缘的轮辋，其中用于产生用于驱动车轮的扭矩的驱动构件被控制，其特征在于 因为该方法包括通过轮缘组件螺栓将驱动扭矩传递到车轮。

公开(公告)号：US20150353190A1

公开(公告)日：2015-12-10

申请号：US14722453

申请日：2015-05-27

Applicant: MESSIER-BUGATTI-DOWTY

Inventor： Sylvain JABER ,  Raffi CEKIC

IPC: B64C25/42 ,  B60T8/171 ,  B60T8/1761

CPC classification number: B64C25/42 ,  B60T8/171 ,  B60T8/17616 ,  B60T8/325 ,  B60T8/329 ,  B64C25/405 ,  B64C25/46 ,  Y02T50/823

Abstract: Method for managing the braking of a wheel (4) of an aircraft (1) fitted with a brake (11), the aircraft comprising brake control means suited to implementing an anti-skid function of the wheel (4), requiring an estimate of a rotational speed of the wheel, the aircraft further comprising means of driving the wheel including an electric motor (6) intended to drive the wheel (4) in rotation, the said electric motor (6) being fitted with a position sensor (8) intended to provide measurements of the angular position of a rotor of the motor (6). The method comprises the step, for implementing the anti-skid function, of estimating the rotational speed of the wheel (4) from measurements of the angular position of the rotor which are supplied by the position sensor (8).

Abstract translation: 用于管理装配有制动器（11）的飞机（1）的车轮（4）的制动的方法，所述飞机包括适于实现车轮（4）的防滑功能的制动控制装置，需要估计 所述飞行器还包括驱动所述车轮的装置，所述装置包括用于驱动所述车轮（4）旋转的电动机（6），所述电动马达（6）装配有位置传感器（8） 旨在提供电动机（6）的转子的角位置的测量。 该方法包括用于实现防滑功能的步骤，用于通过由位置传感器（8）提供的转子的角位置的测量来估计车轮（4）的转速。