公开(公告)号：US09574633B2

公开(公告)日：2017-02-21

申请号：US14591084

申请日：2015-01-07

Applicant: MESSIER-BUGATTI-DOWTY

Inventor： Thomas Lepage ,  Philippe Chico ,  Francois Bonigen ,  Frederic Ragot

IPC: F16D66/00 ,  B64C25/44 ,  F16D65/18 ,  B60T17/22 ,  G01K13/00 ,  G01R31/34 ,  B60T13/74 ,  F16D55/38

CPC classification number: F16D66/00 ,  B60T13/741 ,  B60T17/221 ,  B64C25/44 ,  F16D55/38 ,  F16D65/18 ,  F16D2066/005 ,  G01K13/00 ,  G01R31/343

Abstract: A method for monitoring a blocking member (12) of an electromechanical actuator (1). The monitoring method comprising the steps of: determining a value representative of a power supply current of a motor (11) during an off-load operating phase of the electromechanical actuator (1); comparing the value representative of the power supply current with a predetermined current threshold defined from nominal off-load operating characteristics of the electromechanical actuator (1); and detecting an accidental locking of the blocking member (12) when the value representative of the power supply current is above or equal to the predetermined current threshold. There also is an electromechanical actuator (1) comprising a blocking member (12) monitored by such a method.

Abstract translation: 一种用于监测机电致动器（1）的阻挡构件（12）的方法。 该监视方法包括以下步骤：在机电致动器（1）的卸载操作阶段期间确定代表电动机（11）的电源电流的值; 将代表电源电流的值与从机电致动器（1）的额定负载运行特性定义的预定电流阈值进行比较; 并且当代表电源电流的值高于或等于预定电流阈值时，检测阻塞构件（12）的意外锁定。 还有一种机电致动器（1），其包括通过这种方法监控的阻挡构件（12）。

公开(公告)号：US09815447B2

公开(公告)日：2017-11-14

申请号：US14605488

申请日：2015-01-26

Applicant: MESSIER-BUGATTI-DOWTY

Inventor： Philippe Chico ,  Frédéric Ragot ,  François Bonigen ,  Thomas Lepage

IPC: B60T17/22 ,  B64C25/44 ,  B60T8/17 ,  B60T8/88

CPC classification number: B60T17/221 ,  B60T8/1703 ,  B60T8/885 ,  B60T17/22 ,  B60T2270/406 ,  B64C25/44

Abstract: A method for monitoring at least two aircraft wheel electromechanical braking actuators. For each electromechanical actuator, the method includes first determining a current value representative of the power supply current of the electromechanical actuator and determining a reference current value estimated from the power supply currents of at least one other electromechanical actuator. Then, the representative current value and the reference current value are compared. Any abnormal operation of the electromechanical actuator is detected when the difference between the representative current value and the reference current value is above a predetermined threshold.

公开(公告)号：US09422054B2

公开(公告)日：2016-08-23

申请号：US14060083

申请日：2013-10-22

Applicant: MESSIER-BUGATTI-DOWTY

Inventor： Dominique Onfroy ,  Thomas Lepage ,  Franck Selles ,  Frédéeric Ragot

IPC: B64C25/44 ,  B60T8/17 ,  B60T7/04 ,  B60T7/08 ,  B60T13/74 ,  F16D55/38

CPC classification number: B64C25/44 ,  B60T7/042 ,  B60T7/085 ,  B60T8/1703 ,  B60T13/741 ,  F16D55/38

Abstract: An aircraft electromechanical braking system comprising a braking control unit 10 and at least one electromechanical brake 1, the brake 1 being fitted with at least one electromechanical actuator 4 having a pusher 6 suitable for being moved by means of an electric motor 7. The actuator 4 also has a blocking member 8 for blocking the pusher 6 in position. The control unit 10 is adapted to cause the braking system to operate in an additional braking mode referred to as “combined” mode, in which the motor 7 is activated to bring the pusher 6 into a position in which it exerts a given holding force, and then the blocking member 8 is activated, while activation of the motor 7 is maintained.

Abstract translation: 包括制动控制单元10和至少一个机电制动器1的飞机机电制动系统，制动器1装配有至少一个机电致动器4，其具有适于通过电动机7移动的推动器6.致动器4 还具有用于将推动器6阻挡就位的阻挡构件8。 控制单元10适于使制动系统以称为“组合”模式的附加制动模式操作，其中马达7被启动以使推动器6进入其施加给定保持力的位置， 然后在保持马达7的启动的同时启动阻挡构件8。