Method for monitoring at least two electromechanical braking actuators

Patent metadata

Field	Value
Publication number	US-9815447-B2
Application number	US-201514605488-A
Country	US
Kind code	B2
Filing date	Jan 26, 2015
Priority date	Jan 31, 2014
Publication date	Nov 14, 2017
Grant date	Nov 14, 2017

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.

First claim

The invention claimed is:

1. A method for monitoring and restoring or disabling at least three aircraft wheel electromechanical braking actuators ( 5 ), each electromechanical actuator ( 5 ) being powered by a power supply providing a current (Ia) under control of a braking controller ( 9 ) to selectively apply a braking force to friction members ( 15 ), the monitoring and restoring or disabling method comprising:
activating the electromechanical actuators ( 5 ), and
thereafter, for each active electromechanical actuator ( 5 ), performing the steps of:
determining with a current sensor ( 18 ) a current value (Ivr) representative of the power supply current of the electromechanical actuator;
determining by the braking controller ( 9 ) a reference current value (Ir) estimated from the power supply currents of at least two other electromechanical actuator ( 5 );
comparing by the braking controller ( 9 ) the representative current value (Ivr) and the reference current value (Ir);
detecting by the braking controller ( 9 ) an abnormal operation of the electromechanical actuator ( 5 ) when the difference between the representative current value and the reference current value is above a predetermined threshold (Is), and

following the detection of an abnormal operation of an electromechanical actuator ( 5 ), the steps of:
identifying by the braking controller ( 9 ) the electromechanical actuator ( 5 ) exhibiting the abnormal operation;
signalling by the braking controller ( 9 ) abnormal operation of the electromechanical actuator ( 5 );
performing by the braking controller ( 9 ) a restoration or deactivation of the abnormal electromechanical actuator ( 5 ).

2. The method according to claim 1 , in which the representative current value (Ivr) is an absolute value of an estimation of the power supply current of the electromechanical actuator ( 5 ).

3. The method according to claim 1 , in which the reference current value (Ir) is an average of absolute values of estimations of the power supply currents concerned.

4. The method according to claim 2 , in which the estimations of the power supply currents are average values or instantaneous values of the power supply currents.

5. The method according to claim 1 , in which the representative current value (Ivr) and the reference current value (Ir) are obtained from power supply currents measured during off-load operating phases of the electromechanical actuators.

6. The method according to claim 1 ,
wherein the restoration action comprises performing a corrective or reconfiguration action to try to restore the electromechanical actuator to normal operating conditions; and
wherein the deactivation action comprises deactivating the electromechanical actuator exhibiting an abnormal operation if the corrective or reconfiguration action does not make it possible to restore the electromechanical actuator to the normal operating conditions.

7. The method according to claim 3 , in which the estimations of the power supply currents are average values or instantaneous values of the power supply currents.

Assignees

• Messier Bugatti Dowty

Inventors

• Chico Philippe
• Ragot Frédéric
• Bonigen François
• Lepage Thomas

Classifications

• B60T17/221 Primary

  Procedure or apparatus for checking or keeping in a correct functioning condition of brake systems (hydraulic pressure systems in general F15B19/00, F15B21/04; testing structures or apparatus G01M) · CPC title

• B60T8/885

  using electrical circuitry · CPC title

• B60T17/22 Primary

  Devices for monitoring or checking brake systems; Signal devices · CPC title

• B64C25/44 Primary

  Actuating mechanisms · CPC title

• B60T8/1703

  for aircrafts · CPC title