Method for monitoring a no-back device of an adjustable horizontal trim actuator, corresponding system and aircraft

• US 8,918,291 B2
• Filed: 09/23/2010
• Issued: 12/23/2014
• Est. Priority Date: 11/27/2009
• Status: Active Grant

• Current Assignee: Airbus Operations (European Aeronautic Defence and Space Company EADS NV)
• Original Assignee: Airbus Operations SL (Airbus SE)
• Inventors: Baxerres, Laura, Ferreol, Ivan, Tallot, Cedric
• Primary Examiner(s): Teixeira Moffat, Jonathan C
• Assistant Examiner(s): Casey, Liam R
• Application Number:
  US12/888,965
• Publication Number:
  US 20110127375A1
• Time in Patent Office: 1,552 Days
• Field of Search: 702/34
• US Class Current: 702/34
• CPC Class Codes: B64C 13/24 Transmitting means
• CPC Class Codes: B64C 5/10 adjustable
• CPC Class Codes: B64D 2045/0085 Devices for aircraft health monitoring, e.g. monitoring flutter or vibration
• CPC Class Codes: B64D 45/00 Aircraft indicators or protectors not otherwise provided for camouflage F41H3/00
• CPC Class Codes: F16H 25/2021 with means for avoiding overloading

Abstract

A method and a system for monitoring an actuator equipped with a no-back device or no-back brake, particularly an adjustable horizontal trim actuator provided in aircraft, the method including the steps of: determining a value representative of mechanical work produced by the actuator and comparing the determined value with ranges of values so as to detect a dysfunctioning of the said no-back device. If the actuator is a screw/nut type with a hydraulic motor, the value representative of the mechanical work is determined from an algebraic velocity of the motor and an algebraic differential of hydraulic pressure at terminals of the motor. A negative value corresponding to negative mechanical work then identifies a failure of the no-back device.

Claims

1. A method for monitoring an actuator equipped with a no-back device, comprising:

detecting reversal of a direction of movement of the actuator;

storing in memory, when reversal of the direction of movement of the actuator is detected, a current angular position as a reference angular position of the actuator;

determining a value representative of mechanical work produced by the actuator;

comparing the value representative of the mechanical work produced with ranges of values; and

detecting dysfunctioning of the no-back device by the comparing,

wherein detection of dysfunctioning is temporarily inhibited upon detecting reversal of the direction of movement of the actuator and as long as the angular displacement of the actuator remains within free play of the no-back device, and

wherein a subsequent current angular position is compared with the reference angular position stored in the memory to determine when the angular displacement of the actuator remains within the free play of the no-back device.

2. The method according to claim 1, wherein the actuator includes a screw/nut assembly driven by a motor, and the determination of the value representative of the mechanical work includes a measurement of at least one physical value relating to the motor.

3. The method according to claim 2, wherein the actuator has a hydraulic channel, and the value representative of the mechanical work is determined from an algebraic velocity of the motor and an algebraic differential of hydraulic pressure at terminals of the motor.

4. The method according to claim 3, wherein the dysfunctioning of the no-back device is detected when the value representative of the mechanical work is of a given sign, and the algebraic hydraulic pressure differential and the algebraic velocity each has an absolute value greater than a corresponding threshold value.

5. The method according to claim 1, wherein detection of dysfunctioning is temporarily inhibited as a function of a parameter representative of a rate of deceleration of the actuator.

6. The method according to claim 1, wherein detection of dysfunctioning is a function of an algebraic sign of the value representative of the mechanical work produced.

7. The method according to claim 1, comprising a step of indicating a dysfunctioning of the no-back device when a dysfunctioning of the no-back device is detected for several consecutive determined values.

17. The method according to claim 1, wherein detecting reversal of the direction of movement of the actuator is based on two successive angular velocities of the actuator.

8. A system for monitoring an actuator equipped with a no-back device, comprising:

a reversal detecting module to determine reversal of a direction of movement of the actuator;

memory to store an angular position of the actuator, the memory storing a current angular position as a reference angular position of the actuator when reversal of the direction of movement of the actuator is detected;

a determination module to determine a value representative of mechanical work produced by the actuator;

a comparison module to detect dysfunctioning of the no-back device by comparing the value representative of the mechanical work produced with ranges of values; and

a monitoring module to temporarily inhibit detection of dysfunctioning as a function of a parameter relating to reversal of the direction of movement of the actuator within free play of the no-back device,

wherein a subsequent current angular position is compared with the reference angular position stored in the memory to determine when angular displacement of the actuator is greater than the free play of the no-back device.

9. The monitoring system according to claim 8, wherein the said actuator comprises a screw/nut assembly driven by a motor, and the determination module measures at least one physical value relating to the motor.

10. The monitoring system according to claim 9, wherein the actuator has a hydraulic channel, and the determination module determines the value representative of the mechanical work from an algebraic velocity of the motor and an algebraic differential of hydraulic pressure at terminals of the motor.

11. The monitoring system according to claim 10, wherein the monitoring system detects dysfunctioning of the no-back device when the value representative of the mechanical work is of a given sign, and the algebraic hydraulic pressure differential and the algebraic velocity each has an absolute value greater than a corresponding threshold value.

12. The monitoring system according to claim 8, wherein the monitoring module further inhibits detection of dysfunctioning temporarily as a function of a parameter representative of a rate of deceleration of the actuator.

13. The monitoring system according to claim 8, wherein the comparison module is configured to detect dysfunctioning as a function of an algebraic sign of the value representative of the mechanical work produced.

14. The monitoring system according to claim 8, further comprising an indicator to indicate a dysfunctioning of the no-back device when a dysfunctioning of the said no-back device is detected for several said consecutive determined values.

15. An aircraft comprising an actuator equipped with a no-back device and a system for monitoring the actuator according to claim 8.

16. A method for monitoring an actuator equipped with a no-back device, comprising:

determining a value representative of mechanical work produced by the actuator;

comparing the value representative of the mechanical work produced with ranges of values;

detecting dysfunctioning of the no-back device by the comparing; and

detecting a rate of deceleration of the actuator,

wherein detection of dysfunctioning is temporarily inhibited upon detecting the rate of deceleration of the actuator having an amplitude of which is greater than a threshold amplitude and as long as the amplitude remains greater than the threshold amplitude.