Apparatus and method for testing a linear acuator

Patent metadata

Field	Value
Publication number	US-10481047-B2
Application number	US-201715825747-A
Country	US
Kind code	B2
Filing date	Nov 29, 2017
Priority date	Dec 2, 2016
Publication date	Nov 19, 2019
Grant date	Nov 19, 2019

Abstract

An apparatus for in-situ testing of a linear actuator configured to exert an actuation force in an actuation direction by movement of a first part of the actuator relative to a second part of the actuator. The apparatus includes a test device, a test actuator and a measurement device. The test device includes a first surface configured to contact the first part of the actuator, and a second surface configured to contact the second part of the actuator. The second surface is moveable relative to the first surface to alter a distance therebetween. The test actuator is configured to exert a test force in a direction opposite to the actuation direction, the test force being to drive movement of the second surface away from the first surface. The measurement device is for detecting a change in the distance between the first surface and the second surface.

First claim

The invention claimed is:

1. An apparatus for in-situ testing of a linear actuator configured to exert an actuation force in an actuation direction by movement of a first part of the linear actuator relative to a second part of the linear actuator, wherein the apparatus comprises:
a test device comprising a first surface configured to contact the first part of the linear actuator during operation of the apparatus, and a second surface configured to contact the second part of the linear actuator during operation of the apparatus, wherein the second surface is moveable relative to the first surface to alter a distance between the first surface and the second surface;
a test actuator coupled to the test device and configured to exert a test force in a direction opposite to the actuation direction when the apparatus is in use to test the linear actuator, the test force being to drive movement of the second surface away from the first surface; and
a measurement device for detecting a change in the distance between the first surface and the second surface, wherein the measurement device is integrated with the test device and/or the test actuator.

2. The apparatus of claim 1 , wherein the linear actuator comprises an extending arm, and wherein the test device is configured to enclose a cross-section of the extending arm during operation of the apparatus to test the linear actuator.

3. The apparatus of claim 1 , wherein the test device comprises a load reaction component and a force generation component, and wherein the first surface is comprised in the load reaction component and the second surface is comprised in the force generation component.

4. The apparatus of claim 3 , wherein the load reaction component is configured to react a maximum actuation force exertable by the linear actuator.

5. The apparatus of claim 3 , wherein the force generation component comprises one or more extendible members connected to the test actuator, wherein the one or more extendible members are in contact with the force reaction component such that forces are transmissible from the force generation component to the force reaction component via the one or more extendible members,
wherein extension of the one or more extendible members increases a distance between the first surface and the second surface, and
wherein the test actuator is configured to drive extension of the one or more extendible members.

6. The apparatus of claim 1 , wherein the test actuator is configured to exert the test force according to at least one predetermined parameter, wherein the at least one predetermined parameter includes one or more of:
a magnitude of the test force;
a direction of the test force;
a time period during which the test force is continuously exerted.

7. The apparatus of claim 1 , wherein the test actuator comprises a hydraulic actuator.

8. The apparatus of claim 1 , wherein the first surface is configured to seat on a surface on the first part contacted by the first surface during operation of the actuator, and the second surface is configured to seat on a surface on the second part contacted by the second surface during operation of the actuator.

9. The apparatus of claim 1 , wherein the measurement device is configured to measure a parameter relating to a distance between the first surface and the second surface.

10. The apparatus of claim 9 , wherein the measurement device is configured to detect whether the measured parameter exceeds a predetermined threshold.

11. The apparatus of claim 10 , wherein the test actuator is configured to exert the test force continuously for a time period and the measurement device is configured to continuously measure the parameter during the time period, and wherein the measurement device is further configured to determine a time at which the measured parameter exceeds the predetermined threshold.

12. The apparatus of claim 9 , wherein the test actuator is configured to exert the test force continuously for a predetermined time period, and the measurement device is configured to measure the parameter at the end of the predetermined time period.

13. The apparatus of claim 9 , wherein the parameter is any one of:
distance between the first surface and the second surface;
distance between a first selected point on the test device and a second selected point on the test device;
distance between a selected point on the first part of the linear actuator and a selected point on the second part of the linear actuator;
degree of extension of the one or more extendible members;
position of a selected point on the linear actuator;
position of a selected point on the test device;
position of a component of the test actuator.

14. An apparatus in combination with a linear actuator;
wherein the linear actuator comprises a first part moveably connected to a second part, and is configured to exert an actuation force in an actuation direction by movement of the first part relative to the second part; and
wherein the apparatus is configured for in-situ testing of the linear actuator and comprises:
a test device mounted on the linear actuator such that in an activated configuration of the linear actuator a first surface of the test device contacts the first part of the linear actuator and a second surface of the test device, which is moveable relative to the second surface of the test device in the actuation direction, contacts the second part of the linear actuator;
a test actuator coupled to the test device and configured to exert a test force in a test direction opposite to the actuation direction, the test force being to drive movement of the second surface away from the first surface; and
a measurement device for detecting a change in the distance between the first surface and the second surface, wherein the measurement device is integrated with the test device and/or the test actuator.

15. The apparatus in combination with a linear actuator according to claim 14 , wherein the actuation force is to reduce the distance between the first part of the linear actuator and the second part of the linear actuator, such that the actuation force compresses the test device.

16. The apparatus in combination with a linear actuator according to claim 14 , wherein the linear actuator is configured to actuate a flight control surface of an aircraft, and wherein one of the first and second parts of the linear actuator is connected to a fixed structure of an aircraft, and the other of the first and second parts of the linear actuator is connected to the flight control surface.

17. An aircraft comprising the apparatus in combination with a linear actuator according to claim 14 .

18. A method of testing of a linear actuator in-situ, wherein the linear actuator is configured to exert an actuation force in an actuation direction by movement of a first part of the linear actuator relative to a second part of the linear actuator, the method comprising:
providing a test device on the linear actuator such that, in an activated configuration of the linear actuator, a first surface of the test device contacts the first part of the linear actuator and a second surface of the test device contacts the second part of the linear actuator;
operating the linear actuator to exert the actuation force on the test device;
operating the test device to apply a predetermined test force in a direction opposite to the actuation direction, the test force being to increase the distance between the first surface and the second surface; and
detecting a change in a distance between the first s

Assignees

• Airbus Operations Ltd

Inventors

• Warren Nicky Steven
• Fussell David
• Bennett Daniel

Classifications

• F15B2211/855

  Testing of fluid pressure systems · CPC title

• F15B2211/7051

  Linear output members · CPC title

• B64C13/38

  with power amplification · CPC title

• F15B19/00

  Testing; {Calibrating; Fault detection or monitoring; Simulation or modelling of} fluid-pressure systems or apparatus not otherwise provided for · CPC title

• G01M13/00

  Testing of machine parts · CPC title