Suspension strut servicing

Patent metadata

Field	Value
Publication number	US-10260994-B2
Application number	US-201414891599-A
Country	US
Kind code	B2
Filing date	May 9, 2014
Priority date	May 16, 2013
Publication date	Apr 16, 2019
Grant date	Apr 16, 2019

Abstract

A method for servicing a landing gear strut in service supporting an aircraft including: determining a current amount of damping fluid in the landing gear strut; determining a required amount of the damping fluid for correct servicing of the landing gear strut; and adjusting the current amount of damping fluid in the landing gear strut so that the current amount of damping fluid complies with the required amount of damping fluid.

First claim

The invention claimed is:

1. A method for servicing a landing gear strut in service while supporting an aircraft, wherein the landing gear strut includes a hollow upper strut part and a hollow lower strut part which is slidably coupled to the upper strut part such that the lower strut part extends and retracts from the upper strut part, the method comprising the steps of:
measuring a level of damping fluid within the leading gear strut;
measuring closure of the landing gear strut, wherein the closure is a distance that the lower strut part extends from the upper strut part;
determining a required level of damping fluid for servicing of the landing gear strut based on the measured closure of the strut, wherein the required level varies with the closure of the landing gear strut; and
adjusting an amount of damping fluid in the landing gear strut to cause an upper surface level of the damping fluid to be at the required level of damping fluid.

2. The method according to claim 1 in which the determination of the required level of damping fluid depends on a predetermined required damping fluid volume for servicing of the landing gear strut and an internal volume of a damping fluid chamber in the upper and lower strut parts of the landing gear strut for a predetermined range of strut closure.

3. The method according to claim 1 further comprising the steps of:
measuring a temperature of the strut; and
the determination of the required level of damping fluid further depends on a thermal expansivity of a required volume of damping fluid in the strut and the measured temperature.

4. The method according to claim 3 in which the measurement of the strut temperature uses one or more sensors associated with the strut.

5. The method according to claim 1 comprising the steps of:
measuring a temperature of the strut; and
the determination of the required level of damping fluid further depends on a thermal expansivity of a structure of the strut providing the damping fluid chamber and the measured strut temperature.

6. The method according to claim 1 comprising the steps of:
measuring an interior pressure of the strut; and
the determination of the required level of damping fluid further depends on a compression of a required volume of damping fluid in the strut in response to the measured pressure.

7. The method according to claim 1 comprising the steps of:
measuring an interior pressure of the strut; and
the determination of the required level of damping fluid further depends on a pressure dilation of the strut in response to the measured interior pressure.

8. The method according to claim 1 in which the measurement of the level of damping fluid level within the strut uses a sensor associated with the strut.

9. The method according to claim 8 in which the sensor comprises an ultrasonic transducer.

10. The method according to claim 8 in which the sensor comprises an ultrasonic transducer array.

11. The method according to claim 10 in which the ultrasonic array is driven in a pulse-echo mode.

12. The method according to claim 1 in which the measurement of the strut closure uses one or more sensors associated with the strut.

13. The method according to claim 1 further comprising the steps of:
wherein the measurement of the closure is performed in response to the measured level of damping fluid complying with the determined required level of damping fluid;
determining a required strut closure for correct servicing of a gas spring of the strut; and
adjusting an amount of gas in the strut so that the measured strut closure complies with the required strut closure.

14. The method according to claim 13 in which the determination of the required strut closure depends on a temperature and an interior pressure of the strut.

Assignees

• Airbus Operations Ltd

Inventors

• Shepherd Alan
• Duncan Julian

Classifications

• Y02T50/166

  Cross-Sectional Technologies · mapped topic

• B64C25/60

  Oleo legs · CPC title

• G01M17/04 Primary

  Suspension or damping · CPC title

• G01F23/296

  Acoustic waves · CPC title

• B64F5/60 Primary

  Testing or inspecting aircraft components or systems · CPC title