Methods of monitoring hydraulic fluid levels in an aircraft

Patent metadata

Field	Value
Publication number	US-9316520-B2
Application number	US-201414152258-A
Country	US
Kind code	B2
Filing date	Jan 10, 2014
Priority date	Feb 12, 2013
Publication date	Apr 19, 2016
Grant date	Apr 19, 2016

Abstract

A method of monitoring hydraulic fluid levels in an aircraft includes identifying segments of operation where the aircraft meets a predetermined stability criteria, receiving output from the fluid sensor, calculating hydraulic fluid levels within the at least one hydraulic storage tank, determining a hydraulic fluid value indicative of the amount of hydraulic fluid in the aircraft based on at least the calculated hydraulic fluid level, and providing an indication of the hydraulic fluid value.

First claim

What is claimed is:

1. A method of monitoring hydraulic fluid levels in an aircraft hydraulic system having at least one hydraulic storage tank supplying hydraulic fluid to at least one component of the aircraft, with a fluid sensor providing an output indicative of an amount of hydraulic fluid in the storage tank, the method comprising:
identifying segments of operation where the aircraft meets predetermined stability criteria while the aircraft is in operation;
receiving output from the fluid sensor during the identified segments of operation to define a stable output;
calculating hydraulic fluid levels within the at least one hydraulic storage tank based on the stable output;
determining a hydraulic fluid value indicative of the amount of hydraulic fluid in the aircraft based on at least the calculated hydraulic fluid level; and
providing an indication of the hydraulic fluid value.

2. The method of claim 1 wherein the identified segments of operation include multiple phases of flight of the aircraft.

3. The method of claim 2 wherein the multiple phases of flight include taxi and cruise.

4. The method of claim 1 wherein the calculating the hydraulic fluid levels comprises adjusting the calculated hydraulic fluid levels for at least some of the hydraulic fluid in use as the aircraft is in operation.

5. The method of claim 4 wherein the adjusting the calculated hydraulic fluid levels comprises adding at least some in-use hydraulic fluid to the calculated hydraulic fluid levels.

6. The method of claim 5 wherein the adding comprises adding known hydraulic fluid used by predictable hydraulic-using components.

7. The method of claim 6 wherein the predictable hydraulic-using components comprise trailing edge flaps.

8. The method of claim 1 , further comprising comparing the determined hydraulic value to a predetermined threshold.

9. The method of claim 8 wherein the providing the indication comprises indicating that hydraulic fluid should be emptied when the comparison indicates the determined hydraulic value is greater than the predetermined threshold.

10. The method of claim 8 wherein the providing the indication comprises indicating that hydraulic fluid should be added when the comparison indicates the determined hydraulic value is less than the predetermined threshold.

11. The method of claim 1 , further comprising comparing the determined hydraulic fluid value to historical values.

12. The method of claim 11 , further comprising determining a leak within the hydraulic system based on the comparison.

13. The method of claim 12 wherein the providing the indication comprises indicating the leak.

14. The method of claim 1 wherein the stability criteria includes at least one of a lateral acceleration within 0.01 g of flight's modal value, a vertical acceleration within 0.02 g of flight's modal value, a heading changing less than 3 degrees per half second, and a roll within 1 degree of flight's modal value.

15. The method of claim 1 wherein the stability criteria includes parameters including at least one of a suitable spoiler condition, a suitable flap handle position, a suitable thrust reverser position, and a suitable landing gear position.

16. A method of monitoring hydraulic fluid levels in an aircraft hydraulic system having two hydraulic storage tanks supplying hydraulic fluid to at least one movable component of the aircraft, with a fluid sensor operably coupled to each of the hydraulic storage tanks and providing an output indicative of an amount of hydraulic fluid in its related storage tank, the method comprising:
determining a position of the aircraft and movement of the aircraft;
determining a position of the at least one movable component of the aircraft;
identifying segments of operation where the aircraft meets predetermined stability criteria while the aircraft is in operation;
receiving output from the fluid sensors during the identified segments of operation to define a stable output;
calculating hydraulic fluid levels within the hydraulic storage tanks based on the stable output;
determining hydraulic fluid values indicative of the amount of hydraulic fluid in each of the hydraulic storage tanks based on at least the calculated hydraulic fluid levels;
determining one of an overfill condition, a refill required condition, and a leak condition from the determined hydraulic fluid values; and
providing an indication related to the determined condition.

17. The method of claim 16 wherein the calculating the hydraulic fluid levels comprises adjusting the calculated hydraulic fluid levels for at least some of the hydraulic fluid in use based on the received output regarding the position of the at least one movable component of the aircraft.

18. The method of claim 16 wherein the determining the hydraulic fluid values includes determining at least one of a mean, median, mode, and standard deviation for the calculated hydraulic fluid levels within the two hydraulic storage tanks.

19. The method of claim 18 wherein the determining the condition includes comparing the determined the at least one of the mean, median, mode, and standard deviation hydraulic fluid levels to historical fluid levels.

Assignees

• Ge Aviat Systems Ltd

Inventors

• Horabin Robert William
• Howard Julia Ann
• Heath Daniel James

Classifications

• G01F23/0076

  Physics · mapped topic

• G01F23/00 Primary

  Indicating or measuring liquid level or level of fluent solid material, e.g. indicating in terms of volume or indicating by means of an alarm · CPC title

• G01F23/804 Primary

  containing circuits handling parameters other than liquid level · CPC title

• B64F5/60

  Testing or inspecting aircraft components or systems · CPC title

• B64C13/40 Primary

  using fluid pressure · CPC title