Apparatus and method for testing jet engine fuel manifold flow distribution

• US 20030056578A1
• Filed: 09/21/2001
• Published: 03/27/2003
• Est. Priority Date: 09/21/2001
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Webber, John R., Oloffo, Joseph M., Englund, Michael S., Mitchell, Robert D.
• Granted Patent: US 6,672,145 B2
• Time in Patent Office: Days
• US Class Current: 73/116
• CPC Class Codes: F01D 21/003 Arrangements for testing or measuring for measuring vibrations G01H
• CPC Class Codes: F02C 7/22 Fuel supply systems
• CPC Class Codes: F02C 9/26 Control of fuel supply F02C9/48 takes precedence; fuel valves F02C7/232
• CPC Class Codes: F05D 2270/301 Pressure
• CPC Class Codes: F05D 2270/707 fuzzy logic

Abstract

An apparatus and method for testing the flow distribution through a turbine engine fuel manifold and one or more nozzles connected to the manifold. A plurality of individual fluid measurement vessels, at least one for each of the nozzles being tested, collects test fluid pumped through the manifold and the connected nozzles. The level in each of the measurement vessels is periodically sampled during the test. The test fluid flow rate through each of the nozzles is periodically determined based on the periodically sampled levels.

Claims

1. An apparatus for testing fluid flow distribution through a turbine engine fuel manifold and one or more fuel nozzles connected thereto, the apparatus comprising:

a test fluid supply tank;

one or more test fluid supply lines each including a test fluid inlet in fluid communication with the test fluid supply tank and a test fluid outlet adapted to be coupled to the fuel manifold and its connected fuel nozzles;

a plurality of fluid measurement vessels each operable to receive a test fluid discharged from one of the fuel nozzles when the fuel manifold is coupled to the test fluid supply line outlet;

a plurality of level sensors individually coupled to each of the fluid measurement vessels and operable to determine a level of the test fluid therein and generate a level signal representative of the test fluid level; and

a computer coupled to the one or more level sensors and operable to periodically sample each of the generated level signals and calculate test fluid flow rate through each of the fuel nozzles based on the sampled level signals.

2. The apparatus of claim 1, wherein the fuel manifold includes a primary line and a secondary line, and wherein the one or more test fluid supply lines comprises:

a primary fluid supply line adapted to be coupled to fuel manifold primary line; and

a secondary fluid supply line adapted to be coupled to the fuel manifold secondary line.

3. The apparatus of claim 1, further comprising:

a pump in fluid communication between the test fluid supply tank and the supply line inlets and operable to pump the test fluid from the test fluid supply tank through the supply lines.

4. The apparatus of claim 1, further comprising:

a display device coupled to the computer and operable to display the calculated test fluid flow rates through each of the fuel nozzles.

5. The apparatus of claim 1, further comprising:

a flow sensor in fluid communication with the one or more test fluid supply lines and electrically coupled to the computer, the flow sensor operable to generate a flow signal representative of the test fluid flow rate through the supply lines to the fuel manifold,

wherein the computer periodically samples the flow signal and determines the flow rate through the supply lines therefrom.

6. The apparatus of claim 5, further comprising:

a display device coupled to the computer and operable to display the calculated test fluid flow rates through each of the fuel nozzles and the determined fuel flow rate through the supply lines.

7. The apparatus of claim 1, further comprising:

one or more pressure sensors in fluid communication with the one or more fluid supply lines and electrically coupled to the computer, the pressure sensors each operable to generate a pressure signal representative of test fluid pressure in the supply lines,

wherein the computer periodically samples the pressure signals and determines the pressure in the supply lines therefrom.

8. The apparatus of claim 7, further comprising:

a display device coupled to the computer and operable to display the determined pressure in the supply lines.

9. The apparatus of claim 1, further comprising:

a fluid return line coupled to, and providing fluid communication between, each of the fluid measurement vessels and the test fluid supply tank.

10. The apparatus of claim 9, further comprising:

a jet pump coupled in flow-series in the fluid return line.

11. The apparatus of claim 9, further comprising:

a plurality of remotely operated drain valves individually coupled between the fluid return line and each of the fluid measurement vessels.

12. The apparatus of claim 11, wherein the drain valves are operated in response to commands issued by the computer.

13. The apparatus of claim 1, wherein each of the measurement vessels comprises:

a first vessel including a nozzle receiving portion adapted to receive one of the fuel nozzles therein; and

a second vessel in fluid communication with the first vessel, and including a sensor receiving portion adapted to receive one of the level sensors therein.

14. The apparatus of claim 13, wherein the first vessel includes a substantially transparent portion proximate the nozzle receiving portion, whereby a test fluid spray pattern from the fuel nozzle is observable.

15. The apparatus of claim 1, wherein the one or more test fluid supply lines each include an in-line valve coupled between the test fluid inlet and test fluid outlet, wherein pressure of the test fluid supplied to the fuel manifold is adjusted by operation of the in-line valves.

16. The apparatus of claim 15, wherein the one or more in-line valves are remotely operated.

17. The apparatus of claim 15, wherein the one or more remotely operated in-line valves are positioned automatically in response to commands issued by the computer.

18. The apparatus of claim 1, wherein each of the level sensors comprises:

a tube extending longitudinally within the measurement vessel;

a magnet assembly surrounding a portion of the tube, the magnet assembly emitting a magnetic field and operable to move axially along the tube in response to a changing fluid level;

a transducer electrically coupled to the tube and operable to periodically transmit electrical pulses and receive reflected pulses,

wherein the reflected pulses are generated based on interaction of the transmitted pulses with the magnetic field emitted by the magnet assembly.

19. The apparatus of claim 1, further comprising a display device operable to display the level of the test fluid in each of the fluid measurement vessels based on the generated level signals.

20. The apparatus of claim 19, wherein the test fluid levels are displayed numerically.

21. The apparatus of claim 20, wherein the test fluid levels are displayed graphically.

22. An apparatus for testing fluid flow distribution through a turbine engine fuel manifold and one or more fuel nozzles connected thereto, the apparatus comprising:

a test fluid supply tank;

one or more test fluid supply lines each including a test fluid inlet in fluid communication with the test fluid supply tank and a test fluid outlet adapted to be coupled to the fuel manifold and its connected fuel nozzles;

a plurality of fluid measurement vessels each operable to receive a test fluid discharged from one of the fuel nozzles when the fuel manifold is coupled to the test fluid supply line outlet;

a plurality of level sensors individually coupled to each of the fluid measurement vessels and operable to determine a level of the test fluid therein and generate a level signal representative of the test fluid level;

a computer coupled to the one or more level sensors and operable to periodically sample each of the generated level signals and calculate test fluid flow rate through each of the fuel nozzles based on the sampled level signals; and

a display device coupled to the computer and operable to display the calculated test fluid flow rates through each of the fuel nozzles.

23. The apparatus of claim 22, wherein the fuel manifold includes a primary line and a secondary line, and wherein the one or more test fluid supply lines comprises:

a primary fluid supply line adapted to be coupled to fuel manifold primary line; and

a secondary fluid supply line adapted to be coupled to the fuel manifold secondary line.

24. The apparatus of claim 22, further comprising:

a pump in fluid communication between the test fluid supply tank and the supply line inlets and operable to pump the test fluid from the test fluid supply tank through the supply lines.

25. The apparatus of claim 22, further comprising:

a flow sensor in fluid communication with the one or more test fluid supply lines and electrically coupled to the computer, the flow sensor operable to generate a flow signal representative of the test fluid flow rate through the supply lines to the fuel manifold,

wherein the computer periodically samples the flow signal and determines the flow rate through the supply lines therefrom.

26. The apparatus of claim 25, further comprising:

a display device coupled to the computer and operable to display the calculated test fluid flow rates through each of the fuel nozzles and the determined fuel flow rate through the supply lines.

27. The apparatus of claim 22, further comprising:

one or more pressure sensors in fluid communication with the one or more fluid supply lines and electrically coupled to the computer, the pressure sensors each operable to generate a pressure signal representative of test fluid pressure in the supply lines,

wherein the computer periodically samples the pressure signals and determines the pressure in the supply lines therefrom.

28. The apparatus of claim 27, further comprising:

a display device coupled to the computer and operable to display the determined pressure in the supply lines.

29. The apparatus of claim 22, further comprising:

a fluid return line coupled to, and providing fluid communication between, each of the fluid measurement vessels and the test fluid supply tank.

30. The apparatus of claim 29, further comprising:

a jet pump coupled in flow-series in the fluid return line.

31. The apparatus of claim 29, further comprising:

a plurality of remotely operated drain valves individually coupled between the fluid return line and each of the fluid measurement vessels.

32. The apparatus of claim 31, wherein the drain valves are operated in response to commands issued by the computer.

33. The apparatus of claim 22, wherein each of the measurement vessels comprises:

a first vessel including a nozzle receiving portion adapted to receive one of the fuel nozzles therein; and

a second vessel in fluid communication with the first vessel, and including a sensor receiving portion adapted to receive one of the level sensors therein.

34. The apparatus of claim 33, wherein the first vessel includes a substantially transparent portion proximate the nozzle receiving portion, whereby a test fluid spray pattern from the fuel nozzle is observable.

35. The apparatus of claim 22, wherein the one or more test fluid supply lines each include an in-line valve coupled between the test fluid inlet and test fluid outlet, wherein pressure of the test fluid supplied to the fuel manifold is adjusted by operation of the in-line valves.

36. The apparatus of claim 35, wherein the one or more in-line valves are remotely operated.

37. The apparatus of claim 36, wherein the one or more remotely operated in-line valves are positioned automatically in response to commands issued by the computer.

38. The apparatus of claim 22, wherein each of the level sensors comprises:

a tube extending longitudinally within the measurement vessel;

a magnet assembly surrounding a portion of the tube, the magnet assembly emitting a magnetic field and operable to move axially along the tube in response to a changing fluid level;

a transducer electrically coupled to the tube and operable to periodically transmit electrical pulses and receive reflected pulses,

wherein the reflected pulses are generated based on interaction of the transmitted pulses with the magnetic field emitted by the magnet assembly.

39. The apparatus of claim 22, further comprising a display device operable to display the level of the test fluid in each of the fluid measurement vessels based on the generated level signals.

40. The apparatus of claim 39, wherein the test fluid levels are displayed numerically.

41. The apparatus of claim 40, wherein the test fluid levels are displayed graphically.

42. An apparatus for testing fluid flow distribution through a turbine engine fuel manifold and one or more fuel nozzles connected thereto, the apparatus comprising:

a test fluid supply tank;

one or more test fluid supply lines each including a test fluid inlet in fluid communication with the test fluid supply tank and a test fluid outlet adapted to be coupled to the fuel manifold and its connected fuel nozzles;

a plurality of fluid measurement vessels each operable to receive a test fluid discharged from one of the fuel nozzles when the fuel manifold is coupled to the test fluid supply line outlet;

a plurality of level sensors individually coupled to each of the fluid measurement vessels and operable to determine a level of the test fluid therein and generate a level signal representative of the test fluid level;

a computer coupled to the one or more level sensors and operable to periodically sample each of the generated level signals and calculate test fluid flow rate through each of the fuel nozzles based on the sampled level signals; and

a display device coupled to the computer and operable to display (i) the calculated test fluid flow rates through each of the fuel nozzles and (ii) the test fluid levels both numerically and graphically.

43. A method of testing fluid flow distribution through a turbine engine fuel manifold and one or more fuel nozzles connected thereto, the apparatus comprising:

supplying a test fluid to the fuel manifold at a predetermined pressure;

collecting the test fluid discharged from each of the fuel nozzles in separate measurement vessels;

periodically determining a volume of test fluid discharged from each of the fuel nozzles until each of the measurement vessels have collected a predetermined volume of the test fluid; and

periodically calculating test fluid flow rate through each of the fuel nozzles based on the periodically determined test fluid discharge volume.

44. The method of claim 43, further comprising:

determining a variation between the test fluid flow rates through each of the fuel nozzles.

45. The method of claim 44, wherein the determination of test fluid flow rate variation comprises determining a maximum variation.

46. The method of claim 45, wherein the determination of maximum flow rate variation comprises:

subtracting a minimum fuel nozzle flow rate from a maximum fuel nozzle flow rate to obtain a difference;

determining a median fuel nozzle flow rate through each of the fuel nozzles; and

dividing the difference by the determined median.

47. The method of claim 43, wherein the tested fuel manifold and nozzles each include a primary and a secondary flow path, and wherein the method further comprises:

supplying the test fluid at the predetermined pressure to only the fuel manifold and nozzle primary flow paths.

48. The method of claim 47, further comprising:

supplying the test fluid at the predetermined pressure to only the fuel manifold and nozzle secondary flow paths.

49. The method of claim 47, further comprising:

simultaneously supplying the test fluid at the predetermined pressure to the fuel manifold and nozzle primary and secondary flow paths.

50. The method of claim 43, further comprising:

observing a spray pattern of the test fluid discharged from each of the nozzles.

51. The method of claim 43, wherein the test fluid volume is periodically determined based on a periodically determined test fluid level in each of the measurement vessels.

52. The method of claim 43, further comprising:

displaying the periodically calculated test fluid flow rates through each of the fuel nozzles.

53. The method of claim 43, further comprising:

displaying the periodically determined test fluid volumes discharged from each of the fuel nozzles.

54. The method of claim 53, wherein the periodically determined test fluid volumes are displayed numerically and graphically.

55. A computer-readable medium storage medium containing computer executable code for instructing a computer, which is coupled to a test stand that is configured to test fluid flow distribution through a turbine engine fuel manifold and one or more fuel nozzles, and that includes a plurality of fluid measurement vessels each operable to receive a test fluid discharged from one of the fuel nozzles, to perform the steps of:

periodically determining and displaying a volume of test fluid discharged from each of the fuel nozzles until each of the measurement vessels have collected a predetermined volume of the test fluid; and

periodically calculating and displaying test fluid flow rate through each of the fuel nozzles based on the periodically determined test fluid discharge volume.