Flow vector analyzer for flow bench

• US 6,772,627 B2
• Filed: 03/26/2003
• Issued: 08/10/2004
• Est. Priority Date: 03/26/2002
• Status: Active Grant

• Current Assignee: Ronald J. Fleming
• Original Assignee: Ronald J. Fleming
• Inventors: Fleming, Ronald J.
• Primary Examiner(s): Williams, Hezron
• Assistant Examiner(s): Rogers, David A.
• Application Number:
  US10/397,602
• Publication Number:
  US 20030209084A1
• Time in Patent Office: 503 Days
• Field of Search: 731/47, 731/481, 73/700.1, 731/700.4, 731/700.6, 731/700.7, 731/700.8, 731/700.9, 731/701.1, 738/616.6
• US Class Current: 73/147
• CPC Class Codes: G01M 9/04 Details

Abstract

Apparatus and methods for airflow testing, especially for air testing of gas turbine components on an airflow test bench. Various embodiments of the present invention include the use of a measurement section downstream of the component being tested. The measurement section, in one embodiment, includes apparatus for measurement of gas properties at a plurality of spaced-apart radial locations and/or a plurality of spaced-apart circumferential locations. In another embodiment, the invention includes a method for testing a component including a comparison of gas properties measured in both forward and reverse flow directions.

Claims

1. An apparatus for flow testing of gas through an arc-shaped component, comprising:

a test bench including a source of flowing gas and a housing defining a plenum chamber and an aperture for flowing of the gas into the component, said housing being adapted and configured to mount the component proximate to the aperture; and

a measurement section located downstream of and proximate to the aperture, said measurement section including an arc-shaped inner flowpath and an arc-shaped outer flowpath for receiving therebetween the gas exiting the component, said measurement section including a measurement device between the inner flowpath and the outer flowpath, said measurement device providing a signal in response to the flow of gas proximate thereto, said measurement device being rotatable about the centerline of the arc of the component.

2. The apparatus of claim 1 wherein said measurement section includes a platform with a plurality of measurement devices each located between the inner flowpath and the outer flowpath, said platform being rotatable about the centerline.

3. The apparatus of claim 1 wherein said measurement section includes a plurality of measurement devices, each measurement device has a length in the radial direction between the inner flowpath and the outer flowpath, and each length is different.

4. The apparatus of claim 3 wherein each measurement device includes a sensor, and the sensor is one of a strain gage, pressure transducer, accelerometer, anemometer including a wire, or piezoresistive element.

5. The apparatus of claim 4 wherein at least one of said measurement devices is in the shape of an airfoil.

6. The apparatus of claim 1 wherein said apparatus includes as the component an arc-shaped vane for a gas turbine engine.

7. The apparatus of claim 6 wherein said measurement device includes a sensor for measuring the angular position of said measurement device relative to the component.

8. The apparatus of claim 1 which further comprises a sensor producing a signal corresponding to the torque imparted by the airflow onto said measurement device.

9. The apparatus of claim 1 wherein said measurement device is in the shape of an airfoil.

10. The apparatus of claim 1 wherein said measurement device is in the shape of a plate.

11. The apparatus of claim 1 wherein said measurement device is in the shape of a rod.

12. The apparatus of claim 1 wherein said measurement section includes a plurality of measurement devices.

13. The apparatus of claim 12 wherein each said measurement device includes a sensor producing a signal corresponding to the torque imparted by the airflow onto said measurement device.

14. The apparatus of claim 13 wherein at least one of said measurement devices is in the shape of an airfoil.

15. The apparatus of claim 1 wherein said housing is adapted and configured for mounting a vane for a gas turbine engine.

16. The apparatus of claim 15 wherein the gas flowing through said measurement section exits said measurement section by flowing into ambient conditions.

17. The apparatus of claim 1 wherein the gas flowing through said measurement section exits said measurement section by flowing into ambient conditions.

18. An apparatus for flow testing of gas through a component, comprising:

a test bench including a source of flowing gas and a housing defining a plenum chamber and an aperture for flowing of the gas into the component, said housing being adapted and configured to mount the component proximate to the aperture; and

a measurement section located downstream of and proximate to the aperture, said measurement section including an inner flowpath and an outer flowpath for receiving therebetween the gas exiting the component, said measurement section including at least two circumferentially spaced-apart measurement devices each located between the inner flowpath and the outer flowpath, each said measurement device providing a signal in response to the flow of gas proximate thereto, each measurement device having a length in the radial direction between the inner flowpath and the outer flowpath, and each length being different.

19. The apparatus of claim 18 wherein each said measurement device is in the shape of an airfoil.

20. The apparatus of claim 18 wherein each said measurement device is in the shape of a plate.

21. The apparatus of claim 18 wherein each said measurement device is in the shape of a rod.

22. The apparatus of claim 18 wherein the component is arc-shaped and said measurement section is rotatable across the arc.

23. The apparatus of claim 22 wherein said measurement section includes a sensor for measuring the angular position of said measurement device relative to the component.

24. The apparatus of claim 18 wherein at least one of said measurement devices includes a sensor, and the sensor is one of a strain gage, pressure transducer, accelerometer, anemometer including a wire, or piezoresistive element.

25. The apparatus of claim 18 wherein said housing is adapted and configured for mounting a vane for a gas turbine engine.

26. The apparatus of claim 25 wherein the gas flowing through said measurement section exits said measurement section by flowing into ambient conditions.

27. The apparatus of claim 18 wherein the gas flowing through said measurement section exits said measurement section by flowing into ambient conditions.

28. The apparatus of claim 18 which further comprises a sensor producing a signal corresponding to the torque imparted by the airflow onto said measurement device.

29. An apparatus for flow testing of gas through a component, comprising:

a test bench including a source of flowing gas and a housing defining a plenum chamber and an aperture for flowing of the gas into the component, said housing being adapted and configured to mount the component proximate to the aperture; and

means for simultaneously measuring properties of the gas exiting from the component at a plurality of radial locations and a plurality of circumferential locations, said measuring means being rotatable transverse to the flowpath of the component.

30. The apparatus of claim 29 wherein said measuring means includes a plurality of devices each adapted and configured to bend in response to the gas flowing out of the component and around the device.

31. The apparatus of claim 30 wherein at least one of said measurement devices is in the shape of an airfoil.

32. The apparatus of claim 30 wherein at least one of said measurement devices is in the shape of a plate.

33. The apparatus of claim 30 wherein at least one of said measurement devices is in the shape of a rod.

34. The apparatus of claim 30 wherein said measuring means includes a sensor producing a signal corresponding to the torque imparted by the airflow onto said measuring means.

35. The apparatus of claim 29 wherein said housing is adapted and configured for mounting a vane for a gas turbine engine.

36. The apparatus of claim 35 wherein the gas flowing through said measuring means exits said measuring means by flowing into ambient conditions.

37. The apparatus of claim 29 wherein the gas flowing through said measuring means exits said measuring means by flowing into ambient conditions.

38. The apparatus of claim 29 wherein the component is arc-shaped and said measurement section is rotatable across the arc.

39. The apparatus of claim 38 which further comprises a sensor for measuring the angular position of said measuring means relative to the component.

40. The apparatus of claim 29 wherein said measuring means includes a sensor, and the sensor is one of a strain gage, pressure transducer, accelerometer, anemometer including a wire, or piezoresistive element.