Method and apparatus for measuring ice thickness on substrates using backscattering of gamma rays

• US 6,049,282 A
• Filed: 10/05/1998
• Issued: 04/11/2000
• Est. Priority Date: 08/30/1994
• Status: Expired due to Fees

• Current Assignee: University of Guelph
• Original Assignee: University of Guelph
• Inventors: MacKenzie, Innes K.
• Primary Examiner(s): Lee, Benjamin C.
• Application Number:
  US09/166,720
• Time in Patent Office: 554 Days
• Field of Search: 340/583, 340/962, 340/580, 340/600, 250/320.09, 378/89, 378/90, 702/137, 702/172, 73/590, 62/140, 244/134 F
• US Class Current: 340/583
• CPC Class Codes: B64D 15/20 Means for detecting icing or initiating de-icing
• CPC Class Codes: G01B 15/02 for measuring thickness

Abstract

The present invention provides a method and apparatus for in situ measuring thicknesses of ice buildup on airfoil. The method and device uses a probe including a radioactive ²⁴¹ Am gamma ray source producing 60 keV gamma ray photons which penetrate through the airfoil substrate and a photodetector mounted behind the source for detection of backscattered gamma rays. The probe is mounted on the interior of the airfoil and secondary radiation is backscattered within the ice layer and back through the airfoil substrate to the photodetector. The shape and density of the source holder in addition to the geometrical arrangement of the source and detector with respect to the airfoil substrate are used to block a substantial fraction of gamma rays backscattered in the airfoil substrate thereby favoring scattering in the ice layer over that in the airfoil material.

Claims

1. A method for measuring ice buildup on an outer surface of a substrate, comprising:

providing a gamma ray source in a source holder, the gamma ray source producing a beam of primary gamma rays having sufficient energy to penetrate through said substrate;

providing a photodetection means behind said source holder and positioning said source holder adjacent to an inner surface of said substrate so that the beam of primary gamma rays are directed through said substrate away from the photodetection means, wherein the source holder shields said photodetection means from primary gamma rays from the gamma ray source and shields said photodetection means from at least some of the gamma rays scattered in said substrate; and

measuring an intensity of backscattered gamma rays at said photodetection means and determining from said intensity of gamma rays a thickness of ice buildup on said outer surface of said substrate.

2. The method according to claim 1 wherein the step of determining a thickness of ice buildup includes measuring a background intensity of gamma rays measured by said photodetection means from an ice-free substrate and subtracting said background intensity from said intensity of gamma rays.

3. The method according to claim 2 wherein the step of providing a gamma ray source in a source holder includes providing a cylindrically symmetric source holder to provide an axially symmetric beam of primary gamma rays emerging from said source holder.

4. The method according to claim 3 wherein the gamma ray source is radioactive ²⁴¹ Am.

5. The method according to claim 4 wherein the step of measuring the intensity of backscattered gamma rays includes measuring said intensity with a Nal(TI) X-ray scintillator coupled with a photomultiplier detector.

6. The method according to claim 5 including adjusting the position of the radioactive source in the source holder to control collimation of the beam of primary gamma rays.

7. The method according to claim 1 including measuring a rate of ice buildup on said substrate.

8. An apparatus for measuring an ice layer buildup on an outer surface of an airfoil, comprising:

a) at least one probe mounted on an interior surface of an airfoil, said at least one probe including a source holder containing a source of gamma rays having energies sufficiently high to penetrate through said airfoil, a photodetection means located behind said source holder for measuring an intensity of backscattered photons, the photodetection means being positioned with respect to said source holder so that said source holder blocks primary gamma rays from said source from impinging on said photodetection means and shields said photodetection means from at least some secondary gamma rays backscattered in said airfoil, and wherein gamma rays emerging from said source holder are directed away from said photodetection means; and

b) processing means connected to said photodetection means for calculating a thickness of an ice layer from said intensity of backscattered gamma rays.

9. The apparatus according to claim 8 wherein said source holder and said photodetection means are cylindrically symmetric and are aligned along a common cylindrical axis.

10. The apparatus according to claim 9 wherein said photodetection means includes a cylindrical Nal(TI) X-ray scintillator having a front face, said source holder being mounted on said front face.

11. The apparatus according to claim 10 wherein said photodetection means includes a photomultiplier detector coupled with said Nal(TI) X-ray scintillator.

12. The apparatus according to claim 11 wherein the source holder includes a cylindrical post constructed of a metal selected from the group consisting of molybdenum, gold, platinum, lead, silver, tantalum and tungsten and having dimensions suitable to block primary gamma rays from said source of gamma rays from impinging directly on said photodetection means.

13. The apparatus according to claim 12 wherein said cylindrical post has a preselected diameter so that said cylindrical post absorbs a portion of secondary photons scattered in said airfoil adjacent to said cylindrical post.

14. The apparatus according to claim 13 wherein the source of gamma rays is radioactive ²⁴¹ Am.

15. The apparatus according to claim 13 wherein said processing means is connected to a display means connected to each of said probes for displaying a thickness of an ice layer.

16. The apparatus according to claim 15 wherein said processing means is adapted to calculate a rate of ice buildup on said airfoil.

17. The apparatus according to claim 10 wherein the source of gamma rays is radioactive ²⁴¹ Am.

18. The apparatus according to claim 17 wherein said radioactive ²⁴¹ Am has a source strength in the range from about 1 microcurie to about 30 millicuries.

19. The apparatus according to claim 8 wherein the source holder includes a cylindrical post constructed of a metal selected from the group consisting of molybdenum, gold, platinum, lead, silver, tantalum and tungsten and having dimensions suitable to block primary gamma rays from said source of gamma rays from impinging directly on said photodetection means.

20. The apparatus according to claim 19 wherein said cylindrical post has a preselected diameter so that said cylindrical post absorbs a portion of secondary gamma rays scattered in said airfoil adjacent to said cylindrical post.

21. The apparatus according to claim 20 wherein the source holder includes adjustment means for adjusting the position of the source of gamma rays in the source holder to control collimation of a beam of primary gamma rays emerging from said source holder.

22. The apparatus according to claim 8 wherein said at least one probe is a plurality of probes each mounted at a different location on said airfoil.

23. The apparatus according to claim 22 wherein said processing means is connected to a display means connected to each of said probes for displaying a thickness of an ice layer.

24. The apparatus according to claim 8 wherein said processing means is adapted to calculate a rate of ice buildup on said airfoil.