Methods and systems for evaluating defects in metals

• US 6,512,982 B2
• Filed: 12/20/2000
• Issued: 01/28/2003
• Est. Priority Date: 12/20/2000
• Status: Expired due to Fees

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Yang, Ling, Falsetti, Robert
• Primary Examiner(s): SHAH, KAMINI S
• Application Number:
  US09/742,667
• Publication Number:
  US 20020111749A1
• Time in Patent Office: 769 Days
• Field of Search: 702/34, 702/36, 702/1, 702/108, 700/30, 700/31, 700/106, 707/102, 707/103, 735/79, 735/87, 736/02
• US Class Current: 702/34
• CPC Class Codes: G01B 3/44 preadjustable for wear or tolerance
• CPC Class Codes: G01N 33/2045 Defects
• CPC Class Codes: Y10S 707/99943 Generating database or data structure, e.g. via user interface

Abstract

A method and system for evaluating structural defects in metals is provided. In one embodiment, the method recognizes that the acceptability of a given defect is principally determined by the four basic parameters of operating temperature, operating stress, defect area, and defect shape. Ranges are established for each of these four basic parameters, and intermediate values within these ranges are selected to create a series of index value data sets. The method evaluates these index value data sets by calculating a life cycles estimate for each. Using statistical methods, the life cycles results are analyzed to determine the effect each of the four basic parameters has on the life of a component with a defect. Understanding the relationship between these four basic parameters and life cycles enables the method to provide an interpolation algorithm for finding the life cycles for any component having a defect.

Claims

1. A method in a computer system for estimating a number of life cycles a component having a defect can experience before failure, the component being subjected to an operating temperature and an operating stress during operation, the defect being definable by a defect dimension, the method comprising:

providing a temperature range comprising a plurality of temperature index values, a stress range comprising a plurality of stress index values, and a dimension range comprising a plurality of dimension index values;

providing a plurality of index value data sets, wherein each index value data set comprises one temperature index value, one stress index value, and one dimension index value;

determining life cycles estimates for a plurality of the index value data sets;

selecting two temperature index values that bracket the operating temperature, two stress index values that bracket the operating stress, and two dimension index values that bracket the defect dimension;

determining a temperature interpolation factor based on the two bracketing temperature index values and the operating temperature, a stress interpolation factor based on the two bracketing stress index values and the operating stress, and a dimension interpolation factor based on the two bracketing dimension index values and the defect dimension; and

determining a life cycles estimate for the component having the defect based on the temperature interpolation factor, the stress interpolation factor, the dimension interpolation factor, and a plurality of the index value data set life cycles.

2. A method in a computer system for estimating a number of life cycles a component having a defect can experience before failure, the component being subjected to an operating temperature and an operating stress during operation, the defect being definable by a defect dimension, the method comprising:

providing a first parameter data set comprising a first temperature parameter, a first stress parameter, and a first dimension parameter;

providing a second parameter data set comprising a second temperature parameter, a second stress parameter, and a second dimension parameter;

providing a third parameter data set comprising a third temperature parameter, a third stress parameter, and a third dimension parameter, wherein the third temperature parameter is between the first and second temperature parameters, the third stress parameter is between the first and second stress parameters, and the third dimension parameter is between the first and second dimension parameters;

determining a first number of life cycles based on the first parameter data set;

determining a second number of life cycles based on the second parameter data set; and

determining a third number of life cycles based on the first and second numbers of life cycles.

3. The method of claim 2 wherein the third number of life cycles is determined based on the first number of life cycles, the second number of life cycles, and the relationship between the third parameter data set and the first and second parameter data sets.

4. The method of claim 2 wherein the third number of life cycles is determined by interpolation.

5. The method of claim 2 wherein the third number of life cycles is determined by extrapolation.

6. A method in a computer system for evaluating a metallic component having a defect, the method comprising:

providing two or more index value data sets, wherein each index value data set comprises a temperature index value, a stress index value, and a dimension index value;

evaluating the two or more index value data sets to determine a measure of performance for each of the two or more index value data sets; and

interpolating between the measures of performance for the two or more index value data sets to determine a measure of performance for the metallic component having the defect.

7. The method of claim 6 wherein the measures of performance determined for the two or more index value data sets are numbers of life cycles, and the measure of performance determined for the metallic component is a number of life cycles.

8. The method of claim 6 wherein the measures of performance determined for the two or more index value data sets are strength limits, and the measure of performance determined for the metallic component is a strength limit.

9. The method of claim 6 wherein the metallic component is an IN718 nickel alloy component.

10. The method of claim 6 wherein interpolating between the measures of performance includes calculating a logarithm of one of the measures of performance of the index value data sets.

11. The method of claim 6 further comprising:

providing a display description of the measure of performance for the metallic component having the defect, the display description comprising;

a green colored display portion if the measure of performance for the metallic component is acceptable;

a red colored display portion if the measure of performance for the metallic component is unacceptable; and

a yellow colored display portion if the measure of performance for the metallic component is questionable.

12. The method of claim 6 further comprising:

receiving a defect data set, wherein the defect data set comprises a temperature value, a stress value, and a dimension value; and

wherein

interpolating between the measures of performance includes evaluating the relationship between the defect data set and one or more of the index value data sets.

13. The method of claim 12 wherein the dimension value in the defect data set is an area value.

14. The method of claim 12 wherein the dimension value in the defect data set is a shape value.

15. The method of claim 14 wherein the shape value is a length-to-width ratio.

16. A method in a computer system for evaluating a metallic component having a defect, the method consisting essentially of:

providing a temperature parameter, a stress parameter, an area parameter and a shape parameter corresponding to the defect; and

calculating a measure of performance for the component based on the temperature, stress, area and shape parameters.

17. The method of claim 16 wherein the measure of performance is a number of life cycles.

18. The method of claim 16 wherein the measure of performance is a strength limit.

19. The method of claim 16 wherein the metallic component is an IN718 nickel alloy component.

20. The method of claim 16 wherein the shape parameter is a ratio of the length of the defect to the width of the defect.

21. A method for estimating a number of life cycles a component having a defect can experience before failure, the component being subjected to an operating temperature and an operating stress during operation, the defect being definable by a defect dimension, the method comprising:

providing a first life cycles estimate corresponding to a first parameter data set;

providing a second life cycles estimate corresponding to a second parameter data set;

providing a defect parameter data set; and

determining a defect life cycles estimate based on the first and second life cycles estimates and the defect parameter data set.

22. The method of claim 21 wherein:

the first parameter data set comprises a first temperature parameter, a first stress parameter, or a first dimension parameter; and

the second parameter data set comprises a second temperature parameter, a second stress parameter, or a second dimension parameter.

23. The method of claim 21 wherein:

the first parameter data set comprises a first temperature parameter, a first stress parameter, or a first dimension parameter;

the second parameter data set comprises a second temperature parameter, a second stress parameter, or a second dimension parameter; and

the defect parameter data set comprises a defect temperature parameter, a defect stress parameter, or a defect dimension parameter, wherein the defect temperature parameter is between the first and second temperature parameters, the defect stress parameter is between the first and second stress parameters, and the defect dimension parameter is between the first and second dimension parameters.

24. The method of claim 23 wherein the defect dimension parameter is an area parameter.

25. The method of claim 23 wherein the defect dimension parameter is a shape parameter.

26. The method of claim 21 wherein:

the first parameter data set comprises a first temperature parameter, a first stress parameter, and a first dimension parameter;

the second parameter data set comprises a second temperature parameter, a second stress parameter, and a second dimension parameter; and

the defect parameter data set comprises a defect temperature parameter, a defect stress parameter, and a defect dimension parameter, wherein the defect temperature parameter is between the first and second temperature parameters, the defect stress parameter is between the first and second stress parameters, and the defect dimension parameter is between the first and second dimension parameters.

27. The method of claim 21 wherein the component is an IN718 nickel alloy component.

28. The method of claim 21 wherein determining the defect life cycles estimate includes interpolating between the first and second life cycles estimates.

29. The method of claim 28 wherein interpolating between the first and second life cycles estimates includes calculating a logarithm of one of the life cycles estimates.

30. The method of claim 21 wherein determining the defect life cycles estimate includes logarithmically interpolating between the first and second life cycles estimates.

31. The method of claim 21 wherein:

the first parameter data set comprises a first temperature parameter and a first stress parameter; and

the second parameter data set comprises a second temperature parameter and a second stress parameter.

32. The method of claim 31 wherein the defect parameter data set comprises a defect temperature parameter and a defect stress parameter, and wherein the defect temperature parameter is between the first and second temperature parameters, and the defect stress parameter is between the first and second stress parameters.

33. The method of claim 21 wherein:

the first parameter data set comprises a first temperature parameter and a first dimension parameter; and

the second parameter data set comprises a second temperature parameter and a second dimension parameter.

34. The method of claim 33 wherein the defect parameter data set comprises a defect temperature parameter and a defect dimension parameter, and wherein the defect temperature parameter is between the first and second temperature parameters, and the defect dimension parameter is between the first and second dimension parameters.

35. The method of claim 21 wherein:

the first parameter data set comprises a first stress parameter and a first dimension parameter; and

the second parameter data set comprises a second stress parameter and a second dimension parameter.

36. The method of claim 35 wherein the defect parameter data set comprises a defect stress parameter and a defect dimension parameter, and wherein the defect stress parameter is between the first and second stress parameters, and the defect dimension parameter is between the first and second dimension parameters.

37. A display description for evaluating a metallic component having a defect, the defect being definable by a first defect dimension and a second defect dimension, the display description consisting essentially of:

a material input portion;

a temperature input portion;

a stress input portion;

a first defect dimension input portion; and

a second defect dimension input portion.

38. A computer system for evaluating a metallic component having a defect, the computer system comprising:

one or more interpolation factor components containing computer-executable instructions for determining one or more interpolation factors;

a life cycles component containing computer-executable instructions for calculating a number of life cycles for the metallic component using one or more of the interpolation factors;

a central processing unit for executing the computer-executable instructions for determining the one or more interpolation factors or the life cycles of the metallic component; and

an output device for displaying the life cycles of the metallic component.

39. The computer system of claim 38 wherein the one or more interpolation factor components comprise:

a temperature interpolation component containing computer-executable instructions for determining a temperature interpolation factor;

a stress interpolation component containing computer-executable instructions for determining a stress interpolation factor;

an area interpolation component containing computer-executable instructions for determining an area interpolation factor, and

a shape interpolation component containing computer-executable instructions for determining a shape interpolation factor.

40. The computer system of claim 38 wherein the life cycles component contains computer-executable instructions for calculating the number life cycles for the metallic component using logarithmic interpolation.

41. A computer system for estimating a number of life cycles a component having a defect can experience before failure, the component being subjected to an operating temperature and an operating stress during operation, the defect being definable by a defect dimension, the computer system comprising:

means for providing a first parameter data set;

means for providing a second parameter data set;

means for providing a third parameter data set corresponding to the component having the defect;

means for determining a first life cycles estimate based on the first parameter data set;

means for determining a second life cycles estimate based on the second parameter data set; and

means for determining a third life cycles estimate corresponding to the component having the defect, the third life cycles estimate being based on the first life cycles estimate, the second life cycles estimate, and the third parameter data set.

42. The computer system of claim 41 wherein:

the first parameter data set comprises a first temperature parameter, a first stress parameter, and a first dimension parameter;

the second parameter data set comprises a second temperature parameter, a second stress parameter, and a second dimension parameter; and

the third parameter data set comprises a third temperature parameter, a third stress parameter, and a third dimension parameter, wherein the third temperature parameter is between the first and second temperature parameters, the third stress parameter is between the first and second stress parameters, and the third dimension parameter is between the first and second dimension parameters.

43. A computer-readable medium whose contents cause a computer system to estimate a number of life cycles a component having a defect can experience before failure, the component being subjected to an operating temperature and an operating stress during operation, the defect being definable by a defect dimension, the number of life cycles being estimated by a method comprising:

providing a first life cycles estimate corresponding to a first parameter data set;

providing a second life cycles estimate corresponding to a second parameter data set;

providing a defect parameter data set corresponding to the defect; and

determining a defect life cycles estimate based on the first and second life cycles estimates and the defect parameter data set.

44. The computer-readable medium of claim 43 wherein:

the first parameter data set comprises a first temperature parameter, a first stress parameter, and a first dimension parameter;

the second parameter data set comprises a second temperature parameter, a second stress parameter, and a second dimension parameter; and

the defect parameter data set comprises the operating temperature, the operating stress, and the defect dimension, and wherein the operating temperature is between the first and second temperature parameters, the operating stress is between the first and second stress parameters, and the defect dimension is between the first and second dimension parameters.