Methods for the design, quality control, and management of fatigue-limited metal components

• US 5,625,664 A
• Filed: 10/11/1995
• Issued: 04/29/1997
• Est. Priority Date: 05/18/1994
• Status: Expired due to Term

• Current Assignee: Proto Manufacturing, Ltd. (Proto Manufacturing, Inc.)
• Original Assignee: Fatigue Management Associates LLC
• Inventors: Berkley, Stanley G.
• Primary Examiner(s): WONG, DON KITSUN
• Application Number:
  US08/540,876
• Time in Patent Office: 566 Days
• Field of Search: 378/58, 378/59, 378/70, 378/72, 378/71
• US Class Current: 378/72
• CPC Class Codes: B23K 31/12 relating to investigating the properties, e.g. the weldability, of materials
• CPC Class Codes: F02B 77/081 relating to endless members endless members, e.g. belts, for driving auxiliary apparatus F02B67/04
• CPC Class Codes: G01L 5/0047 measuring forces due to residual stresses
• CPC Class Codes: G01N 23/20 by using diffraction of the radiation by the materials, e.g. for investigating crystal structure; by using scattering of the radiation by the materials, e.g. for investigating non-crystalline materials; by using reflection of the radiation by the materials

Abstract

Improved methods for managing a population of metal components subject to fatigue failure are provided. The residual compressive stress in the critical surfaces of such components, especially in areas of high stress concentration, are measured non-destructively using x-ray diffraction techniques. The measured surface residual compressive stress is used as a management criterion. A component having a surface residual compressive stress greater than a predetermined value can be returned to service. However, once the measured surface residual compressive stress of a component falls below the predetermined value, it can either be removed permanently from service, or it can be reworked to increase its surface residual compressive stress and then returned to service. Additionally, by measuring the surface residual compressive stress of an individual component, the remaining service life of that individual component can be estimated. These methods for management of populations of such metal components allow for increasing the service life of the components in a safe and effective manner. Methods are also provided for the manufacture and/or design of metal parts with improved performance criterion (e.g., reduction in weight) while maintaining acceptable service life. Methods are also provided for establishing quality control procedures using surface residual compressive stress measurements during and/or after the manufacturing process in order to prevent, for example, introduction of metal parts having insufficient surface residual compressive stress levels for their intended use.

Claims

1. A method for designing a fatigue-limited metal part whereby a selected performance criterion for the metal part is improved while maintaining sufficient residual compressive stress to achieve an acceptable service life for the metal part, said method comprising:

(1) providing a prototype of the metal part;

(2) measuring the residual compressive stress in one or more critical surface areas of the prototype during the course of design of the metal part;

(3) modifying the prototype using the difference between the measured residual compressive stress and a predetermined residual compressive stress design level as a guide to improve the selected performance criterion;

(4) remeasuring the residual compressive stress in the one or more critical surface areas of the modified prototype to determine the remeasured residual compressive stress in comparison to the predetermined residual compressive stress design level in order to gauge the effect of the modification; and

(5) repeating steps (2) through (4) for the one or more critical surface areas until an acceptable and functional metal part is obtained, wherein the acceptable and functional metal part has its selected performance criterion improved and has sufficient residual compressive stress in the one or more critical surface areas for its intended use.

2. A method as defined in claim 1, wherein the residual compressive stress and the remeasured residual compressive stress are measured using x-ray diffraction techniques.

3. A method as defined in claim 1, wherein the metal part is a rotating part used in a gas turbine or jet engine.

4. A method as defined in claim 2, wherein the metal part is a rotating part used in a gas turbine or jet engine.

5. A method as defined in claim 3, wherein the metal parts is a disk or a drum rotor.

6. A method as defined in claim 4, wherein the metal part is a disk or a drum rotor.

8. A method as defined in claim 3, wherein the selected performance criterion is a reduction in weight of the metal part.

9. A method as defined in claim 4, wherein the selected performance criterion is a reduction in weight of the metal part.

7. A method as defined in claim is wherein the selected performance criterion is a reduction in weight of the metal part.

10. A method for designing a fatigue-limited metal part whereby the weight of the metal part is reduced while maintaining sufficient residual compressive stress to achieve an acceptable service life for the metal part, said method comprising:

(1) providing a prototype of the metal part;

(2) measuring the residual compressive stress in one or more critical surface areas of the prototype during the course of the design of the metal part;

(3) modifying the prototype using the difference between the measured residual compressive stress and a predetermined residual compressive stress design level as a guide;

(4) remeasuring the residual compressive stress in the one or more critical surface areas of the modified prototype to determine the remeasured residual compressive stress in comparison to the predetermined residual compressive stress design level in order to gauge the effect of the modification; and

(5) repeating steps (2) through (4) for the one or more critical surface areas until an acceptable and functional metal part is obtained having reduced weight and sufficient residual compressive stress in the one or more critical surface areas for its intended use.

11. A method as defined in claim 10, wherein the residual compressive stress and the remeasured residual compressive stress are measured using x-ray diffraction techniques.

12. A method as defined in claim 10, wherein the metal part is a rotating part used in a gas turbine or jet engine.

13. A method as defined in claim 11, wherein the metal part is a rotating part used in a gas turbine or jet engine.

14. A method as defined in claim 12, wherein the metal part is a disk or a drum rotor.

15. A method as defined in claim 13, wherein the metal part is a disk or a drum rotor.

16. A method for designing a fatigue-limited metal part whereby the weight of the metal part is minimized while maintaining sufficient residual compressive stress to achieve an acceptable service life and safety factor for the metal part, said method comprising:

(1) providing a prototype of the metal part;

(2) measuring the residual compressive stress in one or more critical surface areas of the prototype during the course of the design of the metal part;

(3) modifying the prototype by reducing its weight using the difference between the measured residual compressive stress and a predetermined residual compressive stress design level as a guide;

(4) remeasuring the residual compressive stress in the one or more critical surface areas of the modified prototype to determine the remeasured residual compressive stress in comparison to the predetermined residual compressive stress design level in order to gauge the effect of the modification; and

(5) repeating steps (2) through (4) for the one or more critical surface areas until an acceptable and functional metal part is obtained having minimal weight and sufficient residual compressive stress in the one or more critical surface areas to achieve an acceptable service life and safety factor for the metal part.

17. A method as defined in claim 16, wherein the residual compressive stress and the remeasured residual compressive stress are measured using x-ray diffraction techniques.

18. A method as defined in claim 16, wherein the metal part is a rotating part used in a gas turbine or jet engine.

19. A method as defined in claim 17, wherein the metal part is a rotating part used in a gas turbine or jet engine.

20. A method as defined in claim 18, wherein the metal part is a disk or a drum rotor.

21. A method as defined in claim 19, wherein the metal part is a disk or a drum rotor.

22. A quality control method for the manufacture of fatigue-limited metal components, said method comprising measuring the residual compressive stress in one or more critical surface areas for each metal component after its manufacture and before placing it into service, comparing the measured residual compressive stress in one or more critical surface areas to a corresponding predetermined residual compressive stress level for the one or more critical surfaces, and flagging each metal component which has its measured residual compressive stress below its corresponding predetermined residual compressive stress level, whereby flagged metal components are not placed in service.

23. A quality control method as defined in claim 22, wherein the flagged metal components are destroyed or otherwise mutilated to prevent unauthorized use.

24. A quality control method as defined in claim 22, wherein the flagged metal components are reworked to increase the residual compressive stress in the one or more critical surface areas to levels above the corresponding predetermined residual compressive stress, whereby the reworked metal components can be placed in service.

25. A quality control method as defined in claim 22, wherein the residual compressive stress in one or more critical surface areas for each metal component is determined using x-ray diffraction techniques.

26. A quality control method as defined in claim 23, wherein the residual compressive stress in one or more critical surface areas for each metal component is determined using x-ray diffraction techniques.

27. A quality control method as defined in claim 24, wherein the residual compressive stress in one or more critical surface areas for each metal component is determined using x-ray diffraction techniques.