Method and system for determining crack nucleation of a part subject to fretting fatigue

• US 20030074976A1
• Filed: 09/04/2001
• Published: 04/24/2003
• Est. Priority Date: 09/04/2001
• Status: Active Grant

• Current Assignee: Jalees Ahmad
• Original Assignee: Jalees Ahmad
• Inventors: Ahmad, Jalees
• Granted Patent: US 6,612,181 B2
• Time in Patent Office: Days
• US Class Current: 73/808
• CPC Class Codes: G01N 2203/0005 Repeated or cyclic
• CPC Class Codes: G01N 2203/0019 Compressive
• CPC Class Codes: G01N 2203/0025 Shearing
• CPC Class Codes: G01N 2203/0026 Combination of several types of applied forces
• CPC Class Codes: G01N 2203/0064 Initiation of crack
• CPC Class Codes: G01N 2203/0073 Fatigue
• CPC Class Codes: G01N 3/32 by applying repeated or pulsating forces
• CPC Class Codes: G01N 3/56 Investigating resistance to wear or abrasion

Abstract

A method for determining crack nucleation for a part subject to fretting fatigue. Fretting fatigue tests are performed on at least one test specimen having a material composition similar to the part. The results of the test are analyzed to determine a variation of stress intensity factor as a function of time which may be referred to as (Q{N}) for the test specimen. A relationship is then determined between (Q{N}) and crack nucleation (N_i) for the test specimen. A variation of stress intensity factor as a function of time (Q{N}) for the part is determined based on the operating conditions and loads of the part. The (Q{N}) for the part is then corresponded to the (Q{N}) for the test specimen to determine a crack nucleation value (N_i) for the part. In a preferred embodiment, a computer is programmed to conduct the analysis.

Claims

1. A method for determining crack nucleation (N_i) for a part subject to fretting fatigue, comprising the steps of:

A) performing at least one fretting fatigue test on at least one test specimen, wherein said at least one test specimen is comprised of material similar to said part,

B) analyzing said at least one fretting fatigue test to determine a variation of stress intensity factor as a function of time (Q{N}) for said at least one test specimen,

C) determining a relationship between said stress intensity factor as a function of time (Q{N}) and said crack nucleation (N_i) for said at least one test specimen, and

D) determining a variation of stress intensity factor as a function of time (Q{N}) for said part under operating conditions and loads of said part,

E) corresponding said variation of stress intensity factor as a function of time (Q{N}) for said part to said variation of stress intensity factor as a function of time (Q{N}) for said at least one test specimen to determine a crack nucleation (N_i) for said part.

2. The method as in claim 1, wherein said at least one fretting fatigue test is a plurality of fretting fatigue tests and said at least one test specimen is a plurality of test specimens.

3. The method as in claim 1, wherein said operating loads and conditions are projected operating loads and conditions.

4. The method as in claim 1, wherein said operating loads and conditions are actual operating loads and conditions.

5. The method as in claim 1, wherein said at least one test specimen is comprised of material identical to said part.

6. The method as in claim 1, wherein said crack nucleation (N_i) for said at least one test specimen is specimen failure (N_f).

7. The method as in claim 1, wherein said analyzing said at least one fretting fatigue test to determine a variation of stress intensity factor as a function of time (Q{N}) for said at least one test specimen is accomplished utilizing a closed form procedure.

8. The method as in claim 1, wherein said analyzing said at least one fretting fatigue test to determine a variation of stress intensity factor as a function of time (Q{N}) for said at least one test specimen is accomplished utilizing a numerical mathematical procedure.

9. The method as in claim 8, wherein said numerical mathematical procedure is the finite element method.

10. The method as in claim 1, wherein said determining a variation of stress intensity factor as a function of time (Q{N}) for said part under the operating conditions and loads of said part is accomplished utilizing a closed form procedure.

11. The method as in claim 1, wherein said determining a variation of stress intensity factor as a function of time (Q{N}) for said part under the operating conditions and loads of said part is accomplished utilizing a numerical mathematical procedure.

12. The method as in claim 11, wherein said numerical mathematical procedure is the finite element method.

13. The method as in claim 1, further comprising the step of modifying the design of said part to extend said crack nucleation (N_i) for said part and then repeating said steps as necessary until a desired crack nucleation (N_i) for said part is achieved.

14. The method as in claim 1, further comprising the step of modifying the material composition of said part to extend said crack nucleation (N_i) for said part and then repeating said steps as necessary until a desired crack nucleation (N_i) for said part is achieved.

15. The method as in claim 1, further comprising the step of modifying the surface characteristics of said part to extend said crack nucleation (N_i) for said part and then repeating said steps as necessary until a desired crack nucleation (Ns) for said part is achieved.

16. The method as in claim 1, further comprising the step of modifying the material composition and the design of said part to extend said crack nucleation (N_i) for said part and then repeating said steps as necessary until a desired crack nucleation (N_i) for said part is achieved.

26. The computer as in claim 16, wherein said determining a variation of stress intensity factor as a function of time (Q{N}) for said part under the operating conditions and loads of said part is accomplished utilizing a closed form procedure.

27. The computer as in claim 16, wherein said determining a variation of stress intensity factor as a function of time (Q{N}) for said part under the operating conditions and loads of said part is accomplished utilizing a numerical mathematical procedure.

28. The computer as in claim 27, wherein said numerical mathematical procedure is the finite element method.

17. A computer system for determining crack nucleation (N_i) in a part subject to fretting fatigue, comprising:

A) a computer processor, and

B) a memory unit connected to said processor and storing a program for controlling the operation of said processor, said processor operative with said program in said memory to;

1) analyze the results of at least one fretting fatigue test to determine the variation of stress intensity factor as a function of time (Q{N}) for at least one test specimen, wherein said at least one fretting fatigue test was performed on at least one test specimen, wherein said at lest one test specimen is comprised of material similar to said at least one part,

2) determine a relationship between said stress intensity factor as a function of time (Q{N}) and said crack nucleation (N_i) for said at least one test specimen,

3) determine a variation of stress intensity factor as a function of time (Q{N}) for said part under the operating conditions and loads of said part, and

4) correspond said variation of stress intensity factor as a function of time (Q{N}) for said part to said variation of stress intensity factor as a function of time (Q{N}) for said at least one test specimen to determine a crack nucleation (N_i) for said part.

18. The computer as in claim 17, wherein said at least one fretting fatigue test is a plurality of fretting fatigue tests and said at least one test specimen is a plurality of test specimens.

19. The computer as in claim 17, wherein said operating loads and conditions are projected operating loads and conditions.

20. The computer as in claim 17, wherein said operating loads and conditions are actual operating loads and conditions.

21. The computer as in claim 17, wherein said at least one test specimen is comprised of material identical to said part.

22. The computer as in claim 17, wherein said crack nucleation (N_i) for said at least one test specimen is specimen failure (N_f).

23. The computer as in claim 17, wherein said analyzing said at least one fretting fatigue test to determine a variation of stress intensity factor as a function of time (Q{N}) for said at least one test specimen is accomplished utilizing a closed form procedure.

24. The computer as in claim 17, wherein said analyzing said at least one fretting fatigue test to determine a variation of stress intensity factor as a function of time (Q{N}) for said at least one test specimen is accomplished utilizing a numerical mathematical procedure.

25. The method as in claim 24, wherein said numerical mathematical procedure is the finite element method.