Method for detecting stress and strain

• US 6,650,405 B2
• Filed: 05/21/2001
• Issued: 11/18/2003
• Est. Priority Date: 05/31/2000
• Status: Expired due to Term

• Current Assignee: Simpson Strong-Tie Company Incorporated (Simpson Manufacturing Company Incorporated)
• Original Assignee: Duhane Lam, Mark William Ellens
• Inventors: Lam, Duhane, Ellens, Mark William
• Primary Examiner(s): Frech, Karl D.
• Assistant Examiner(s): Kim, Ahshik
• Application Number:
  US09/861,510
• Publication Number:
  US 20020001073A1
• Time in Patent Office: 911 Days
• Field of Search: 356/32, 356/73, 356/33, 738/00
• US Class Current: 356/33
• CPC Class Codes: G01B 11/18 using photoelastic elements

Abstract

A method of detecting stress and strain using a powder coat finish and photoelastic techniques. A part is provided with a photoelastic layer comprising a non-opaque powder coat finish that becomes optically anisotropic when stressed. Photoelastic techniques are used to detect and measure stress and strain in the part. Fringe patterns appear in the photoelastic layer indicating the locations and magnitudes of the stress and strain when the part is illuminated with polarized light and viewed through a polarizing filter. Stress and strain resulting from applied forces are detected. Structural deformation in parts that have experienced plastic deformation is also detected. Photoelastic techniques using powder coat as a photoelastic technique are less expensive and easier to apply than traditional photoelastic coatings. Applications include testing of prototypes, stress testing, inspection and monitoring of production parts, and anywhere that viewing and measuring of stress and strain are of interest.

Claims

1. A method for detecting stress and strain, the method comprising:

a. providing a part coated with a photoelastic layer comprising non-opaque powder coat that becomes optically anisotropic when subjected to stress and strain;

b. detecting stress and strain in said part using the photoelastic properties of said photoelastic layer.

2. The method according to claim 1, wherein the step of providing a part coated with a photoelastic layer comprises applying a dry, finely divided solid to said part and curing the solid powder to form a continuous film which adheres to said part to form said photoelastic layer.

3. The method according to claim 2, wherein the step of applying a dry, finely divided solid comprises electrostatically applying the solid.

4. The method according to claim 1, wherein the step of providing a part coated with a photoelastic layer comprises providing a reflective layer and applying said photoelastic layer on top of said reflective layer.

5. The method according to claim 4, wherein the step of providing a reflective layer comprises applying a dry, finely divided solid to said part and curing the solid powder to form a continuous film which adheres to said part to form said reflective layer.

6. The method according to claim 1, wherein the step of providing a part coated with a photoelastic layer comprises applying said photoelastic layer directly to said part.

7. The method according to claim 1, wherein the step of providing a part coated with a photoelastic layer comprises sequentially applying a plurality of coats to form said photoelastic layer.

8. The method according to claim 1, wherein the powder coat comprises a polyester material.

9. The method according to claim 1, wherein the powder coat comprises the chemical triglycidyl isocyanurate.

10. The method according to claim 1, wherein said photoelastic layer is between 5 μ

m and 3000 μ

m thick.

11. The method according to claim 1, further comprising the step of observing fringe patterns in said photoelastic layer to quantify the stress and strain in said part.

12. The method according to claim 1, wherein the step of detecting stress and strain comprises:

a. illuminating said part with polarized light;

b. viewing the light reflected from said part through a polarizing filter to determine if fringe patterns are visible in said photoelastic layer.

13. The method according to claim 12, wherein said part is illuminated with circularly polarized light.

14. The method according to claim 12, wherein the step of viewing the reflected light comprises viewing the reflected light through a quarter-wave plate.

15. The method according to claim 12, wherein the step of viewing the reflected light comprises recording the reflected light with a camera.

16. A method for performing photoelastic analysis on a part comprising applying a photoelastic layer as a dry, finely divided solid and curing the solid powder to form a continuous film which adheres to said part, whereby stress and strain in said part can be detected.

17. The method according to claim 16 wherein said photoelastic layer comprises a non-opaque plastic which becomes optically anisotropic when stressed.

18. The method according to claim 16, comprising applying a reflective layer to the part prior to applying said photoelastic layer.

19. The method according to claim 18, wherein the step of applying said reflective layer comprises applying a dry, finely divided solid and curing the solid powder to form a continuous film which adheres to said part.

20. The method according to claim 16, wherein the step of applying said photoelastic layer comprises applying a plurality of coats to form said photoelastic layer.

21. The method according to claim 16, wherein the solid is a polyester powder coat.

22. The method according to claim 16, wherein the solid powder comprises the chemical triglycidyl isocyanurate.

23. The method according to claim 16, comprising applying said photoelastic layer such that said photoelastic layer has a thickness between 5 μ

m and 3000 μ

m.

24. A method for detecting plastic deformation, the method comprising:

a. providing a part coated with a photoelastic layer of non-opaque powder coat that becomes optically anisotropic when subjected to stress and strain;

b. applying a load to said part;

c. illuminating said part with a source of polarized light;

d. viewing the light reflected from said part through a polarizer after removal of said load;

whereby the presence of fringe patterns in said photoelastic layer indicates that plastic deformation of said part has occurred.

25. The method according to claim 24, comprising applying a reflective layer to said part prior to applying said photoelastic layer.

26. The method according to claim 25, wherein the step of applying said reflective layer comprises applying a dry, finely divided solid and curing the solid powder to form a continuous film which adheres to said part.

27. The method according to claim 24, wherein the step of providing a part coated with a photoelastic layer comprises sequentially applying a plurality of coats to form said photoelastic layer.

28. The method according to claim 24, wherein the powder is a polyester powder.

29. The method according to claim 24, wherein the powder comprises the chemical triglycidyl isocyanurate.

30. The method according to claim 24, wherein the photoelastic layer is between 5 μ

m and 3000 μ

m thick.