Method and device for visually measuring structural fatigue using a temperature sensitive coating

• US 6,575,620 B1
• Filed: 02/15/2000
• Issued: 06/10/2003
• Est. Priority Date: 02/15/2000
• Status: Expired due to Fees

• Current Assignee: Air Force Government of The United States of America As Represented By The Secretary
• Original Assignee: United States Of America As Represented By The Secretary Of The Air Force
• Inventors: Watkins, A. Neal, Dale, Gary, Banaszak, David, Jordan, Jeffrey D.
• Primary Examiner(s): Gutierrez, Diego
• Assistant Examiner(s): VERBITSKY, GAIL KAPLAN
• Application Number:
  US09/504,428
• Time in Patent Office: 1,211 Days
• Field of Search: 374/4-7, 374/4.5, 374/46, 374/57, 374/117, 374/192, 374/52, 374/118, 736/62, 736/63, 736/68, 736/65, 738/02, 735/83, 735/77, 738/08
• US Class Current: 374/4
• CPC Class Codes: G01N 21/6447 by visual observation
• CPC Class Codes: G01N 2203/0064 Initiation of crack
• CPC Class Codes: G01N 2203/0066 Propagation of crack
• CPC Class Codes: G01N 2203/0073 Fatigue
• CPC Class Codes: G01N 2203/0222 Temperature
• CPC Class Codes: G01N 2203/0694 Temperature
• CPC Class Codes: G01N 25/72 Investigating presence of flaws
• CPC Class Codes: G01N 3/068 with optical indicating or recording means

Abstract

A method and device for visually detecting crack length of a temperature sensitive paint coated test structure during excitation of the test structure. The method and device of the invention capitalizes on surface temperature changes of the test structure as structural fatigue increases. Test structure surface temperature changes are realized in corresponding fluorescence intensity changes in the temperature sensitive paint and recorded with a CCD camera. Improvements over conventional structural fatigue systems include the ability to detect fatigue during flight testing, to record fatigue without stopping the electrodynamic excitation and the ability to detect crack onset and crack length resulting in more accurate cycles-to-fatigue analysis.

Claims

1. A visual structural fatigue crack length measurement device comprising:

a test structure having a temperature responsive paint coating;

a test structure mechanical excitation means for resonance and narrowband random excitation, said resonance and narrowband random excitation increasing a rate of fatigue crack generation in said test structure wherein, said test structure mechanical excitation means comprises;

a signal generator, an excitation signal waveform filter and power amplifier connected to said signal generator, an electrodynamic shaker, and a test structure receiving fixture attaching said test structure to said electrodynamic shaker;

a test structure mechanical excitation means signal recorder;

a video system for viewing and acquiring images of thermal sensitivity variations of the temperature responsive paint coating and for measuring the fatigue crack length in the test structure based on said acquired images wherein, the intensity variations in said temperature responsive paint coating correspond to variations in local temperature of said test structure; and

wherein, the variations in the local temperature correspond to said test structure fatigue crack.

2. The visual structural fatigue crack length measurement device of claim 1 wherein said test structure mechanical excitation means signal recorder comprises a test structure excitation signal time history recording sensor connected to a signal generator connected filter and a power amplifier.

3. The visual structural fatigue crack length measurement device of claim 1 wherein said thermal sensitivity variations viewing video system comprises:

a blue light;

a CCD; and

video processing software.

4. The visual structural fatigue crack length measurement device of claim 1 further comprising a temperature sensitive paint coating receiving and stabilizing white base coat applied to said test structure.

5. The visual structural fatigue crack length measurement device of claim 4 wherein said test structure paint coating further comprises a probe doped active sol-gel temperature sensitive paint.

6. The visual structural fatigue crack length measurement device of claim 4 wherein said test structure paint coating further comprises a luminescent probe containing sol-gel temperature sensitive paint.

7. The visual structural fatigue crack length measurement device of claim 4 wherein said probe doped active sol-gel temperature sensitive paint comprises platinum meso tetra (pentafluorophenyl)porphine.

8. A visual structural fatigue crack length measurement method comprising the steps:

coating a test structure with a fluorescent intensity varying fatigue-responsive temperature sensitive paint coating,

generating a test structure excitation signal by using a test structure mechanical excitation means capable of resonance and narrowband random excitation, said resonance and narrowband random excitation increasing a rate of fatigue crack generation in said test structure;

wherein, said test structure mechanical excitation means comprises;

a signal generator, an excitation signal waveform filter and power amplifier connected to said signal generator, an electrodynamic shaker, a test structure receiving fixture to said electrodynamic shaker;

applying said test structure excitation signal to said test structure;

applying said test structure excitation signal to said test structure;

acquire images of a fatigue induced test structure crack using a video system for viewing thermal sensitivity variations of the temperature responsive paint coating and measuring the length of the test structure crack based on acquired images wherein, the intensity variations in said temperature responsive paint coating correspond to variations in local temperature of said test structure; and

wherein, the variations in the local temperature are corresponding to said test structure fatigue crack.

9. The visual structural fatigue crack length measurement method of claim 8 further including the step of applying a stabilizing coat of white spray paint to said test structure prior to said coating step.

10. The visual structural fatigue crack length measurement method of claim 9 wherein said coating step further includes the step of coating said test structure with a probe doped active sol-gel temperature sensitive paint.

11. The visual structural fatigue crack length measurement method of claim 10 wherein said coating step further includes coating said test structure with an active sol-gel temperature sensitive paint containing a luminescent probe therein.

12. The visual structural fatigue crack length measurement method of claim 11 wherein said coating step further includes coating said test structure with a platinum mesotetra (pentafluorophenyl)porphine coating.

13. The visual structural fatigue crack length measurement method of claim 8 wherein said recording step further includes the steps of:

sensing a waveform filtered and amplified output signal from said generating step and;

recording a time history output from said sensing step.

14. The visual structural fatigue crack length measurement method of claim 8 wherein said generating step further includes the steps of:

generating an electrical signal;

filtering and amplifying said electrical signal; and

vibrating a test structure using an electrical signal activating electrodynamic shaker responsive to said filtered and amplified electrical signal.

15. The visual structural fatigue crack length measurement method of claim 8 wherein said recording step further comprises:

measuring test structure motion using test structure mounted first and second accelerometers;

communicating a signal from said test structure mounted accelerometers to a recorder; and

recording an output signal incorporating data from said communicating step.

16. The visual structural fatigue crack length measurement method of claim 8 wherein said video recording step further comprises the steps of:

illuminating the test structure using output energy from a blue light-emitting diode; and

acquiring an image comprising pixels of said illuminated test structure using a CCD camera; and

determining amplitude of pixels obtained in said acquiring step;

analyzing image from said acquiring step by dividing the amplitude of each pixel in an image by an amplitude of each pixel in an initial image acquired before applying said excitation signal to said test structure to determine the test structure intensity change from said vibrating step.