Part evaluation system/method using both resonance and surface vibration data

• US 10,067,094 B2
• Filed: 05/02/2016
• Issued: 09/04/2018
• Est. Priority Date: 06/20/2011
• Status: Active Grant

• Current Assignee: Vibrant Corproation
• Original Assignee: Vibrant Corproation
• Inventors: Hunter, Lemna J., Jauriqui, Leanne, Weaver, Greg
• Primary Examiner(s): Shah, Manish S
• Assistant Examiner(s): Miller, Rose M
• Application Number:
  US15/144,665
• Publication Number:
  US 20170089867A1
• Time in Patent Office: 855 Days
• Field of Search: 73579, 73602, 73643
• CPC Class Codes: G01H 13/00 Measuring resonant frequency
• CPC Class Codes: G01H 7/00 Measuring reverberation time ; room acoustic measurements
• CPC Class Codes: G01H 9/002 for representing acoustic field distribution sonar systems for imaging G01S7/56, G01S15/89; acoustic holography G03H3/00
• CPC Class Codes: G01H 9/008 by using ultrasonic waves measuring position using ultrasonic waves G01S15/02
• CPC Class Codes: G01N 2291/014 Resonance or resonant frequency
• CPC Class Codes: G01N 2291/017 Doppler techniques
• CPC Class Codes: G01N 2291/103 one emitter, two or more receivers
• CPC Class Codes: G01N 29/12 by measuring frequency or resonance of acoustic waves measuring frequency or resonant frequency of mechanical vibrations or acoustic waves in general G01H1/06, G01H3/04, G01H13/00; acoustic resonators G10K11/04; vibration or shock testing of structures G01M7/00
• CPC Class Codes: G01N 29/223 Supports, positioning or alignment in fixed situation mounting transducers per se G10K11/004
• CPC Class Codes: G01N 29/2418 using optoacoustic interaction with the material, e.g. laser radiation, photoacoustics photoacoustic cells G01N21/1702; measuring characteristics of vibrations by using radiation-sensitive means G01H9/00; acousto-optical conversion techniques for short-range imaging G01S15/8965; sound-producing devices using laser bundle G10K15/046
• CPC Class Codes: G01N 29/44 Processing the detected response signal , e.g. electronic circuits specially adapted therefor digital signal processing per se G06F17/00
• CPC Class Codes: G01N 29/4436 with a reference signal amplitude comparison G01N29/48

Abstract

A part (120) may be subjected to both a resonance inspection and a surface vibration inspection. Various protocols (230; 240; 250; 280; 260) are disclosed as to how the results of one or more of these inspections may be used to evaluate the part (120).

Claims

1. A method of evaluating a part, wherein a resonance inspection comprises exciting a part-under-test at a plurality of input frequencies and obtaining a frequency response of said part-under-test at each of said plurality of input frequencies, wherein a surface vibration inspection comprises vibrating said part-under-test and assessing surface vibrations of said part-under test, and wherein said method comprises the steps of:

conducting a first inspection of a first part-under-test, wherein said first inspection comprises performing said resonance inspection on said first part-under-test;

conducting a second inspection of said first part-under-test, wherein said second inspection comprises performing said surface vibration inspection on said first part-under-test, wherein said second inspection comprises identifying at least one mode shape in surface inspection results from said second inspection for use in relation to said first inspection by associating a frequency with said at least one mode shape, and wherein said first inspection comprises utilizing said frequency associated with said at least one mode shape; and

evaluating said first part-under-test based upon each of said first and second inspections including using said surface inspection results from said second inspection to associate at least one resonance frequency peak in resonance inspection results from said first inspection with said at least one mode shape to at least identify a vibrational mode of said at least one resonance frequency peak in said resonance inspection results from said first inspection to compare said at least one resonance frequency peak to a resonance standard associated with said vibrational mode.

2. The method of claim 1, wherein said resonance inspection comprises obtaining said frequency response of said first part-under-test using laser vibrometry.

3. The method of claim 1, wherein said surface vibration inspection is selected from the group consisting of holographic interferometry, laser vibrometry, laser Doppler velocimetry, scanning laser vibrometry, and 2-d and 3-d scanning laser vibrometry.

4. The method of claim 1, wherein said evaluating step comprises determining if said first part-under-test is equivalent to a control group.

5. The method of claim 1, further comprising the step of:

disposing said first part-under-test in a fixture, wherein each of said first and second inspections are completed with said first part-under-test remaining in said fixture.

6. The method of claim 1, wherein said evaluating step comprises using said resonance inspection results from said first inspection to assess an anomaly in said surface inspection results from said second inspection.

7. The method of claim 1, wherein said evaluating step comprises using said surface inspection results from said second inspection to assess an anomaly in said resonance inspection results from said first inspection.

8. The method of claim 1, wherein said second inspection comprises identifying a plurality of mode shapes in said surface inspection results from said second inspection, and where said evaluating step comprises using said surface inspection results from said second inspection to associate each of a plurality of resonance frequency peaks in said resonance inspection results with a different vibrational mode.

9. The method of claim 8, wherein each said vibrational mode is selected from the group consisting of any one of multiple orders of each of a bending mode, a torsional mode, longitudinal modes, coupling modes, flexural modes, and axial modes.

10. The method of claim 8, wherein said evaluating comprises comparing said plurality of resonance frequency peaks in said resonance inspection results to a corresponding resonance standard associated with a respective corresponding one of said different vibrational modes.

11. The method of claim 1, wherein said resonance standard is stored on a computer-readable storage medium, wherein said evaluating step comprises using at least one processor, and wherein said resonance standard is based upon spectra from conducting a separate said resonance inspection on each of a plurality of parts.

12. The method of claim 11, wherein said resonance standard is further based upon conducting a separate said surface vibration inspection on each of said plurality of parts, and correlating results from said surface vibration inspection with results from said resonance inspection for each of said plurality of parts.

13. The method of claim 12, wherein said resonance standard is for a new production part.

14. The method of claim 12, wherein said resonance standard defines a normal aging of said first part-under-test.

15. The method of claim 12, wherein said resonance standard comprises a plurality of subgroups, wherein said method further comprises defining said subgroups using results from said surface vibration analysis on each of said plurality of parts and from said resonance inspection for each of said plurality of parts.

16. The method of claim 11, wherein said resonance standard is further based upon conducting a separate thermal surface analysis on each of said plurality of parts during said resonance inspection of said plurality of parts, and correlating results from said thermal surface analysis with results from said resonance inspection for each of said plurality of parts.

17. The method of claim 1, wherein said resonance standard is generated by mathematical modeling.

18. The method of claim 17, wherein said resonance standard comprises expected resonance inspection results derived via the mathematical modeling.

19. The method of claim 18, wherein said expected resonance inspection results are associated with said vibrational mode and said at least one resonance frequency peak is compared to said expected resonance inspection results.

20. The method of claim 17, wherein said resonance standard is for a new production part.

21. The method of claim 17, wherein said resonance standard defines a normal aging of said first part-under-test.

22. The method of claim 17, wherein said mathematical modeling associates a plurality of vibrational modes with corresponding frequencies in said resonance inspection.