Method for measuring fastener stress utilizing longitudinal and transverse ultrasonic wave time-of-flight

• US 4,602,511 A
• Filed: 06/20/1985
• Issued: 07/29/1986
• Est. Priority Date: 06/20/1985
• Status: Expired due to Term

• Current Assignee: Progress Bank
• Original Assignee: J A Green Company
• Inventors: Holt, Albert C.
• Primary Examiner(s): Kreitman, Stephen A.
• Application Number:
  US06/746,917
• Time in Patent Office: 404 Days
• Field of Search: 73/581, 73/597, 73/629, 73/761
• US Class Current: 73/581
• CPC Class Codes: G01N 29/07 by measuring propagation velocity or propagation time of acoustic waves

Abstract

A method and apparatus for measuring tensile stress in a fastener already in place. This method capitalizes on the discovery that a longitudinal wave will travel roughly twice as fast as a transverse wave and the times-of-flight of the two waves are affected to different degrees by tensile stress. Longitudinal and transverse ultrasonic signals are applied to a first end of the fastener. The longitudinal and transverse signals are detected at this same first end of the fastener after they are reflected off of the second end of the fastener. The time-of-flight for each of the longitudinal and transverse waves is measured. The tensile stress, T, in the fastener is then determined by applying substantially the following equation: ##EQU1## where v₁₀ and v₂₀ =the velocities of the longitudinal and transverse signals, respectively, in a similar fastener not under stress;

k=the length of the unstressed portion of the fastener;

λ and μ=Lame'"'"' constants for the fastener material; and

D₁ and D₂ =material constants for the fastener representing a simplified combination of second and third order elastic material constants.

Claims

1. A method for measuring tensile stress in a fastener under tensile stress comprising:

applying a longitudinal ultrasonic signal to a first end of said fastener;

applying a transverse ultrasonic signal to said first end of said fastener;

detecting said longitudinal and transverse signals at said first end after reflection from a second end of said fastener;

measuring the time-of-flight, t₁, taken by said longitudinal signal to travel from said first end to said second end and back;

measuring the time-of-flight, t₂, for said transverse signal to travel from said first end to said second end and back; and

determining the tensile stress, T, in said fastener substantially according to the equation ##EQU5## (where v₁₀ and v₂₀ =velocities of said longitudinal and transverse signals, respectively, in said fastener without stress, k=unstressed length of said fastener, λ and

μ

=the Lame'"'"' constants for said fastener and D₁ and D₂ represent elastic properties of said fastener).

2. The method of claim 1 wherein said steps of measuring times t₁ and t₂ each comprise the steps of:

determining a frequency f₁ where said detected signal is out of phase with said applied signal by approximately 180°

;

determining a second frequency f₂ of said signal, f₂ being the next adjacent frequency at which said detected signal is out of phase with said applied signal by approximately 180°

; and

determining the time-of-flight from the frequency difference according to the equation t=1/(f₁ -f₂).

3. The method of claim 2 wherein said steps of determining frequencies f₁ and f₂ each comprise the steps of:

adding said applied signal to said detected signal after reflection; and

varying the frequency of said signal until the sum of said applied and detected signals is approximately zero.

4. The method of claim 2 further comprising the step of averaging a plurality of frequency difference determinations.

5. The method of claim 1 wherein said signals are sinusoidal with a frequency of 5-10 mHz and further comprising the step of gating said signals to produce pulses of 1 to 5 microseconds duration.

6. The method of claim 5 further comprising the steps of:

generating said sinusoidal signals; and

amplifying said sinusoidal signals.

7. The method of claim 6 further comprising the step of compensating for the difference in paths travelled by said applied and said detected signals outside said fastener.

8. The method of claim 1 further comprising the step of conditioning said first end of said fastener to give a flat surface for applying and detecting said signals.

9. The method of claim 1 further comprising the step of focusing said signals so that they are reflected from a center portion of said second end of said fastener.

10. The method of claim 1 wherein said longitudinal and transverse signals are simultaneously applied to said first end of said fastener.

11. A method for measuring tensile stress in a fastener comprising:

simultaneously applying a pulse of a longitudinal ultrasonic sinusoidal signal and a transverse ultrasonic sinusoidal signal to said first end of said fastener;

detecting said longitudinal and transverse signals at said first end after reflection from a second end of said fastener;

adding said applied signal to said detected signal for each of said longitudinal and transverse signals to produce a summed signal;

varying the frequency of said sine wave signal for each of said longitudinal and transverse signals to a frequency f(1), where said longitudinal summed signal is approximately zero, and a frequency of f(t), where said transverse signal is approximately zero;

varying said frequency to next adjacent frequencies f(1)₂ and f(t)₂ where said longitudinal and transverse summed signals, respectively, are approximately zero;

determining the times-of-flight, t₁ and t₂, for said longitudinal and transverse signals, respectively, to travel the length of said fastener and back from the frequency difference according to the equation t=1/(f₁ -f₂);

determining the tensile stress in said fastener substantially according to the equation ##EQU6## (where v₁₀ and v₂₀ =velocities of said longitudinal and transverse signals, respectively, in said fastener without stress, k=unstressed length of said fastener, λ and

μ

=the Lame'"'"' constants for said fastener and D₁ and D₂ represent elastic properties of said fastener).

12. The method of claim 11 further comprising the step of averaging a plurality of frequency difference determinations.

13. The method of claim 11 wherein said signals are sinusoidal with a frequency of 5-10 mHz and further comprising the step of gating said signals to produce pulses of 1 to 5 microseconds duration.

14. The method of claim 11 further comprising the steps of:

generating said sinusoidal signals; and

amplifying said sinusoidal signals.

15. The method of claim 11 further comprising the step of compensating for the difference in paths travelled by said applied and said detected signals outside said fastener.

16. The method of claim 11 further comprising the step of conditioning said first end of said fastener to give a flat surface for applying and detecting said signals.

17. The method of claim 11 further comprising the step of focusing said signals so that they are reflected from a center portion of said second end of said fastener.

18. A method for measuring tensile stress in a fastener comprising:

applying a longitudinal ultrasonic signal to a first end of said fastener;

applying a transverse ultrasonic signal to said first end of said fastener;

detecting said longitudinal and transverse signals at said first end after reflection from a second end of said fastener;

measuring the time, t₁, taken by said longitudinal signal to travel from said first end to said second end and back;

measuring the time, t₂, for said transverse signal to travel from said first end to said second end and back;

measuring the length, k, of the unstressed portion of the fastener;

determining the velocities, v₁₀ and v₂₀, of said longitudinal and transverse signals, respectively, in a similar fastener not under stress;

determining the material constants, D₁ and D₂, for said similar fastener under a known tensile stress T from the equations ##EQU7## (wherein a₀ equals the unstressed length of a portion of said similar fastener to be put under stress, E equals Young'"'"'s Modulus, λ and

μ

are the Lame'"'"' constants for the fastener); and

determining the tensile stress, T, from the equation ##EQU8##

19. An apparatus for measuring tensile stress in a fastener comprising:

means for applying a longitudinal ultrasonic signal to a first end of said fastener;

means for applying a transverse ultrasonic signal to said first end of said fastener;

means for detecting said longitudinal and transverse signals at said first end after reflection from a second end of said fastener;

means for measuring the time-of-flight, t₁, taken by said longitudinal signal to travel from said first end to said second end and back;

means for measuring the time-of-flight, t₂, for said transverse signal to travel from said first end to said second end and back; and

means for determining the tensile stress, T, in said fastener substantially according to the equation ##EQU9## (where v₁₀ and v₂₀ equal velocities of said longitudinal and transverse signals, respectively, in said fastener without stress, k equals the unstressed length of said fastener, λ and

μ

are the Lame'"'"' constants for said fastener and D₁ and D₂ represent elastic properties of said fastener).

20. The apparatus of claim 19 wherein said means for measuring times t₁ and t₂ each comprise:

means for determining a frequency f₁ where said detected signal is out of phase with said applied signal by approximately 180°

;

means for determining a second frequency f₂ of said signal, f₂ being the next adjacent frequency at which said detected signal is out of phase with said applied signal by approximately 180°

; and

means for determining the time-of-flight from the frequency difference according to the equation t=1/(f₁ -f₂).

21. The apparatus of claim 20 wherein said means for determining frequencies f₁ and f₂ each comprise:

means for adding said applied signal to said detected signal after reflection; and

means for varying the frequency of said signal until the sum of said applied and detected signals is approximately zero.

22. The apparatus of claim 20 further comprising means for averaging a plurality of frequency difference determinations.

23. The apparatus of claim 19 wherein said signals are sinusoidal with a frequency of 5-10 mHz and further comprising means for gating said signals to produce pulses of 1 to 5 microseconds duration.

24. The apparatus of claim 23 further comprising:

means for generating said sinusoidal signals; and

means for amplifying said sinusoidal signals.

25. The apparatus of claim 24 further comprising means for compensating for the difference in paths travelled by said applied and said detected signals outside said fastener.

26. The apparatus of claim 19 further comprising means for conditioning said first end of said fastener to give a flat surface for applying and detecting said signals.

27. The apparatus of claim 19 further comprising means for focusing said signals so that they are reflected from a center portion of said second end of said fastener.

28. The apparatus of claim 19 further comprising means for applying said longitudinal and transverse signals to said first end of said fastener.