Dual wall turbine blade ultrasonic wall thickness measurement technique

• US 7,272,529 B2
• Filed: 07/08/2005
• Issued: 09/18/2007
• Est. Priority Date: 07/08/2005
• Status: Expired due to Fees

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Singh, Surendra, Hall, James A., Hogan, Robert J.
• Primary Examiner(s): Tsai; Carol S. W.
• Application Number:
  US11/178,020
• Publication Number:
  US 20070118330A1
• Time in Patent Office: 802 Days
• Field of Search: 702/171, 735/88, 736/02, 736/20, 736/24, 736/25, 736/28, 736/41, 600/446, 600/449, 600/450
• US Class Current: 702/171
• CPC Class Codes: F01D 21/003 Arrangements for testing or measuring for measuring vibrations G01H
• CPC Class Codes: G01B 17/02 for measuring thickness

Abstract

A method and apparatus is provided to analyze a dual wall structure having at least one hollow core therein and having the same unknown material sound velocities in walls and in post as well. A transducer is located in at least two different positions with respect to the structure, whereby the transducer propagates an ultrasonic wave toward the dual wall structure. A portion of the ultrasonic wave is reflected back to the transducer. One wave traverses a portion of the dual wall structure that has a core filled with a medium having a known material acoustic property. A second wave traverses a portion of the post that has an unknown material sound velocity. From time of flight measurements of the above mentioned waves, the wall thickness and core shift, if any, can be determined.

Claims

1. A method to determine a dual wall thickness and to detect core dimensions of a workpiece, comprising the steps of:

(a) propagating at least one incident ultrasonic wave from a transducer toward the workpiece either in pulse echo or pitch-catch mode;

(b) receiving a first reflected ultrasonic wave by said transducer, said first reflected ultrasonic wave resulting from said incident ultrasonic wave encountering at least one acoustic interface of the workpiece, said incident ultrasonic wave and said first reflected ultrasonic wave both traversing material having an unknown material sound velocity;

(c) receiving a second reflected ultrasonic wave by said transducer, said second reflected ultrasonic wave resulting from incident ultrasonic wave encountering said at least one acoustic interface of the workpiece, said incident ultrasonic wave and said first reflected ultrasonic wave both traversing material having a known and unknown material sound velocity in core and walls respectively;

(d) determining at least one duration of time from each of said propagating steps to each of said respective receiving steps from said first position and said second position; and

(e) calculating the dual wall thickness and core dimensions of the workpiece, based on the determined durations of time.

2. The method of claim 1, wherein:

said incident ultrasonic waves are propagated at a frequency between about 1 megahertz and about 100 megahertz.

3. The method of claim 1, wherein:

said material having a known material sound velocity fills at least one hollow core or void within the workpiece.

4. The method of claim 1 wherein:

the workpiece is immersed in a liquid or otherwise coupled with a liquid during said steps (a), (b) and (c).

5. The method of claim 1, further comprising:

computer readable media operably connected to at least one of said determining step, or said calculating step.

6. The method of claim 1, wherein:

said calculating step uses the equation V_m,hkl=(X_S/t_S), where V_m,hkl is the velocity of said incident ultrasonic wave in a post, and a thickness of a front wall of the workpiece is determined by X₁=V_m,hkl·

t₁, where X₁ is the thickness of the front wall;

a thickness of a back wall of the workpiece is determined by X₃=V_m,hkl·

t₃, where X₃ is the thickness of the back wall; and

a computer-readable media is operable with said calculating step.

7. The method of claim 1, wherein:

said calculating step uses at least one of the equations;

X_s=V_m,hklt_s=X₁+X₂+X₃ 

 

Equation 1;

X_S=V_m,hklt₁=V₂+t₂+V_m,hklt₃ 

 

Equation 2;

V_m,hklt=X_s/t_s 

 

Equation 3;

X_s=(X_s/t_s)t₁+V₂t₂+(X_s/t_s)t₃ 

 

Equation 3.5

X_s=(V₂t₂t_s)/(t_s−

t₁−

t₃) 

 

Equation 4;

X₂=V₂t₂ 

 

Equation 5a;

X₁=V_m,hklt₁ 

 

Equation 5b;

X₃=V_m,hklt₃ 

 

Equation 5c;

to determine wall thickness or core shift.

8. The method of claim 1, wherein:

said propagating step (a) occurs in at least two different locations in one single pass of the workpiece.

9. The method of claim 1, wherein:

said material having a known material sound velocity fills at least one hollow core or void within the workpiece.

10. The method of claim 1, wherein:

said transducer is a contact transducer that propagates waves in either single delay line pulse echo mode or dual element in pitch-catch.

11. The method of claim 10, wherein:

said transducer is a focused or non-focused transducer.

12. An ultrasonic inspection method for a dual wall structure having solid material and a hollow core, comprising the steps of:

(a) positioning an immersion transducer for wave propagation toward a surface of the dual wall structure, said immersion transducer capable of propagating a pulsed incident longitudinal ultrasonic wave at position A and capable of being repositioned at a position B relative to the workpiece for propagating a pulsed incident longitudinal ultrasonic wave at position B;

(b) propagating said pulsed incident longitudinal ultrasonic wave at position A of said surface, said pulsed incident longitudinal ultrasonic wave at position A directed substantially perpendicular to said surface;

(c) receiving a first reflected ultrasonic wave resulting from said pulsed incident longitudinal ultrasonic wave at position A encountering at least one acoustic interface;

(d) propagating said pulsed incident longitudinal ultrasonic wave at position B toward a second area of said surface, said pulsed incident longitudinal ultrasonic wave at position B directed substantially perpendicular to said area;

(e) receiving a reflected ultrasonic wave resulting from said pulsed incident longitudinal ultrasonic wave at position B encountering said at least one acoustic interface, whereby the position of said transducer at one of said locations enables either of said incident and resulting reflected wave, or said incident at another position and resulting reflected wave to traverse through the solid material of the workpiece, and the position of the transducer at the other said location enables the other of said incident and resulting reflected wave, or said incident and reflected wave to traverse through the hollow core of the workpiece, respectively; and

(f) measuring the time of flight from said propagating step to said receiving step.

13. The method of claim 12, wherein said wave propagation occurring at a frequency between about 10 megahertz to about 100 megahertz.

14. The method of claim 12, further comprising a step of calculating the dual wall thickness or detecting core shift by the equation V_m,hkl=(Xs/t_s), where V_m,hkl is the velocity of said pulsed incident longitudinal ultrasonic wave at position B in a turbine blade post, and a thickness of a front wall of the workpiece is determined by X₁=V_m,hkl·

t₁, where X₁ is the thickness of the front wall and a thickness of a back wall of the workpiece is determined by X₃=V_m,hkl·

t₃, where X₃ is the thickness of the back wall.

15. An ultrasonic testing method to determine characteristics of a dual wall turbine blade having a hollow core and post therein, comprising the steps of:

(a) positioning an immersion transducer at a position A for wave propagation toward an area on a surface of the turbine blade, said immersion transducer capable of propagating an incident pulsed ultrasonic wave and receiving a reflected ultrasonic wave, said immersion transducer capable of being repositioned at a position B for wave propagation and reception;

(b) propagating said incident pulsed ultrasonic wave and receiving said reflected ultrasonic wave while said transducer is at said position A, and while said transducer is at said position B, said position A directs said incident pulsed ultrasonic wave to traverse the hollow core of the dual wall turbine blade, and said position B directs said incident pulsed and reflected ultrasonic waves to traverse the post of the dual wall turbine blade;

(c) measuring a time of flight of said incident pulsed ultrasonic wave and said reflected wave while said immersion transducer is at said position A and said position B, respectively; and

(d) determining the characteristics of the turbine blade from information obtained from said measuring step.

16. The method of claim 15, wherein said determining step includes calculating the dual wall thickness or detecting core shift by the equation V_m,hkl=(X_s/t_s), where V_m,hkl is the velocity of said incident pulsed ultrasonic wave in a turbine blade post, and a thickness of a front wall of the workpiece is determined by X₁=V_m,hkl·

t₁, where X₁ is the thickness of the front wall and a thickness of a back wall of the workpiece is determined by X₃=V_m,hkl·

t₃, where X₃ is the thickness of the back wall; and

presenting the results of said determining step.

17. The method of claim 15, wherein:

said incident pulsed ultrasonic wave is propagated at a frequency between about 1 megahertz and about 100 megahertz.

18. The method of claim 15, wherein:

said incident pulsed ultrasonic wave is propagated at a frequency between about 10 megahertz and about 100 megahertz.

19. The method of claim 15, wherein:

said propagating step lasts for a time needed for data acquisition.

20. The method of claim 15, wherein:

said propagating step takes place at least 2 different locations relative to the turbine blade and in a single path.

21. The method of claim 15 wherein said determining step includes using equations;

X_s=V_m,hklt_s=X₁+X₂+X₃

X_S=V_{m, hkl}t₁+V₂t₂+V_m,hklt₃

V_m,hkl=X_s/t_s

X_s=(X_s/t_s)t₁+V₂t₂+(X_s/t_s)t₃

X_s=(V₂t₂t_s)/(t_s−

t₁−

t₃)

X₂=V₂t₂

X₁=V_m,hklt₁

X₃=V_m,hklt₃

to calculate wall thickness or core shift.

22. The method of claim 15, wherein said determining step includes the use of computer-readable media for determining, storage, writing, reading, or memory.

23. The method of claim 15, wherein said transducer is either a flat transducer, a parallel transducer, an immersion transducer, a cylindrical transducer, a spherical transducer, a focused (Spherical or Cylindrical) and non-focused (Collimated or Parallel), or a contact transducer.