Rotating array probe system for non-destructive testing

• US 8,798,940 B2
• Filed: 04/11/2011
• Issued: 08/05/2014
• Est. Priority Date: 04/16/2010
• Status: Active Grant

• Current Assignee: Evident Scientific Incorporated (Evident Corporation)
• Original Assignee: Olympus Ndt Incorporated (Olympus Corporation)
• Inventors: Drummy, Michael, Imbert, Christophe
• Primary Examiner(s): Breene, John
• Assistant Examiner(s): RIVERA VARGAS, MANUEL A
• Application Number:
  US13/083,648
• Publication Number:
  US 20110257903A1
• Time in Patent Office: 1,212 Days
• Field of Search: 702/35, 702/39
• US Class Current: 702/35
• CPC Class Codes: G01M 13/045 Acoustic or vibration analysis
• CPC Class Codes: G01N 2291/2623 Rails; Railroads
• CPC Class Codes: G01N 2291/2634 cylindrical from outside
• CPC Class Codes: G01N 29/225 Supports, positioning or alignment in moving situation
• CPC Class Codes: G01N 29/262 by electronic orientation or focusing, e.g. with phased arrays phased arrays per se G10K11/34
• CPC Class Codes: G01N 29/275 by moving both the sensor and the material

Abstract

A device is disclosed for performing non-destructive inspection and testing (NDT/NDI) of an elongated test object, wherein the inspection system includes: a test object conveyor for conveying the test object along a longitudinal conveyance path; a probe assembly including phased-array probes, the probe assembly being configured to induce signals in the test object and sense echoes reflected from the test object; a probe assembly conveyor configured to movably support the probe assembly, to move the probe assembly on a circumferential path about the test object; and a control system coupled to the test object conveyor and to the probe assembly conveyor and configured to allow data acquisition by and from the phased-array probes while, simultaneously, the test object moves along the longitudinal path and the phased-array probes move on the circumferential path. The test system may include phased-array probes of different types to optimize detecting faults or cracks in the test object which extend in different directions.

Claims

1. An inspection system for performing non-destructive testing of test object, the inspection system comprising:

a test object conveyor for conveying the test object along a longitudinal conveyance path;

at least one probe assembly further including at least one phased-array probe, the phased-array probe being configured to send ultrasonic beams to the test object and to sense echo signals induced in the test object and convert the echoes to electronic response data and a probe assembly conveyor configured to movably support the probe assembly, to move the probe assembly on a circumferential path about the test object;

at least one data acquisition unit disposed on the probe assembly conveyor which acquires the response data from the phased-array probe, provides phased array firing command to the phased-array probe in order to apply desired focus angles for the ultrasonic beams for the testing and perform a first part of data processing including producing real-time A-scan data;

a control and data processing system coupled to the test object conveyor and to the probe assembly conveyor and the data acquisition unit, the processing system configured to send command to the data acquisition unit, receive and provide a second part of data processing received from the data acquisition unit while, simultaneously while the test object moves along the longitudinal path and the phased-array probes move on the circumferential path.

2. The inspection system of claim 1, wherein the probe assembly comprises at least two phased-array probes, which are longitudinally juxtaposed to one another on said probe assembly conveyor.

3. The inspection system of claim 2, including a couplant irrigation source for coupling couplant fluid from a first to a second bearing structure, and including couplant fluid dispersants located adjacent the at least two phased-array probes.

4. The inspection system of claim 3, wherein the couplant dispersants are configured to generate a substantial laminar flow of couplant between an outer surface of a water wedge coupled to the phased-array probes and an opposing surface of the test object.

5. The inspection system of claim 2, including a pressurized gas source for coupling a pressurized gas from a first to a second bearing structure, and including pressurized gas dispersants located adjacent to the at least two phased-array probes.

6. The inspection system of claim 5, wherein the probe assembly conveyor is configured to rotate the probe assembly around the longitudinal path at a substantially constant rotational speed.

7. The inspection system of claim 2, including a pressurized gas source, and including pressurized gas dispersants located adjacent to the at least two phased-array probes.

8. The inspection system of claim 1, including at least one circumferential position sensor acquiring data regarding circumferential position of the phased-array probe, and at least one longitudinal position sensor acquiring data regarding the test object'"'"'s longitudinal position.

9. The inspection system of claim 8, wherein the first part of the data processing is produced by the data acquisition unit as real-time A-scan data based on the sensed signals by the phased-array probe, the data regarding the longitudinal position and the data regarding the circumferential position.

10. The inspection system of claim 9, including at least one predetermined gate or threshold for determining when sensed signals indicate a flaw in the A-scan data.

11. The inspection system of claim 10, including a warning and marking mechanism providing the longitudinal and circumferential positions of the flaw that is detected.

12. The inspection system of claim 1, referring to FIG. 8a, wherein,

the test object conveyor is effective to convey the test object over axial distances including the axial distance Δ

l during the time of Δ

t, the probe assembly conveyor and the phased-array probe are operated according to following Eq. 1

Vpipe≦

m·

Lprobe/T=m·

Lprobe·

(rpm)/60 (m/s) 

 

Eq. 1

and wherein,

a) L_probe is defined as a probe aperture span which is the distance between a given element position in a first aperture and a respective element position in a last aperture;

b) Δ

t is defined as a scan cycle time, which begins at the start of a pulse-receive cycle of the phased-array probe for the first aperture and ends at the completion of a pulse-receive cycle for the last aperture =;

c) V_pipe is a constant, and is the speed that test object is fed;

d) Δ

l is an axial distance that the pipe travels during Δ

t;

e) rpm is the rotating speed of the rotating probe assembly conveyor;

f) T is the time it takes for the phased-array probe to rotate 360 degrees around test object, which is rpm<sup>−

1</sup>;

g) V_aperture is a constant and is the speed of the phased-array probe head of each aperture scan cycle;

h) V_rotate is an angular speed of the rotating probe assembly conveyor;

i) n is the number of apertures of each PA probe;

j) m is the total number of probes disposed on the probe assembly conveyor; and

k) Δ

y is a unit circumferential scan resolution.

13. The inspection system of claim 12, wherein Δ

y is determined by Eq. 2;

Δ

y=Vaperture·

Δ

t/n=2π

R·

rpm·

Δ

t/n 

 

Eq. 2

wherein R is the radius of the test object.

14. The inspection system of claim 1, wherein the probe assembly comprises at least two phased-array probes of a first type, which are circumferentially juxtaposed to one another on said probe assembly conveyor and are configured to optimize sensing of structural cracks or faults of the test object generally extending in the longitudinal path.

15. The inspection system of claim 1, wherein the probe assembly comprises at least two phased-array probes of a second type, which are circumferentially juxtaposed to one another on said probe assembly conveyor and are configured to optimize sensing of cracks or faults generally extending at a substantial angle to the longitudinal path.

16. The inspection system of claim 1, wherein the probe assembly comprises:

at least two phased-array probes of a first type, and at least two phased-array probes of a second type.

17. The inspection system of claim 1, wherein the test object conveyor is configured and controlled to carry the test object at a known speed along said longitudinal conveyance path throughout substantially the entirety of the longitudinal path.

18. The inspection system of claim 1, including a wireless system for wirelessly communicating data signals from the probe assembly to a processing computer.

19. The inspection system of claim 1, wherein the at least one phased array probe senses the longitudinal position of the test object.

20. The inspection system of claim 1, wherein the probe assembly conveyor is constructed and configured to enable rotational movement of the phased-array probes over an angular range substantially including 0°

to 360°

about the longitudinal path.

21. The inspection system of claim 1, wherein the assembly probe conveyor includes a position adjuster which is configured to control a spacing provided between the phased-array probes and the test object.

22. The inspection system of claim 1, including a mechanism for rotating the test object and for adjusting a center of mass thereof.

23. The inspection system of claim 1, wherein the probe assembly conveyor is effective to move the probe assembly at the same axial speed as the test object for testing an initial test object section.

24. The inspection system of claim 1, wherein the control system includes a computer program which is configured to store maximum linear and rotational speed values for the test object and for the phased-array probes.

25. The inspection system of claim 1, wherein the phased-array probes comprise acoustical transducers.

26. The inspection system of claim 1, wherein the phased-array probes comprise elements that are configured to induce and sense Eddy Currents in the test object.

27. The inspection system of claim 1, including an electrical generator mounted to the probe assembly conveyor and configured to generate electrical power for the probe assembly.

28. The inspection system of claim 1, including a stationary couplant irrigation assembly which sprays couplant to each of the at least one of the probe in such a way that the couplant forms a laminate layer between the surface of the test object and a test surface of the probe facing the surface of the test object.

29. An inspection system for performing non-destructive testing of test object, the inspection system comprising:

a test object conveyor for conveying the test object along a longitudinal conveyance path;

at least one probe assembly further including at least one phased-array probe, the phased-array probe being configured to send ultrasonic beams to the test object and to sense echo signals induced in the test object and convert the echoes to electronic response data and a probe assembly conveyor configured to movably support the probe assembly, to move the probe assembly on a circumferential path about the test object;

at least one data acquisition unit disposed on the probe assembly conveyor which acquires the response data from the phased-array probe, provides phased array firing commands to the phased-array probe in order to apply desired focus angles for the ultrasonic beams for the testing and perform a first part of data processing including producing real-time A-scan data;

a control and data processing system coupled to the test object conveyor and to the probe assembly conveyor configured to allow data acquisition by and from the phased-array probes while, simultaneously, the test object moves along the longitudinal path and the phased-array probes move on the circumferential path, wherein the probe assembly conveyor includes a first stationary bearing structure which rotatably supports a second rotatable bearing structure, the second bearing structure being configured to support the probe assembly.

30. The inspection system of claim 29, including an electrical coupling structure for coupling electric power and signals between the first bearing structure and the second bearing structure.

31. The inspection system of claim 30, wherein the electrical coupling structure comprises a slip ring cavity.