IP Library Granted Patent US 9,804,129
Granted Patent B2
US 9,804,129 · App. 14/529,072 · Granted Oct 31, 2017

Apparatus for inspecting a tube

Inventors: Barry A. Fetzer (Renton, WA); Navpreet S. Grewal (Redmond, WA); Peter Kuk-kyung Hwang (Kent, WA); William R. Schell (Edgewood, WA); Kate Brown Boudreau (Seattle, WA)
Assignee: The Boeing Company
G01N29/043G01N29/225G01N2291/023G01N2291/044G01N2291/106G01N2291/2636
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 9,804,129
App. No.
14/529,072
Granted
Oct 31, 2017
Kind
B2
Abstract

An apparatus for inspecting a tubular workpiece may include a probe assembly and a rotation mechanism. The probe assembly may include a transducer array positionable adjacent to an inner surface of the tubular workpiece. The probe assembly may generate transmitted sound waves and may receive reflected sound waves. The rotation mechanism may rotate the probe assembly relative to the tubular workpiece in a manner such that the transducer array passes over the inner surface in a circumferential direction during transmission of the transmitted sound waves.

Claims (53)

1. An apparatus for inspecting the integrity of a swage joint of a tubular workpiece, comprising:

a probe assembly having a transducer array positionable adjacent to an inner surface of a tubular workpiece having a tube end, the transducer array being configured to generate transmitted sound waves toward the inner surface and receive reflected sound waves;

a rotation mechanism configured to rotate the probe assembly about a rotational axis relative to the tubular workpiece in a manner such that the transducer array passes over the inner surface in a circumferential direction during transmission of the transmitted sound waves; and

the probe assembly configured to measure, during rotation of the probe assembly and transmission of the sound waves, a change in diameter of the inner surface of the tube end along an axial direction to verify the integrity of the swage joint.

2. The apparatus of claim 1 wherein:

the transducer array is configured to generate the transmitted sound waves at a frequency of at least approximately 10 MHz.

3. The apparatus of claim 1 wherein:

the probe assembly is configured to substantially continuously generate the transmitted sound waves and received the reflected sound waves during rotation of the probe assembly relative to the tubular workpiece.

4. The apparatus of claim 1 further comprising:

a display device coupled to the probe assembly;

the probe assembly being configured to generate electrical signals representative of the reflected sound waves; and

the display device being configured to receive the electrical signals and generate a graphical image representative of the inner surface during rotation of the probe assembly relative to the tubular workpiece.

5. The apparatus of claim 1 wherein:

the probe assembly is configured such that the transducer array is maintained at a substantially constant distance from the inner surface during rotation of the probe assembly relative to the tubular workpiece.

6. The apparatus of claim 1 wherein:

the probe assembly being configured such that a location thereof is radially adjustable relative to the rotational axis.

7. The apparatus of claim 1 wherein:

the transducer array includes a plurality of transducer elements arranged as a linear array; and

the linear array has an array longitudinal axis being maintained in generally parallel relation to the rotational axis during rotation of the probe assembly relative to the tubular workpiece.

8. The apparatus of claim 7 wherein:

the tube end has a fitting joined to the tube end at a joint section of the swage joint at the tube end; and

the linear array having an axial length such that the transducer elements are spaced pass over the joint section and at least a portion of a non-joint section of the tube end.

9. The apparatus of claim 1 further comprising:

a clamping mechanism configured to clamp the tubular workpiece in a fixed position such that a tube end of the tubular workpiece is maintained in substantially centered relation to the rotational axis of the rotation mechanism during rotation of the probe assembly relative to the tubular workpiece.

10. The apparatus of claim 1 further comprising:

a container configured to contain a liquid and being sized and configured to immerse the probe assembly a tube end of the tubular workpiece in the liquid during rotation of the probe assembly relative to the tubular workpiece.

11. An apparatus for inspecting the integrity of a swage joint of a tubular workpiece, comprising:

a probe assembly having a transducer array positionable adjacent to an inner surface of a tube end of a tubular workpiece having a tube end, the transducer array being configured to generate transmitted sound waves toward the inner surface and receive reflected sound waves; and

a rotation mechanism configured to rotate the probe assembly about a rotational axis relative to the tubular workpiece in a manner such that the transducer array passes over the inner surface in a circumferential direction during transmission of the transmitted sound waves;

a container configured to contain a liquid and being sized and configured to immerse the probe assembly and the tube end in the liquid during rotation of the probe assembly relative to the tubular workpiece; and

the probe assembly configured to measure, during rotation of the probe assembly and transmission of the sound waves, a change in diameter of the inner surface of the tube end along an axial direction to verify the integrity of the swage joint.

12. The apparatus of claim 11 wherein:

the transducer array is configured to generate the transmitted sound waves at a frequency of at least approximately 10 MHz.

13. The apparatus of claim 11 wherein:

the probe assembly is configured to substantially continuously generate the transmitted sound waves and received the reflected sound waves during rotation of the probe assembly relative to the tubular workpiece.

14. The apparatus of claim 11 further comprising:

a display device coupled to the probe assembly;

the probe assembly being configured to generate electrical signals representative of the reflected sound waves; and

the display device being configured to receive the electrical signals and generate a graphical image representative of the inner surface during rotation of the probe assembly relative to the tubular workpiece.

15. The apparatus of claim 11 wherein:

the probe assembly is configured such that the transducer array is maintained at a substantially constant distance from the inner surface during rotation of the probe assembly relative to the tubular workpiece.

16. The apparatus of claim 11 wherein:

the probe assembly being configured such that a location thereof is radially adjustable relative to the rotational axis.

17. The apparatus of claim 11 wherein:

the transducer array includes a plurality of transducer elements arranged as a linear array; and

the linear array has an array longitudinal axis being maintained in generally parallel relation to the rotational axis during rotation of the probe assembly relative to the tubular workpiece.

18. The apparatus of claim 17 wherein:

the tube end has a fitting joined to the tube end at a joint section of the swage joint at the tube end; and

the linear array having an axial length such that the transducer elements are spaced pass over the joint section and at least a portion of a non-joint section of the tube end.

19. The apparatus of claim 11 further comprising:

a clamping mechanism configured to clamp the tubular workpiece in a fixed position such that a tube end of the tubular workpiece is maintained in substantially centered relation to the rotational axis of the rotation mechanism during rotation of the probe assembly relative to the tubular workpiece.

20. The apparatus of claim 19 wherein:

the clamping mechanism includes an opposing pair of jaws laterally movable in opposing directions and configured to clamp the tubular workpiece such that a workpiece longitudinal axis is approximately coincident with the rotational axis of the rotation mechanism.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 30, 2014
From: FETZER, BARRY A.; GREWAL, NAVPREET S.; HWANG, PETER KUK-KYUNG; SCHELL, WILLIAM R.; BOUDREAU, KATE BROWN
To: THE BOEING COMPANY
Reel/Frame 034076/0231 →
Continuity (2)
Division 13482409 · May 29, 2012
Related Publication 20150053014A1 · Feb 26, 2015