NON-DESTRUCTIVE ULTRASONIC INSPECTION APPARATUS, SYSTEMS, AND METHODS

• US 20160123933A1
• Filed: 10/30/2014
• Published: 05/05/2016
• Est. Priority Date: 10/30/2014
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Fetzer, Barry A., Brown, Christopher R., Bray, Kevin R., Duncan, Michael J., Walton, Steven R.
• Granted Patent: US 9,664,652 B2
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: G01N 2291/106 one or more transducer arrays
• CPC Class Codes: G01N 2291/2694 Wings or other aircraft parts
• CPC Class Codes: G01N 29/225 Supports, positioning or alignment in moving situation
• CPC Class Codes: G01N 29/24 Probes transducers for acoustic waves B06B, G10K; for measuring G01H
• CPC Class Codes: G01N 29/265 by moving the sensor relative to a stationary material
• CPC Class Codes: G01N 29/28 providing acoustic coupling , e.g. water impedance matching G10K11/02

Abstract

As described herein, a system for inspecting a component includes an ultrasonic inspection probe with a component surface interface, and a robotic device with an end effector coupled to the ultrasonic inspection probe. The robotic device is automatably controllable to move the ultrasonic inspection probe across a surface of the component. Additionally, the system includes an angle sensor subsystem coupled between the ultrasonic inspection probe and the end effector. The angle sensor subsystem is configured to operably detect an actual orientation of the end effector relative to a presently inspected portion of the surface of the component. The system includes a controller configured to receive orientation data from the angle sensor subsystem, the orientation data comprising the actual orientation of the end effector, compare the actual orientation to a desired orientation, and control the robotic device to adjust an orientation of the end effector to be in the desired orientation.

Claims

1. A system for inspecting a component, comprising:

an ultrasonic inspection probe comprising a component surface interface;

a robotic device comprising an end effector coupled to the ultrasonic inspection probe, wherein the robotic device is automatably controllable to move the ultrasonic inspection probe across a surface of the component;

an angle sensor subsystem coupled between the ultrasonic inspection probe and the end effector, wherein the angle sensor subsystem is configured to operably detect an actual orientation of the end effector relative to a presently inspected portion of the surface of the component; and

a controller configured to receive orientation data from the angle sensor subsystem based on the actual orientation of the end effector, compare the actual orientation to a desired orientation, and control the robotic device to adjust the actual orientation of the end effector to be in the desired orientation.

2. The system of claim 1, wherein the desired orientation comprises a longitudinal axis of the end effector perpendicular to the presently inspected portion of the surface of the component.

3. The system of claim 1, further comprising an articulation subsystem coupled between the inspection probe and the end effector, the articulation subsystem configured to operably maintain the component surface interface properly engaged with the presently inspected portion of the surface of the component.

4. The system of claim 3, wherein the articulation subsystem comprises a two-axis gimbal structure coupled between the ultrasonic inspection probe and the end effector, wherein the two-axis gimbal structure is configured to passively absorb pitch and roll movement of the ultrasonic inspection probe to maintain the component surface interface substantially parallel to the presently inspected portion of the surface of the component.

5. The system of claim 4, wherein the articulation subsystem further comprises a pneumatic actuator coupled between the two-axis gimbal structure and the end effector, wherein the pneumatic actuator is configured to passively absorb movement of the ultrasonic inspection probe, via the two-axis gimbal structure, along an axis substantially perpendicular to the presently inspected portion of the surface of the component.

6. The system of claim 4, wherein the angle sensor subsystem comprises a plurality of transducers coupled to the two-axis gimbal structure.

7. The system of claim 6, wherein the plurality of transducers comprises a rotary variable differential transformer (RVDT) coupled to each axis of the two-axis gimbal structure.

8. The system of claim 1, wherein the ultrasonic inspection probe comprises:

a housing;

an ultrasonic array coupled to the housing;

a component surface interface of the housing, the component surface interface comprising a liquid couplant port, an engagement lip engageable with a surface of the component, and at least one vacuum port, wherein the engagement lip circumferentially circumscribes the liquid couplant port and the at least one vacuum port circumferentially circumscribes the engagement lip, wherein the at least one vacuum port is fluidly coupleable with a vacuum source;

a liquid couplant chamber disposed between the ultrasonic array and the liquid couplant port of the component surface interface, wherein the liquid couplant chamber is in fluid communication with the liquid couplant port and the liquid couplant chamber is fluidly coupleable with a liquid couplant supply; and

an articulation subsystem coupled to the housing and configured to operably maintain the engagement lip of the component surface interface properly engaged with the presently inspected portion of the surface of the component.

9. An apparatus for inspecting a component, comprising:

a housing;

an ultrasonic array coupled to the housing;

a component surface interface of the housing, the component surface interface comprising a liquid couplant port, an engagement lip engageable with a surface of the component, and at least one vacuum port, wherein the engagement lip circumferentially circumscribes the liquid couplant port and the at least one vacuum port circumferentially circumscribes the engagement lip, wherein the at least one vacuum port is fluidly coupleable with a vacuum source;

a liquid couplant chamber disposed between the ultrasonic array and the liquid couplant port of the component surface interface, wherein the liquid couplant chamber is in fluid communication with the liquid couplant port and the liquid couplant chamber is fluidly coupleable with a liquid couplant supply; and

an articulation subsystem coupled to the housing and configured to operably maintain the component surface interface properly engaged with a presently inspected portion of the surface of the component.

10. The apparatus of claim 9, further comprising a central axis extending from the ultrasonic array and through the liquid couplant chamber and liquid couplant port, wherein the articulation subsystem is configured to operably maintain the central axis substantially perpendicular to the presently inspected portion of the surface of the component.

11. The apparatus of claim 9, wherein the engagement lip of the component surface interface is protruded relative to the at least one vacuum port so as to be positionable closer to the surface of the component relative to the at least one vacuum port.

12. The apparatus of claim 9, wherein the housing is coupled to an end effector of a robotic device, wherein the robotic device is automatably controllable to move the apparatus across the surface of the component.

13. The apparatus of claim 12, wherein the articulation subsystem comprises a two-axis gimbal structure coupled between the housing and the end effector, wherein the two-axis gimbal structure is configured to passively absorb pitch and roll movement of the housing.

14. The apparatus of claim 13, wherein the articulation subsystem further comprises a pneumatic actuator coupled between the two-axis gimbal structure and the end effector, wherein the pneumatic actuator is configured to passively absorb movement of the housing, via the two-axis gimbal structure, along an axis substantially perpendicular to the presently inspected portion of the surface of the component.

15. The apparatus of claim 13, further comprising:

an angle sensor subsystem coupled to the two-axis gimbal structure, wherein the angle sensor subsystem is configured to detect an actual orientation of the end effector relative to the presently inspected portion of the surface of the component; and

a controller configured to receive orientation data from the angle sensor subsystem corresponding to the actual orientation of the end effector, compare the actual orientation to a desired orientation, and control the robotic device to adjust the actual orientation of the end effector to be in the desired orientation.

16. The apparatus of claim 15, wherein the desired orientation comprises a longitudinal axis of the end effector perpendicular to the presently inspected portion of the surface of the component.

17. The apparatus of claim 15, wherein the angle sensor subsystem comprises a plurality of transducers coupled to the two-axis gimbal structure.

18. The apparatus of claim 17, wherein the plurality of transducers comprises a rotary variable differential transformer (RVDT) coupled to each axis of the two-axis gimbal structure.

19. A method for inspecting a component, comprising:

robotically moving an ultrasonic inspection probe across a surface of the component to inspect structural characteristics of the component, wherein moving the ultrasonic inspection probe comprises automatably controlling a robotic device comprising an end effector to which the ultrasonic inspection probe is coupled;

detecting an actual orientation of the end effector relative to a presently inspected portion of the surface of the component, wherein detecting the actual orientation of the end effector comprises receiving orientation data from an angle sensor subsystem that is coupled between the ultrasonic inspection probe and the end effector;

comparing the actual orientation to a desired orientation; and

controlling the robotic device to adjust the actual orientation of the end effector to be in the desired orientation.

20. The method of claim 19, further comprising adjusting the actual orientation of the end effector according to predetermined orientation adjustments at predetermined locations across the surface of the component from a previously performed inspection of the component.