Automated inspection for internal corrosion

Patent metadata

Field	Value
Publication number	US-11668773-B2
Application number	US-202016948029-A
Country	US
Kind code	B2
Filing date	Aug 27, 2020
Priority date	Mar 22, 2019
Publication date	Jun 6, 2023
Grant date	Jun 6, 2023

Abstract

A system for magnetically inspecting a metallic component uses a manipulator configured to manipulate a relative position between a part fixture that holds the metallic component and a probe fixture that holds a magnetic probe, thereby causing the probe tip to trace an inspection route along the surface of the metallic component so that the probe tip contacts the metallic component such that an angular difference between the probe axis and a vector normal to the surface is less than a predetermined angle delta. The magnetic probe has a probe tip that measures magnetic permeability of the metallic component along the inspection route, which the controller receives. A method of performing the magnetic inspection is also disclosed.

First claim

The invention claimed is:

1. A system for magnetically inspecting a metallic component having a surface, the system comprising:
a holder configured to hold the metallic component
a probe fixture configured to hold a magnetic probe having a probe tip aligned with a probe axis, the magnetic probe configured to measure a magnetic permeability of the metallic component;
a manipulator configured to manipulate a relative position between the holder and the probe fixture; and
a controller configured to:
control the manipulator to trace an inspection route upon the surface of the metallic component along which the probe tip contacts the metallic component such that an angular difference between the probe axis and a surface tangent plane of the metallic component is 90±10 degrees;
receive the magnetic permeability of the metallic component measured by the magnetic probe along the inspection route;
determine a magnetic anomaly map based on the magnetic permeability of the metallic component;
determine a first corrosion element thickness based on the magnetic anomaly map;
determine a first remaining non-corrosion wall thickness based on a calculation using the first corrosion element thickness and a three-dimensional model of the metallic component; and
transmit the first remaining non-corrosion wall thickness to an operator via an input output interface.

2. The system of claim 1 , wherein the controller is further configured to calculate, based on a three-dimensional model of the metallic component, the inspection route.

3. The system of claim 1 , wherein the controller is further configured to generate, based on the magnetic permeability measured along the inspection route, a magnetic anomaly map and/or a corrosion map of the magnetic component.

4. The system of claim 1 , wherein:
tracing the inspection route defines a linear speed; and
the linear speed is within a target speed tolerance of a target speed.

5. The system of claim 4 , wherein the target speed ranges from 0.2-10 inches/second (0.5-25 cm/sec).

6. The system of claim 5 , wherein the target speed tolerance is +5% of the target speed.

7. The system of claim 1 , further comprising a mechanical biasing component, wherein:
the probe tip contacting the metallic component defines a contact force; and
the mechanical biasing component is configured to maintain the contact force within a contact force tolerance of a target contact force.

8. The system of claim 7 , wherein the mechanical biasing component comprises a mechanically compressible component.

9. The system of claim 1 , further comprising a force transducer, wherein:
the probe tip contacting the metallic component defines a contact force; and
the force transducer is configured to produce a contact force signal that is indicative of the contact force.

10. The system of claim 9 , wherein the controller is further configured to cause the manipulator to maintain the contact force within a contact force tolerance of a target contact force.

11. The system of claim 10 wherein: the target contact force ranges from 0-1 pounds force (lbf) (0-4.4 Nt).

12. The system of claim 11 , wherein the contact force tolerance is ±20% of the target contact force.

13. The system of claim 1 , wherein:
the manipulator is manipulatable with three, four, five, or six axes of movement; and
the manipulator comprises an actuator configured to manipulate the holder.

14. The system of claim 13 , further comprising a holder extension configured to separate the metallic component from the actuator by at least a critical separation distance.

15. The system of claim 14 , wherein:
the holder extension comprises a nonmetallic material defining a length; and
the length is at least 4 inches (10 cm).

16. The system of claim 1 , wherein the magnetic probe is stationary.

17. The system of claim 1 , wherein the metallic component is a blade of a gas turbine engine.

18. A method of inspecting a metallic component having a surface the method comprising:
holding, by a holder, the metallic component;
holding, by a probe fixture, a magnetic probe having a probe tip aligned with a probe axis, the magnetic probe being configured to measure a magnetic permeability of the metallic component;
calculating, by a controller, an inspection route over at least a portion of the surface based at least in part on a three-dimensional model of the metallic component;
manipulating, by a manipulator controlled by the controller, a relative position between the holder and the probe fixture so as to cause the probe tip to trace the inspection route upon the surface of the metallic component along which the probe tip contacts the metallic component such that an angular difference between the probe axis and a surface tangent plane of the metallic component is 90±10 degrees;
receiving, by the controller, the magnetic permeability of the metallic component measured by the magnetic probe along the inspection route;
determining, by the controller, a magnetic anomaly map based on the magnetic permeability of the metallic component;
determining, by the controller, a corrosion map based on the magnetic anomaly map;
determining, by the controller, a material remaining map based on a comparison of the corrosion map and a three-dimensional model of the metallic component; and
transmitting, by an input/output interface, the material remaining map to an operator via an input output interface.

19. A system for magnetically inspecting a metallic component having a surface, the system comprising:
a holder configured to hold the metallic component
a probe fixture configured to hold a magnetic probe having a probe tip aligned with a probe axis, the magnetic probe configured to measure a magnetic permeability of the metallic component;
a manipulator configured to manipulate a relative position between the holder and the probe fixture; and
a controller configured to:
control the manipulator to trace an inspection route upon the surface of the metallic component along which the probe tip contacts the metallic component such that an angular difference between the probe axis and a surface tangent plane of the metallic component is 90±10 degrees;
receive the magnetic permeability of the metallic component measured by the magnetic probe along the inspection route;
determine a magnetic anomaly map based on the magnetic permeability of the metallic component;
determine a corrosion map based on the magnetic anomaly map;
determine a material remaining map based on a comparison of the corrosion map and a three-dimensional model of the metallic component; and
transmit the material remaining map to an operator via an input output interface.

Assignees

• Raytheon Tech Corp

Inventors

• Debiccari Andrew
• Ouyang Zhong

Classifications

• G01M15/14

  Testing gas-turbine engines or jet-propulsion engines · CPC title

• G01R33/1223 Primary

  Measuring permeability, i.e. permeameters (G01R33/14 takes precedence) · CPC title

• G01N27/83

  by investigating stray magnetic fields · CPC title

• G01N27/87

  using probes · CPC title