Method of inspecting a surface of a component using a probe

Patent metadata

Field	Value
Publication number	US-11650129-B2
Application number	US-202117454703-A
Country	US
Kind code	B2
Filing date	Nov 12, 2021
Priority date	Nov 17, 2020
Publication date	May 16, 2023
Grant date	May 16, 2023

Abstract

A method of inspecting a surface of a component, e.g. a turbine or compressor blade of a gas turbine engine. The method comprises (a) providing a probe for inspecting the component surface; (b) defining a reference surface that is offset from the component surface; (c) moving the probe so as to contact a plurality of discrete spaced apart inspection points on the component surface, each contact of the probe with an inspection point comprising a first movement of the probe from the reference surface to the inspection point; (d) retracting the probe from the component surface after each contact with an inspection point; and (e) inspecting the component surface each time the probe contacts an inspection point.

First claim

We claim:

1. A method of inspecting a surface of a component, the method comprising the steps of:
providing a probe for inspecting the component surface, wherein the probe is an eddy current probe;
defining a reference surface that is offset from the component surface;
moving the probe so as to contact a plurality of discrete spaced apart inspection points on the component surface, each contact of the probe with an inspection point comprising a first movement of the probe from the reference surface to the inspection point;
retracting the probe from the component surface after each contact with an inspection point; and
inspecting the component surface each time the probe contacts an inspection point, wherein the inspection comprises eddy current testing.

2. The method of claim 1 , wherein movement of the probe is along a tool path and the method further comprises defining the tool path.

3. The method of claim 1 , wherein the probe is spring loaded.

4. The method of claim 1 , wherein the probe includes a camera and an illuminated camera system.

5. The method of claim 1 , wherein the component is a blade or vane of a gas turbine engine.

6. The method of claim 1 , further comprising receiving a continuous time-based signal from the probe and identifying portions of the signal that are associated with the probe being in contact with an inspection point of the component surface.

7. The method of claim 6 , further comprising determining, for each of the portions of the signal, whether the portions of the signal are indicative of a defect in the component surface.

8. The method of claim 1 , wherein each contact of the probe with an inspection point further comprises a second movement of the probe from the inspection point to the reference surface.

9. The method of claim 8 , wherein the first and second movements of the probe are each in a direction that is normal to the component surface at the inspection point.

10. The method of claim 8 , wherein the first and second movements of the probe are each in a direction that is at an angle to a direction normal to the component surface at the inspection point.

11. The method of claim 8 , wherein each contact of the probe with an inspection point further comprises a third movement of the probe along the reference surface.

12. The method of claim 1 , wherein the probe is mounted to a robotic device.

13. The method of claim 12 , wherein the probe is moved relative to the robotic device.

14. The method of claim 12 , wherein movement of the probe is by the robotic device and the probe is maintained in a fixed position relative to the robotic device throughout the movement of the probe.

15. The method of claim 14 , wherein movement of the probe along the reference surface is provided by moving the robotic device while maintaining the probe in a fixed position relative to the robotic device, and each movement of the probe towards or away from the component surface is performed by moving the probe relative to the robotic device.

Assignees

• Rolls Royce Plc

Inventors

• Jeketo Alejandro
• Walker Ben J
• Kell James

Classifications

• G01N27/902

  by moving the sensors · CPC title

• G01B7/34

  for measuring roughness or irregularity of surfaces · CPC title

• G01B7/285 Primary

  of propellers or turbine blades · CPC title

• B25J9/1679

  characterised by the tasks executed · CPC title

• G01M15/14 Primary

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