System and method for inspection of hole location on turbine airfoils

• US 20070276629A1
• Filed: 04/07/2006
• Published: 11/29/2007
• Est. Priority Date: 04/07/2006
• Status: Active Grant

• Current Assignee: Raytheon Technologies Corporation d/b/a RTX
• Original Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Koonankeil, James
• Granted Patent: US 7,574,035 B2
• Time in Patent Office: Days
• US Class Current: 702/185
• CPC Class Codes: B23P 2700/06 Cooling passages of turbine components, e.g. unblocking or preventing blocking of cooling passages of turbine components
• CPC Class Codes: F01D 25/285 Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures
• CPC Class Codes: F01D 5/005 Repairing methods or devices
• CPC Class Codes: F05D 2230/80 Repairing, retrofitting or upgrading methods
• CPC Class Codes: G01B 11/002 for measuring two or more coordinates
• CPC Class Codes: G01B 11/24 for measuring contours or curvatures

Abstract

An inspection system for locating multiple features on an exterior of an object includes a fixture, a camera, a computer and software. The fixture secures the object and includes a plurality of nest points for mating with specific positions on the exterior of the object, and a reference point located at a specific position relative to the nest points and within a best-plane of the object. The camera is positioned normal to the best-plane of the object and obtains video imaging of a plurality of the features and the reference point. The computer communicates with the camera and collects the video imaging. The software determines the actual parameters of the features relative to the reference point based on the video imaging.

Claims

1. An inspection system for locating multiple features on an exterior of an object, the inspection system comprising:

a fixture for securing the object comprising;

a plurality of nest points for mating with specific positions on the exterior of the object; and

a reference point located at a specific position relative to the nest points and within a best-plane of the object;

a camera positioned normal to the best-plane of the object for obtaining video images of a plurality of the features and the reference point;

a computer in communication with the camera for collecting the video images; and

software for determining actual location of the features relative to the reference point based on the video images.

2. The inspection system of claim 1 wherein the camera is a fixed-focus cameras.

3. The inspection system of claim 1 and further comprising an LED light source to enhance contrast between the object and the features.

4. The inspection system of claim 1 wherein the best-plane comprises a plane relative to the exterior of the object wherein a plurality of the multiple features on the exterior of the object are visible from a single vantage point.

5. The inspection system of claim 4 wherein the camera is fixed at the single vantage point such that the camera views the features and the reference point from a known orientation.

6. The inspection system of claim 1 and further comprising:

a plurality of best-planes for the object;

a plurality of reference points on the fixture; and

a camera provided for each best-plane such that it captures at least one of the reference points.

7. The inspection system of claim 1 wherein the reference point comprises a circular hole in the fixture.

8. The inspection system of claim 7 wherein a plane parallel to a front of the hole is parallel to the best-plane.

9. The inspection system of claim 1 wherein the software includes design parameters for each of the features normalized to a best-plane view of the camera and compares the design parameters of the features with actual parameters of the features.

10. The inspection system of claim 9 wherein the software locates the actual parameters and design parameters on a coordinate system referenced from the reference point.

11. The inspection system of claim 9 wherein the parameters include location and shape.

12. The inspection system of claim 1 wherein the software:

determines a plurality of points around the periphery of each feature as visible from the best-plane to define a shape;

determines a centroid of the shape;

assigns a coordinate location to the centroid relative to a reference point; and

compares the coordinate location to a design coordinate location for the shape.

13. The inspection system of claim 1 wherein the object comprises a blade for a gas turbine engine and the features comprise cooling holes located on facets of the blade.

14. A method for locating multiple features on an object, the method comprising:

positioning the object in a fixture such that the fixture mates with the object at specific nest points;

positioning a reference point on the fixture relative to the nest points and within a best-plane of the object;

positioning a camera along a best-plane of the object such that it has a view of multiple features within the best-plane and the reference point;

capturing a video image of the object including a plurality of the features and the reference point;

performing software analysis of the video image to locate actual positions of the plurality of features relative to the reference point.

15. The method of claim 14 and further comprising the step of shining a light source at the object in order to produce contrast between the object and the features.

16. The method of claim 14 wherein the best-plane comprises a plane relative to the exterior of the object wherein a plurality of the features on the exterior of the object are visible from a single vantage point.

17. The method of claim 16 wherein the camera is fixed at the single vantage point such that the camera views the features and the reference point from a known orientation.

18. The method of claim 14 wherein the step of positioning a reference point comprises positioning a circular hole in the fixture in a plane parallel to the best-plane.

19. The method of claim 14 and further comprising the step of comparing the actual positions with design positions for each of the features normalized to a best-plane view of the camera.

20. The system of claim 14 and further comprising:

determining a plurality of points around the periphery of each feature as visible from the best-plane to define a shape;

determining a centroid of the shape;

assigning a coordinate location to the centroid relative to a reference point; and

comparing the coordinate location to a reference coordinate location for the shape.

21. The method of claim 14 wherein the object comprises a blade for a gas turbine engine and the features comprise cooling holes located on facets of the blade.

22. The method of claim 14 wherein the software analysis determines a shape of each feature for comparison with a design shape of the feature.