Adaptive repair method for aerofoil blades

• US 10,452,809 B2
• Filed: 04/21/2017
• Issued: 10/22/2019
• Est. Priority Date: 04/29/2016
• Status: Active Grant

• Current Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Inventors: Huckerby, Karl S.
• Primary Examiner(s): Johnson, Cedric
• Application Number:
  US15/493,192
• Publication Number:
  US 20170316146A1
• Time in Patent Office: 914 Days
• Field of Search: None
• CPC Class Codes: B23P 6/007 using only additive methods, e.g. build-up welding
• CPC Class Codes: F01D 5/005 Repairing methods or devices
• CPC Class Codes: G05B 19/401 characterised by control arrangements for measuring, e.g. calibration and initialisation, measuring workpiece for machining purposes G05B19/19 takes precedence
• CPC Class Codes: G05B 2219/45147 Machining blade, airfoil
• CPC Class Codes: G06F 30/17 Mechanical parametric or variational design
• CPC Class Codes: G06F 30/20 Design optimisation, verification or simulation optimisation, verification or simulation of circuit designs G06F30/30
• CPC Class Codes: Y02P 90/02 Total factory control, e.g. smart factories, flexible manufacturing systems [FMS] or integrated manufacturing systems [IMS]

Abstract

This disclosure concerns an adaptive repair method, for example for aerofoil blade components. The method generates a digitized model of a physical component and uses data from the digitized model to align a part of the physical component with a nominal CAD model of the component. A combination of the digitized data and data from the nominal CAD model are then used to create an adapted model for repair of the component.

Claims

1. An adaptive repair method comprising:

providing a digitized model of a base portion of a physical component;

aligning a corresponding base portion of a nominal CAD model of the physical component with the digitized model of the base portion of the physical component such that the nominal CAD model extends beyond the digitized model of the base portion of the physical component used for alignment;

extracting a set of co-ordinate points from the nominal CAD model once aligned;

lofting a cross-sectional profile based on a measured profile of the base portion along a path defined by the co-ordinate points of the nominal CAD model once aligned to the digitized model of the base portion of the physical component to create an adapted model for repair of the physical component; and

adding material to the physical component based on the adapted model as part of adaptively repairing the physical component.

2. The adaptive repair method according to claim 1, wherein the digitized model of the base portion of the physical component is created by digitizing an entire component and electronically cutting back the resulting model to a predetermined crop plane.

3. The adaptive repair method according to claim 1, wherein the physical component is physically cut back before being digitized to create the digitized model of the base portion of the physical component.

4. The adaptive repair method according to claim 1, wherein the cross-sectional profile is adapted to create an oversized material addition region in the adapted model for adding material to the physical component.

5. The adaptive repair method according to claim 4, wherein the adapted model includes tool path data within the oversized material addition region for a reprofiling step in the adaptive repair method.

6. The adaptive repair method according to claim 1, further comprising machining the physical component based on the adapted model.

7. The adaptive repair method according to claim 1, wherein the physical component is an aerofoil blade and the co-ordinate points comprise points at the leading edge and/or trailing edge of the aerofoil blade.

8. The adaptive repair method according to claim 7, wherein the co-ordinate points comprise points on the concave and/or convex surfaces of the aerofoil blade.

9. The adaptive repair method according to claim 1, wherein the co-ordinate points are located in a number of planes, at least one of the planes intersecting the digitized model of the base portion of the physical component, and at least one plane being located beyond the digitized model of the base portion of the physical component.

10. The adaptive repair method according to claim 9, wherein at least ten planes are located beyond the digitized model of the base portion of the physical component.

11. The adaptive repair method according to claim 9, wherein at least three planes intersect the digitized model of the base portion of the physical component.

12. The adaptive repair method according to claim 9, wherein at four planes intersect the digitized model of the base portion of the physical component and seventeen planes are located beyond the digitized model of the base portion of the physical component.

13. An adaptive repair method comprising:

providing a component, a digitized model of a portion of the component, and an adapted model; and

adding material to the component based on the adapted model as part of adaptively repairing the component, wherein the adapted model is provided by;

aligning a corresponding portion of a nominal CAD model of the component with the digitized model of the base portion of the component such that the nominal CAD model extends beyond the digitized model of the portion of the component,

extracting a set of co-ordinate points from the aligned nominal CAD model, and

lofting a cross-sectional profile based on a measured profile of the portion along a path defined by the co-ordinate points of the aligned nominal CAD model to create the adapted model for repair of the component.

14. The adaptive repair method according to claim 13, further comprising machining the component based on the adapted model.

15. The adaptive repair method according to claim 13, wherein the digitized model of the portion of the component is created by digitizing an entire component and electronically cutting back the resulting model to a predetermined crop plane.

16. The adaptive repair method according to claim 13, wherein the component is physically machined before digitizing to create the digitized model of the portion of the component.

17. An adaptive repair method comprising:

providing a digitized model of a base portion of a physical component;

aligning a corresponding base portion of a nominal CAD model of the physical component with the digitized model of the base portion of the physical component such that the nominal CAD model extends beyond the digitized model used for alignment;

extracting a set of co-ordinate points from the aligned nominal CAD model; and

lofting a cross-sectional profile based on a measured profile of the base portion along a path defined by the co-ordinate points of the aligned nominal CAD model to create an adapted model for repair of the physical component; and

machining the physical component based on the adapted model.

18. The adaptive repair method according to claim 17, wherein the digitized model of the base portion of the physical component is created by digitizing an entire component and electronically cutting back the resulting model to a predetermined crop plane.

19. The adaptive repair method according to claim 17, wherein the physical component is physically machined before digitizing to create the digitized model of the base portion of the physical component.

20. The adaptive repair method according to claim 17, wherein the adapted model includes tool path data within an oversized material addition region for a reprofiling step in the repair process.