Method of surface-treating a cast intermetallic component

Patent metadata

Field	Value
Publication number	US-10106876-B2
Application number	US-201514966237-A
Country	US
Kind code	B2
Filing date	Dec 11, 2015
Priority date	Jan 9, 2015
Publication date	Oct 23, 2018
Grant date	Oct 23, 2018

Abstract

There is proposed a method of surface-treating a cast intermetallic component, which is intended primarily to reduce or remove surface porosity from the component. The method includes the steps of: providing a cast intermetallic component; placing the component in an inert atmosphere; focussing a laser beam on a surface of the component; traversing the laser beam over at least a region of said surface while the component is in said inert atmosphere; and controlling the laser beam during said traversing step so as to locally melt the intermetallic material of the component to a depth of no more than 300 μm, as measured from said surface of the component.

First claim

The invention claimed is:

1. A method of surface-treating a cast intermetallic titanium component, the method comprising the steps of:
providing a cast intermetallic titanium component;
placing the cast intermetallic titanium component in an inert atmosphere;
focussing a laser beam on a surface of the cast intermetallic titanium component;
traversing the laser beam over at least a region of said surface whilst the cast intermetallic titanium component is in said inert atmosphere; and
controlling the laser beam during said traversing step so as to locally melt the intermetallic material of the cast component to a predetermined threshold depth of no more than 300 μm, as measured from said surface of the cast component,
the method further including a step of analysing the cast component, prior to said steps of focussing and traversing the laser beam, in order to identify target surface-connected and/or near-surface pores in the cast component and determining the maximum depth of said target pores from the surface of the cast component; wherein said step of controlling the laser beam comprises operating the laser beam so as to locally melt the intermetallic material of the cast component to said maximum depth,
the analysing step comprising comparing the maximum depth of the target pores to the predetermined threshold depth, if the maximum depth of the target pores is less than or equal to the predetermined threshold depth, then the laser beam is focussed on the surface of the cast component and the laser beam is traversed over at least the surface whilst the cast component is in said inert atmosphere.

2. A method according to claim 1 , wherein the laser beam is controlled so as to locally melt the intermetallic material of the cast component to a depth of no more than 150 μm as measured from said surface of the cast component.

3. A method according to claim 1 , wherein said step of analysing the cast component comprises capturing an image of the surface region of the cast component.

4. A method according to claim 3 , wherein said image comprises a stereo-optical image.

5. A method according to claim 3 , wherein said image comprises an X-ray image.

6. A method according to claim 3 , wherein said step of controlling the laser beam comprises controlling the laser beam based on features of said image.

7. A method according to claim 3 , wherein said step of analysing the cast component is performed manually.

8. A method according to claim 3 , wherein said step of analysing the cast component is performed automatically using a computer.

9. A method according to claim 1 , wherein said focussing step comprises focussing the laser beam such that it energizes a target area on the surface of the cast component, and wherein said step of traversing comprises moving the laser beam incrementally relative to the cast component so as to energize successive said target areas on the surface of the cast component; each target area being energized for a discrete dwell period and overlapping at least the immediately preceding target area.

10. A method according to claim 1 , wherein said step of traversing comprises movement of the laser beam.

11. A method according to claim 1 , wherein said step of traversing comprises movement of the cast component.

12. A method according to claim 1 , wherein a heat load is applied to said cast component during said focussing, traversing and controlling steps, said heat load being applied to the opposite side of the cast component to that on which said surface is provided.

13. A method according to claim 1 , wherein said cast component is pre-tensioned during said focussing, traversing and controlling steps.

14. A method according to claim 1 , wherein said step of controlling the laser beam comprises controlling at least one of: the power; the focus; the beam-shape; and the pulse period of the laser beam.

15. A method according to claim 1 , performed on a cast component which is formed of gamma titanium aluminide.

16. A method according to claim 1 , performed on a cast component in the form of a turbine blade for a gas turbine engine.

17. A method according to claim 1 , wherein said step of placing the cast component in an inert atmosphere comprises placing the cast component in a vacuum chamber.

18. A method according to claim 1 , comprising the use of a plurality of said laser beams.

19. A method according to claim 1 , performed simultaneously on a plurality of said cast components.

20. A method according to claim 1 , further comprising hot isostatic pressing the cast component after the steps of focussing and traversing the laser beam.

21. A method of surface-treating a cast intermetallic titanium component, the method comprising the steps of:
providing a cast intermetallic titanium component;
placing the cast intermetallic titanium component in an inert atmosphere;
focussing a laser beam on a surface of the cast intermetallic titanium component; traversing the laser beam over at least a region of said surface whilst the cast intermetallic titanium component is in said inert atmosphere; and
controlling the laser beam during said traversing step so as to locally melt the intermetallic material of the cast component to a predetermined threshold depth of no more than 300 μm, as measured from said surface of the cast component, and hot isostatic pressing the cast component,
the method further including a step of analysing the cast component, prior to said steps of focussing and traversing the laser beam, in order to identify target surface-connected and/or near-surface pores in the cast component and determining the maximum depth of said target pores from the surface of the cast component; wherein said step of controlling the laser beam comprises operating the laser beam so as to locally melt the intermetallic material of the cast component to said maximum depth,
the step of analysing the component comprises capturing an image of the surface region of the component and the image is selected from the group consisting of a stereo-optical image, an X-ray image and a combination of a stereo-optical image and an X-ray image.

Assignees

• Rolls Royce Plc

Inventors

• Tuppen Stephen John
• Clark Daniel

Classifications

• F05D2230/40

  Heat treatment · CPC title

• B23K26/123

  in an atmosphere of particular gases · CPC title

• C22F1/183 Primary

  of titanium or alloys based thereon · CPC title

• F01D5/286

  Particular treatment of blades, e.g. to increase durability or resistance against corrosion or erosion (F01D5/288 takes precedence) · CPC title

• C21D1/34

  Methods of heating (C21D1/06 takes precedence) · CPC title