METHOD OF MANUFACTURING A MULTIPLE COMPOSITION COMPONENT

• US 20110123386A1
• Filed: 11/15/2010
• Published: 05/26/2011
• Est. Priority Date: 11/26/2009
• Status: Active Grant

• Current Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Inventors: HOLMES, Shaun R., MITCHELL, Robert J., HARDY, Mark C., RAE, Catherine M.F.
• Granted Patent: US 8,703,045 B2
• Time in Patent Office: Days
• US Class Current: 419/49
• CPC Class Codes: B22F 2999/00 Aspects linked to processes or compositions used in powder metallurgy
• CPC Class Codes: B22F 3/15 Hot isostatic pressing
• CPC Class Codes: B22F 5/009 of turbine components other than turbine blades of turbine blades B22F5/04
• CPC Class Codes: B22F 5/106 Tube or ring forms
• CPC Class Codes: B22F 7/062 involving the connection or repairing of preformed parts

Abstract

The present invention relates to a method of manufacturing a multiple composition component 10, comprising: arranging first, second and third constituent parts 40, 30, 42 having first, second and third compositions respectively A, B, C so that the first constituent part 40 shares a first boundary with the second constituent part 30 and the second constituent part 30 shares a second boundary with the third constituent part 40. The first, second and third constituent parts 40, 30, 42 are each either a powder or a solid so that the first and second boundaries are each a solid adjacent to a powder. The arrangement is then processed so as to form a single solid component having first, second and third regions 16, 18, 20 having first, second and third compositions A, B, C respectively.

Claims

1. A method of manufacturing a multiple composition component, comprising:

arranging first, second and third constituent parts having first, second and third compositions respectively so that the first constituent part shares a first boundary with the second constituent part and the second constituent part shares a second boundary with the third constituent part;

wherein the first, second and third constituent parts are each either a powder or a solid; and

processing so as to form a single solid component having first, second and third regions having the first, second and third compositions respectively, the processing including hot isostatic pressing and/or diffusion bonding, the hot isostatic pressing and/or diffusion bonding comprising hot isostatic pressing at a first temperature for a first predetermined time and hot isostatic pressing at a second temperature for a second predetermined time, wherein the first temperature is less than the second temperature.

2. A method as claimed in claim 1, wherein the hot isostatic pressing comprises hot isostatic pressing at a first temperature of 850°

C. to 1000°

C. and applying a pressure of 100 MPa for 4 hours and hot isostatic pressing at a second temperature of 50°

C. below the gamma prime solvus temperature of the composition which has the lowest volume fraction of gamma prime phase and applying a pressure of 100 MPa for 2 hours.

3. A method according to claim 1, wherein at least one of the first and second boundaries is a solid adjacent to a powder

4. A method according to claim 3, wherein the first and second boundaries are each a solid adjacent to a powder.

5. A method according to claim 1, wherein the first and/or second boundary is annular.

6. A method according to claim 1, wherein the first and third constituent parts are powders, and the second constituent part is a solid.

7. A method according to claim 1, wherein the first and third constituent parts are solids, and the second constituent part is a powder.

8. A method according to claim 1, wherein the first and second constituent parts are powder, and the third constituent part is a solid or the first and second constituent parts are solid and the third constituent part is a powder.

9. A method according to claim 1, wherein the second composition has a similar gamma phase composition to the gamma phase composition of the first composition and the gamma phase composition of the third composition and the volume fraction of the precipitation strengthening gamma prime phase of the second composition is between the volume fraction of the gamma prime phase of the first composition and the volume fraction of the gamma prime phase of the third composition.

10. A method according to claim 1, wherein the second composition is a mixture of the first and third compositions.

11. A method according to claim 1, wherein the second composition is the same as the first or third composition.

12. A method according to claim 1, wherein the second composition is a pure element which is the same as an element present in the first or third composition.

13. A method according to claim 1, wherein the first, second and third constituent parts are metal alloys.

14. A method according to claim 1, wherein the first and/or secondary boundary comprises a mechanical interlock between a solid and a powder.

15. A method according to claim 1, wherein the component is selected from the group consisting of a turbine disk, a compressor disk, a fan disk, a bladed disk, a bladed ring, a bladed drum and a casing.