Method for the production on a three-dimensional product

Patent metadata

Field	Value
Publication number	US-10315272-B2
Application number	US-201615012076-A
Country	US
Kind code	B2
Filing date	Feb 1, 2016
Priority date	Feb 9, 2015
Publication date	Jun 11, 2019
Grant date	Jun 11, 2019

Abstract

There is disclosed a method for the production of a three-dimensional product (2) via an additive layer manufacturing process such as an electron beam manufacturing process to selectively fuse parts (17) of a powder bed (16), said parts (17) corresponding to successive cross-sections of the product (2). The method involves the use of said additive layer manufacturing process to form a tool (12) by selectively fusing additional parts (18) of the powder bed (16), said additional parts (18) corresponding to successive cross-sections of the tool (12). The method also comprises a subsequent step of manipulating the tool (12) perform a processing function on the product (2).

First claim

The invention claimed is:

1. A method for the production of a three-dimensional product having a cavity, the method comprising:
producing the product having the cavity via an additive layer manufacturing process to selectively fuse parts of a powder bed, said parts corresponding to successive cross-sections of the product,
removing a cake of sintered powder from at least an external surface of the product,
forming a tool at least partially within the cavity by selectively fusing additional parts of the powder bed through the use of said additive layer manufacturing process, said additional parts corresponding to successive cross-sections of the tool,
hardening the material of the tool to make it harder than the material forming the product, and
manipulating the tool whereby to polish an internal wall of the product which bounds the cavity.

2. The method according to claim 1 , wherein hardening includes chemically treating the material of the tool.

3. The method according to claim 2 , wherein hardening includes carburizing or nitriding the material of the tool.

4. The method according to claim 1 , wherein said additive layer manufacturing process is used to form said tool simultaneously with at least part of said product.

5. The method according to claim 4 , wherein the additive layer manufacturing process comprises the steps of: a) laying down a powder layer on said powder bed, and b) focussing energy on a predetermined area of said powder layer to fuse said area of the powder layer and thereby form a cross-section of the product; wherein steps a) and b) are repeated to form successive cross-sections of the product, and wherein at least some of said successive steps b) include focussing energy on a designated tool area of the respective powder layer, to fuse the tool area and thereby form successive cross-sections of said tool within the powder bed.

6. The method according to claim 5 , the method being used to manufacture a metal component, in which said powder is metal powder, and in which said steps of focussing energy on said areas of the powder layers includes the use of an electron beam to melt said areas of the powder layers.

7. The method according to claim 1 , wherein said additive layer manufacturing process is an electron beam melting process.

8. The method according to claim 1 , wherein said tool is formed in spaced relation to at least one surface of the product.

9. The method according to claim 8 , wherein said tool is shaped such that at least part of the tool substantially conforms to the shape of the or each said surface.

10. The method according to claim 1 , further comprising using the tool to remove sintered powder, arising from the additive layer manufacturing process, from the cavity during or prior to polishing.

11. The method according to claim 1 , wherein manipulating the tool includes vibrating the tool.

12. The method according to claim 11 , wherein the tool is subjected to ultrasonic vibrations.

13. The method according to claim 1 , wherein said tool is formed in a position in which part of the tool projects from the cavity, said projecting part of the tool being used for manipulation of the tool.

14. The method according to claim 10 , wherein said tool is formed in a position in which part of the tool projects from the cavity, said projecting part of the tool being used for manipulation of the tool.

15. The method according to claim 1 , wherein said cavity is a passage extending through at least part of the product.

16. The method according to claim 15 , wherein said tool extends completely through said passage in spaced relation to the or each internal surface of the passage.

17. The method according to claim 15 , wherein said passage follows a non-linear path, and wherein said tool is shaped to follow said path.

18. The method according to claim 1 , wherein the product is a component of a gas turbine engine.

19. The method according to claim 1 , wherein removing the cake of sintered powder from at least the external surface of the product includes air-blasting.

20. The method according to claim 1 , wherein removing the cake of sintered powder from at least the external surface of the product occurs before removing sintered powder within the cavity using the tool.

Assignees

• Rolls Royce Plc

Inventors

• Blackmore Michael Lewis

Classifications

• B23K15/0086 Primary

  welding for purposes other than joining, e.g. build-up welding · CPC title

• B22F5/04 Primary

  of turbine blades · CPC title

• B22F2003/245

  Making recesses, grooves etc on the surface by removing material · CPC title

• B22F2005/002

  Tools other than cutting tools · CPC title

• B33Y10/00

  Processes of additive manufacturing · CPC title