Method of providing an abrasive means and of additively manufacturing a component

Patent metadata

Field	Value
Publication number	US-11033964-B2
Application number	US-201716302651-A
Country	US
Kind code	B2
Filing date	Jun 1, 2017
Priority date	Jun 13, 2016
Publication date	Jun 15, 2021
Grant date	Jun 15, 2021

Abstract

A method of providing an abrasive structure for additive manufacturing includes determining of a design of a portion of a powdery base material and selectively solidifying the portion in a bed of the base material according to the determined design such that an abrasive structure is generated, wherein the abrasive structure is still movable in the bed of the base material. Further, an additively manufactured component has an internal surface with a surface roughness of less than 100 μm, preferably less than 60 μm.

First claim

The invention claimed is:

1. A method of additively manufacturing a component comprising:
additively assembling a structure for the component out of the bed such that the structure is provided with an internal surface and the base material covers at least a part of the internal surface,
providing the abrasive structure comprising determining of a design of a portion of a powdery base material and selectively solidifying the portion in a bed of the base material according to the determined design such that an abrasive structure is generated, wherein the abrasive structure is movable in the bed of the base material, and
actuating the abrasive structure such that the internal surface is mechanically processed by the abrasive structure.

2. The method according to claim 1 ,
wherein the selective solidification is carried out in that a scanning speed of a solidification unit, or a laser unit of an according additive manufacturing system, is adjusted according to the determined design of the abrasive structure.

3. The method according to claim 1 ,
wherein the design of the portion is determined such that a plurality of clusters are formed for the abrasive structure within the bed of the base material.

4. The method according to claim 1 ,
wherein a partly assembled structure or a component is assembled such that, an internal surface defines a cavity in which the abrasive structure is retained.

5. The method according to claim 4 ,
wherein the abrasive structure is an abrasive blasting means and wherein a fluid or pressure blast is guided through an opening from an outside of the cavity such that the internal surface is mechanically processed by the abrasive structure.

6. The method according to claim 4 ,
wherein after additive assembly, the cavity is sealed.

7. The method according to claim 4 , further comprising, after actuation of the abrasive structure, opening of the cavity such that the base material and/or the abrasive structure at least partly is removeable from the cavity.

8. The method according to claim 4 ,
wherein the component is completed, and one or more cluster(s) remain in the cavity, allowing for damping dynamic loads during an operation of the component.

9. The method according to claim 1 ,
wherein the abrasive structure is a vibratory abrasive means.

10. The method according to claim 1 ,
wherein the determining of the design is carried out by a computer algorithm such that the internal surface is effectively mechanically processed.

11. The method according to claim 1 , wherein the internal surface:
includes a surface roughness of less than 100 μm.

12. The method according to claim 11 ,
wherein the internal surface has a surface roughness of less than 60 μm.

Assignees

• Siemens Ag
• Siemens Energy Global Gmbh & Co Kg

Inventors

• Geisen Ole

Classifications

• B22F10/66

  by mechanical means · CPC title

• B22F10/36

  of energy beam parameters · CPC title

• B22F10/28

  Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM] · CPC title

• B33Y40/20

  Post-treatment, e.g. curing, coating or polishing · CPC title

• B33Y40/00

  Auxiliary operations or equipment, e.g. for material handling · CPC title