IP Library › Granted Patent US 11,104,068
Granted Patent B2
US 11,104,068 · App. 15/802,567 · Granted Aug 31, 2021

Method for enhancing the finish of additively-manufactured components

Inventors: Laura Buerger (Dachau, DE); Ralph Kropp (Wartenberg, DE); Jeroen Risse (Aachen, DE)
Assignee: MTU AERO ENGINES AG
B29C64/188B22F10/20B29C64/153B33Y10/00B33Y30/00B33Y40/00B22F10/30B22F2003/247B29C64/35Y02P10/25
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Quick Facts
Patent No.
US 11,104,068
App. No.
15/802,567
Granted
Aug 31, 2021
Kind
B2
Abstract

Discloses are a method and apparatus for the additive manufacture of components by applying layers of powder material on a substrate or a previously produced part of a component and at least partial fusing of the powder material in the powder layer in line with the component cross-section contour along the powder layer and to an underlying solid material of the component or substrate for the purpose of building up several solid layers one on top of the other. Following fusion of the powder material the solid layer just generated is cleaned of powder material and, prior to deposition of the next solid layer, the edge of the solid layer is post-processed by softening the fusion-bonded material.

Claims (17)

1. A method for the additive manufacturing of a component, wherein the method comprises applying layers of powder material on a substrate or a previously produced part of a component and at least partial fusing of the powder material in a powder layer in line with a component cross-section contour along the powder layer and to an underlying solid material of the component or substrate for the purpose of building up several solid layers disposed one on top of the other, and wherein after producing a solid layer by fusion of the powder material and subsequent solidification, the solid layer just generated is cleaned of powder material and then, prior to deposition of a next solid layer, an edge of the solid layer is post-processed by heating the edge of the solid layer so that only material at the edge is at least one of softened and remelted and thereafter solidified again.

2. The method of claim 1 , wherein cleaning of the solid layer of powder material is carried out after every deposition of a solid layer.

3. The method of claim 1 , wherein the cleaning of a solid layer comprises removal of powder material from one or more solid layers deposited prior to a most recently applied solid layer.

4. The method of claim 1 , wherein cleaning of the solid layer is carried out by at least one method selected from mechanical removal of powder material, brushing, wiping, vacuuming, cleaning by spraying with a fluid, blowing off with compressed air or other gases, raising from a surrounding powder bed and lowering of a powder bed.

5. The method of claim 1 , wherein fusing of the powder material is carried out by employing an energy beam.

6. The method of claim 5 , wherein fusing of the powder material is carried out by at least one of selective laser melting or sintering and selective electron beam melting or sintering.

7. The method of claim 1 , wherein post-processing of the edge of a solid layer is carried out several times prior to deposition of a next solid layer.

8. The method of claim 1 , wherein heating of the edge of the solid layer results in softening and/or melting the edge of the solid layer and is carried out by using an energy beam.

9. The method of claim 8 , wherein the energy beam comprises at least one of a laser beam and an electron beam.

10. The method of claim 8 , wherein softening and/or melting of the edge of the solid layer is effected with from 60% to 90% of that power of the energy beam with which fusing of the powder material occurs during deposition of a solid layer.

11. The method of claim 8 , wherein softening and/or melting of the edge of the solid layer is effected with from 70% to 80% of that power of the energy beam with which fusing of the powder material occurs during deposition of a solid layer.

12. The method of claim 8 , wherein softening and/or melting of the edge of the solid layer takes place at from 20% to 50% of that feed rate of the energy beam at which the energy beam for fusing the powder material is moved during deposition of a solid layer.

13. The method of claim 8 , wherein softening and/or melting of the edge of the solid layer takes place at from 30% to 40% of that feed rate of the energy beam at which the energy beam for fusing the powder material is moved during deposition of a solid layer.

14. The method of claim 10 , wherein softening and/or melting of the edge of the solid layer takes place at from 20% to 50% of that feed rate of the energy beam at which the energy beam for fusing the powder material is moved during deposition of a solid layer.

15. The method of claim 11 , wherein softening and/or melting of the edge of the solid layer takes place at from 30% to 40% of that feed rate of the energy beam at which the energy beam for fusing the powder material is moved during deposition of a solid layer.

16. The method of claim 1 , wherein an energy beam for post-processing by heating stems from the same radiation source as an energy beam for fusing the powder material.

17. The method of claim 16 , wherein the energy beams for the post-processing and fusion are generated differently and/or are influenced or shaped differently.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 4, 2022
From: MTU AERO ENGINES AG
To: FRAUNHOFER GESELLSCHAFT, PATENTE UND LIZENZEN
Reel/Frame 058888/0512 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 11, 2018
From: BUERGER, LAURA; KROPP, RALPH; RISSE, JEROEN
To: MTU AERO ENGINES AG; FRAUNHOFER-GESELLSCHAFT ZUR FOERDERUNG DER ANGEWANDTEN FORSCHUNG E.V.
Reel/Frame 044595/0537 →
Priority Claims (1)
DE 102016121594.5 · Nov 10, 2016 · national
Continuity (1)
Related Publication 20180126634A1 · May 10, 2018