Process for the production of articles made of a gamma-prime precipitation-strengthened nickel-base superalloy by selective laser melting (SLM)

Patent metadata

Field	Value
Publication number	US-9844812-B2
Application number	US-201213667172-A
Country	US
Kind code	B2
Filing date	Nov 2, 2012
Priority date	Nov 4, 2011
Publication date	Dec 19, 2017
Grant date	Dec 19, 2017

Abstract

A process for producing a crack-free and dense three-dimensional article of a gamma-prime precipitation-strengthened nickel-base superalloy, with more than 6 wt. % of [2 Al (wt. %)+Ti (wt. %)], which involves: (a) preparing a powder layer of a gamma-prime precipitation-strengthened nickel-based alloy material, with uniform thickness on a SLM apparatus substrate plate, or on a previously processed powder layer; (b) melting the prepared powder layer by scanning with a focused laser beam an article cross section area according to a three-dimensional sliced model with calculated cross sections, stored in the SLM control unit; (c) lowering the substrate plate by one layer thickness; and (d) repeating (a) to (c) until reaching a final cross section according to the three-dimensional sliced model, wherein, for (b), the laser power, focus diameter of the focal spot, and scan speed of the focused laser beam are adjusted to obtain heat dissipation welding.

First claim

The invention claimed is:

1. A process for producing a crack-free three-dimensional article by selective laser melting (SLM), the process comprising:
(a) preparing a powder layer, including a powder of a material including a gamma-prime precipitation-strengthened nickel-base alloy, with a regular and uniform thickness on a substrate plate of an SLM apparatus or on a previously processed powder layer;
(b) melting the prepared powder layer by scanning with a focused laser beam an area corresponding to a cross section of the article according to a three-dimensional sliced model of the article, with calculated cross sections, stored in an SLM control unit of an SLM apparatus, the melting performed such that a laser power, focus diameter of the focal spot, and scan speed of the focused laser beam are adjusted to obtain heat dissipation welding resulting in a weld bead aspect ratio of depth to width smaller than 0.5 during the melting of the prepared powder layer, wherein the laser power is 50-150 W, the scan speed is 80-700 mm/s, the focus diameter is 0.1-0.5 mm, and a hatch distance for the laser is 0.01-0.5 mm and a laser operational mode for generating the laser beam is a continuous wave mode;
(c) lowering the substrate plate by one layer thickness;
(d) repeating (a) to (c) until reaching a final cross section according to the three-dimensional sliced model, and
wherein, in (a), the gamma-prime precipitation-strengthened nickel-base alloy comprises more than 6 wt. % of [2 Al (wt. %)+Ti (wt. %)] and wherein the gamma-prime precipitation-strengthened nickel-base alloy comprises Ni, unavoidable impurities, and:
3.2-4.2 wt. % Al,
2.8-3.8 wt. % Ti,
14.5-17 wt. % Cr,
7.8-9.0 wt. % Co,
1.2-1.9 wt. % Mo,
2.1-3.5 wt. % W,
1.0-2.0 wt. % Ta,
0.5-1.5 wt. % Nb,
<0.15 wt. % C, and
<0.02 wt. % B.

2. The process of claim 1 , wherein, in (b), a laser source-in pulsed mode is used and a pulse frequency thereof is adjusted to obtain heat dissipation welding.

3. The process of claim 1 , wherein adjustment of the focus diameter is done with specific focusing equipment.

4. The process of claim 1 , wherein adjustment of the focus diameter is done by displacing the substrate plate.

5. The process of claim 1 , comprising adjusting a particle size distribution of the powder with respect to the thickness of the powder layer, such that the powder is flowable and has a bulk density >60% for preparing powder layers with regular and uniform thickness and to reduce shrinking effects.

6. The process of claim 5 , wherein an exact particle size distribution is obtained by sieving.

7. The process of claim 1 , wherein the powder is obtained by gas atomization.

8. The process of claim 1 , wherein (a) to (c) are performed in a protective gas atmosphere.

9. The process of claim 8 , wherein the protective gas atmosphere comprises nitrogen or argon.

10. The process of claim 1 , further comprising:
cooling substrate plate to conduct away process heat and thereby reducing time required for solidification of the weld bead.

11. The process of claim 1 , further comprising, prior to the melting (b):
pre-melting the powder to loosely melt or pre-sinter the powder of the powder layer together, whereafter the melting of the prepared powder layer is performed to make the powder layer more dense to obtain a denser three-dimensional article.

12. The process of claim 1 , further comprising, after the article has been formed into a three-dimensional article:
applying a post heat treatment to the three-dimensional article to further optimize a microstructure thereof.

13. The process of claim 12 , wherein the post heat treatment is hot isostatic pressing (HIP).

14. The process of claim 1 , wherein the weld bead aspect ratio of depth to width is between 0.3 and 0.1.

15. The process of claim 5 , wherein an exact particle size distribution is obtained by winnowing or air separation.

16. The process of claim 5 , wherein an exact particle size distribution is obtained by sieving and winnowing.

17. The process of claim 1 , wherein the powder is obtained by a plasma-rotating-electrode process.

18. The process of claim 8 , wherein the gamma-prime precipitation-strengthened nickel-base alloy consists of Ni, unavoidable impurities, and:
3.2-4.2 wt. % Al,
2.8-3.8 wt. % Ti,
14.5-17 wt. % Cr,
7.8-9.0 wt. % Co,
1.2-1.9 wt. % Mo,
2.1-3.5 wt. % W,
1.0-2.0 wt. % Ta,
0.5-1.5 wt. % Nb,
<0.15 wt. % C, and
<0.02 wt. % B; and
wherein the protective gas atmosphere comprises a gas suitable to establish a reducing atmosphere.

Assignees

• Alstom Technology Ltd
• Ansaldo Energia Ip Uk Ltd

Inventors

• Rickenbacher Lukas Emanuel
• Spierings Adriaan Bernardus

Classifications

• B22F3/15

  Hot isostatic pressing · CPC title

• B22F2999/00

  Aspects linked to processes or compositions used in powder metallurgy · CPC title

• B22F2003/248

  Thermal after-treatment · CPC title

• B22F9/082

  atomising using a fluid (using centrifugal force B22F9/10) · CPC title

• B33Y10/00

  Processes of additive manufacturing · CPC title