Device and a method for fabricating a three-dimensional part by selectively melting a powder bed

Patent metadata

Field	Value
Publication number	US-11980943-B2
Application number	US-202117382850-A
Country	US
Kind code	B2
Filing date	Jul 22, 2021
Priority date	Dec 14, 2015
Publication date	May 14, 2024
Grant date	May 14, 2024

Abstract

A device for fabricating a three-dimensional part by selectively melting a powder bed, the device including a first tank for containing a first powder and provided with a first powder dispenser valve, a second tank for containing a second different powder and provided with a second powder dispenser valve, a first and a second monitoring device for monitoring the quantity of first powder delivered by the first valve and the quantity of second powder delivered by the second valve, a mixer chamber in communication with the first and second valves and including a third powder dispenser valve, and a mixer for mixing the powder particles in the chamber, a support for receiving the powder delivered by the third valve and on which the parts is to be fabricated, a powder spreader for spreading powder on the support, and a heater member for locally melting the powder spread on the support.

First claim

The invention claimed is:

1. A method of fabricating a three-dimensional part by selectively melting a powder bed, the part comprising a successive stack of layers, the method comprising the following steps for fabricating one layer:
a) delivering a monitored quantity of a first powder from a first tank;
b) delivering a monitored quantity of a second powder different from the first powder from a second tank;
c) mixing the first powder and the second powder as delivered in steps a) and b);
d) depositing a layer of the mixture of the first powder and the second powder obtained in step c); and
e) melting at least a portion of the layer of the mixture deposited in step d),
wherein the first powder presents a first grain size and the second powder presents a second grain size, the first grain size being different from the second grain size,
wherein the mixing at step c) comprises:
mixing the first powder and the second powder within a mixer chamber, the mixing chamber comprising an inlet orifice and an outlet orifice for a gas stream inside the mixer chamber, said gas stream inlet and outlet orifices being configured to cause a gas to flow in the mixer chamber so as to mix the first powder and the second powder contained in said mixer chamber, and
wherein the outlet orifice has a protection cover configured to prevent powder from escaping from the mixer chamber via said outlet orifice, and said method further comprising preventing powder from escaping from the mixer chamber via said outlet orifice using the protection cover.

2. The method according to claim 1 , wherein the monitored quantity of the first powder and/or the monitored quantity of the second powder varies between two successive layers.

3. The method according to claim 1 , wherein the three-dimensional part for fabrication is a part for aviation.

4. The method according to claim 1 , further comprising:
monitoring with a first monitoring device the quantity of first powder delivered from the first tank; and
monitoring with a second monitoring device the quantity of second powder delivered from the second tank.

5. The method according to claim 1 , further comprising:
spreading the layer of the mixture using a powder spreader on a support.

6. The method according to claim 1 , wherein the mixing at step c) comprises receiving a gas stream for mixing said first powder and said second powder.

7. The method according to claim 1 , wherein the first and second powders are made of the same material.

8. The method according to claim 1 , wherein the first and second powders are made of materials that are different.

9. The method according to claim 8 , wherein the first powder is constituted by a first material and the second powder is constituted by a second material, the first and second materials being chemically compatible.

10. The method according to claim 8 , wherein the first powder is constituted by a metal alloy and the second powder is constituted by a pure metal.

11. The method according to claim 4 , wherein the first monitoring device and the second monitoring device each comprise scales for weighing the respective powder.

12. The method according to claim 1 , wherein the melting at step e) comprises utilizing a laser or an electron beam generator.

13. The method according to claim 1 , further comprising recovering powder in succession from one of the first tank and the second tank, and then from the other of the first tank and the second tank.

Assignees

• Safran Aircraft Engines

Inventors

• Mottin Jean-Baptiste
• Fribourg Guillaume

Classifications

• B22F5/04 Primary

  of turbine blades · CPC title

• B22F3/003

  Apparatus, e.g. furnaces (in general F27B) · CPC title

• B22F7/06

  of composite workpieces or articles from parts, e.g. to form tipped tools {(B22F7/002 takes precedence)} · CPC title

• B22F10/28

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

• B22F12/57

  Metering means · CPC title