IP Library Granted Patent US 12,337,528
Granted Patent B2
US 12,337,528 · App. 15/102,087 · Granted Jun 24, 2025

Method for producing a part by selective melting of powder

Inventors: Stephane Knittel (Moissy-Cramayel, FR); Pascal Fabrice Bilhe (Moissy-Cramayel, FR)
Assignee: SAFRAN AIRCRAFT ENGINES
B29C64/153B22F3/1039B22F3/23B22F10/28B23K15/0086B23K15/0093B23K26/0006B23K26/342B33Y10/00B33Y80/00C22C1/047C22C1/058C22C32/0078F01D5/28B22F5/009B22F5/04B22F12/63B23K2101/001B23K2103/08B23K2103/10B23K2103/14F05D2220/323F05D2230/233F05D2230/234F05D2230/31F05D2300/11F05D2300/121F05D2300/131F05D2300/132Y02P10/25
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Quick Facts
Patent No.
US 12,337,528
App. No.
15/102,087
Granted
Jun 24, 2025
Kind
B2
Abstract

A method of fabricating a part by selectively melting powder is provided. The method includes: depositing a first layer of a first powder having a first element as its main element; depositing, on the first layer, a second layer of a second powder having a second element as its main element, which second element is different from the first element; and moving a first energy beam over the second layer, the energy delivered by the first beam serving to initiate an exothermic reaction between the first element and the second element, the energy given off by the exothermic reaction acting to locally melt together the first and second layers.

Claims (30)

1. A method of fabricating a part by selectively melting powder, the method comprising reiterating following steps until the part is obtained:

depositing a first layer of a first powder having a first element as a main element of the first powder by moving a bottom wall of a first tank containing the first powder upward so that a predetermined amount of the first powder is situated above a horizontal plane at a top of the first tank, and then moving a first wiper or a first roller to move the first powder into a vessel, the first layer of the first powder having a constant predetermined thickness;

lowering a bottom wall of the vessel;

depositing a second layer of a second powder having a second element as a main element of the second powder on top of the first layer of the first powder by moving a bottom wall of a second tank containing the second powder upward so that a predetermined amount of the second powder is situated above the horizontal plane, and then moving a second wiper or a second roller to move the second powder into the vessel, the second layer of the second powder having a constant predetermined thickness, wherein the second element is different from the first element; and

moving an energy beam over a determined zone of the second layer of the second powder, energy delivered by the energy beam being less than energy required for locally melting of the second layer of the second powder and serving to initiate an exothermic reaction between the first element and the second element, in which energy given off by the exothermic reaction acts to locally melt together the first layer of the first powder and the second layer of the second powder so as to form a layer of material of the part,

wherein the vessel is disposed between the first tank and the second tank.

2. The method according to claim 1 , wherein:

the first element is selected from the following elements: Nb, Mo, V, Ta, Cr, Fe, Co, Ni;

the second element is selected from the following elements: Si or Al; and

the exothermic reaction takes place between the first element and Si or Al, and causes silicides or aluminides to be formed.

3. The method according to claim 1 , wherein the first element is Nb or Mo.

4. The method according to claim 1 , wherein the second element is Si.

5. The method according to claim 1 , wherein:

the first element is Ti;

the second element is selected from the following elements: Si or Al; and

the exothermic reaction takes place between the first element and Si or Al, and causes silicides or aluminides to be formed.

6. The method according to claim 5 , wherein the second element is Al.

7. The method according to claim 1 , wherein the method is applied to fabricating a metal part that is to be subjected to operating temperatures lying in the range 600° C. to 1500° C. or higher than 1500° C.

8. The method according to claim 1 , wherein the method is applied to fabricating a turbomachine part.

9. The method according to claim 1 , wherein the energy beam is a laser beam or an electron beam.

10. The method according to claim 1 , further comprising, prior to the depositing the second layer of the second powder on the first layer of the first powder, moving the energy beam over the first layer of the first powder to locally and superficially melt the first layer of the first powder so as to form a skin at a surface of the first layer of the first powder.

11. The method according to claim 10 , wherein the energy beam is a laser beam or an electron beam.

12. The method of claim 1 , wherein a melting temperature of the second powder is lower than a melting temperature of the first powder.

13. A method of fabricating a part by selectively melting powder, the method comprising reiterating following steps until the part is obtained:

depositing a first layer of a first powder having a first element as a main element of the first powder by moving a bottom wall of a first tank containing the first powder upward so that a predetermined amount of the first powder is situated above a horizontal plane at a top of the first tank, and then moving a first wiper or a first roller to move the first powder into a vessel, the first layer of the first powder having a constant predetermined thickness;

lowering a bottom wall of the vessel;

depositing a second layer of a second powder having a second element as a main element of the second powder on top of the first layer of the first powder by moving a bottom wall of a second tank containing the second powder upward so that a predetermined amount of the second powder is situated above the horizontal plane, and then moving a second wiper or a second roller to move the second powder into the vessel, the second layer of the second powder having a constant predetermined thickness, wherein the second element is different from the first element; and

moving an energy beam over a determined zone of the second layer of the second powder, energy delivered by the energy beam being able to melt the second layer of the second powder, and the energy delivered by the energy beam serving to initiate an exothermic reaction between the first element and the second element, in which energy given off by the exothermic reaction acts to locally melt together the first layer of the first powder and the second layer of the second powder so as to form a layer of material of the part,

wherein the vessel is disposed between the first tank and the second tank.

14. The method of claim 13 , wherein a melting temperature of the second powder is lower than a melting temperature of the first powder.

Assignments (3)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 28, 2016
From: KNITTEL, STEPHANE; BILHE, PASCAL FABRICE
To: SNECMA
Reel/Frame 039879/0327 →
Priority Claims (1)
FR 1362253 · Dec 6, 2013 · national
Continuity (1)
Related Publication 20160305256A1 · Oct 20, 2016
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