IP Library Granted Patent US 10,710,156
Granted Patent B2
US 10,710,156 · App. 14/902,699 · Granted Jul 14, 2020

Process for additive manufacturing of parts by melting or sintering particles of powder(s) using a high-energy beam with powders adapted to the targeted process/material pair

Inventors: Christophe Colin (Evry, FR); Laetitia Kirschner (Paris, FR)
Assignees: SAFRAN AIRCRAFT ENGINES; EUROPEAN AERONAUTIC DEFENCE AND SPACE COMPANY EADS FRANCE; AIRBUS HELICOPTERS
B22F1/0048B22F1/0014B22F3/1055B23K26/342B28B1/001C04B35/62839C04B35/71C22C1/0491B22F1/0096B22F9/04B22F9/082B22F2003/1056B22F2009/041B33Y10/00B33Y70/00C04B2235/5296C04B2235/5463C04B2235/5481C04B2235/665C22C33/0207C22C33/0257Y02P10/295
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Quick Facts
Patent No.
US 10,710,156
App. No.
14/902,699
Granted
Jul 14, 2020
Kind
B2
Abstract

A method of fabricating parts out of metallic, intermetallic, ceramic, ceramic matrix composite, or metal matrix composite material with discontinuous reinforcement, includes melting or sintering powder particles by means of a high-energy beam. The powder used is a single powder of particles that present sphericity lying in the range 0.8 to 1.0 and of form factor lying in the range 1 to √2, each powder particle presenting substantially identical mean composition, and the grain size distribution of the particles of the powder is narrowed around the mean diameter value d50% in such a manner that: (d90%−d50%)/d50%≤0.66; and (d50%−d10%)/d50%≤0.33; with a “span”: (d90%−d10%)/d50%≤1.00.

Claims (48)

1. A method of fabricating a part out of a material with discontinuous reinforcement, the method comprising:

melting or sintering powder particles of the material with discontinuous reinforcement via a high-energy beam,

wherein

the material is a metallic, intermetallic, ceramic, ceramic matrix composite, or a metal matrix composite material,

the powder particles have substantially identical mean composition, a sphericity of from 0.8 to 1.0, a form factor of from 1 to √2, and a grain size distribution narrowed around a mean diameter value d 50% in such a manner that:

( d 90% −d 50% )/ d 50% ≤0.66,

( d 50% −d 10% )/ d 50% ≤0.33, and

( d 90% −d 10% )/ d 50% ≤1.00,

the composition of the powder particles comprises an additional chemical element in a quantity of more than 0 and less than 0.5 wt % and suitable for modifying the material's microstructure,

and

the additional chemical element facilitates wetting of the reinforcement by a liquid, which is formed by melting a portion of the powder particles via the high-energy beam.

2. The method according to claim 1 ,

wherein a span value defined as:

( d 90% −d 10% )/ d 50%

is less than or equal to 0.50, with:

( d 90% −d 50% )/ d 50% ≤0.33, and

( d 50% −d 10% )/ d 50% ≤0.17.

3. The method according to claim 1 ,

wherein the powder particles are obtained by atomizing or centrifuging a parent alloy.

4. The method according to claim 1 ,

wherein the powder particles are obtained by coating or by encrustation.

5. The method according to claim 1 ,

wherein the powder particles are obtained by milling/mixing.

6. The method according to claim 1 ,

wherein the powder particles are obtained by granulating a suspension.

7. The method according to claim 1 ,

wherein the composition of the powder particles is enriched in at least one chemical element, which is a chemical element of the material.

8. The method according to claim 7 ,

wherein the at least one chemical element, or an oxide of the at least one chemical element, is volatile at a temperature produced by the high-energy beam.

9. The method according to claim 8 ,

wherein the material is a Ti6Al4V metal alloy and the volatile chemical element is aluminum.

10. The method according to claim 9 ,

wherein an enriched content of aluminum from the powder particles ranges from 0.15 wt % to 3 wt % relative to the Ti6Al4V alloy.

11. The method according to claim 8 , wherein the material is a metal alloy based on aluminum or on lithium, and the volatile chemical element is lithium.

12. The method according to claim 1 ,

wherein the high-energy beam is a laser beam.

13. The method according to claim 12 ,

wherein the melting or sintering comprises applying a direct metal deposition technique, a selective laser melting technique, or a selective laser sintering technique to a powder bed.

14. A method of fabricating a part out of a material with discontinuous reinforcement, the method comprising:

melting or sintering powder particles via a high-energy beam,

wherein

the material is a metallic, intermetallic, ceramic, ceramic matrix composite, or a metal matrix composite material,

the powder particles have substantially identical mean composition, a sphericity of from 0.8 to 1.0, a form factor of from 1 to √2, and a grain size distribution narrowed around a mean diameter value d 50% in such a manner that:

( d 90% −d 50% )/ d 50% ≤0.66,

( d 50% −d 10% )/ d 50% ≤0.33, and

( d 90% −d 10% )/ d 50% ≤1.00,

the composition of the powder particles comprises an additional chemical element in a quantity of more than 0 and less than 0.5 w % and suitable for modifying the material's microstructure, and

when the material is a ceramic material, the additional chemical element is suitable for improving the ceramic material's absorptivity of a radiation emitted by the high-energy beam.

Assignments (6)
MERGER Recorded Nov 4, 2021
From: AIRBUS GROUP SAS
To: AIRBUS
Reel/Frame 058021/0445 →
CHANGE OF NAME Recorded Nov 4, 2021
From: EUROPEAN AERONAUTIC DEFENCE AND SPACE COMPANY EADS FRANCE
To: AIRBUS GROUP SAS
Reel/Frame 058029/0266 →
CONFIRMATORY ASSIGNMENT Recorded Nov 4, 2021
From: AIRBUS; AIRBUS HELICOPTERS
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 058029/0638 →
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 Mar 1, 2016
From: COLIN, CHRISTOPHE; KIRSCHNER, LAETITIA
To: SNECMA; EUROPEAN AERONAUTIC DEFENCE AND SPACE COMPANY EADS FRANCE; AIRBUS HELICOPTERS
Reel/Frame 037857/0912 →
Priority Claims (1)
FR 13 01591 · Jul 4, 2013 · national
Continuity (1)
Related Publication 20160175929A1 · Jun 23, 2016
Cited By (2)
US 12,186,810 US 12,611,711