IP Library Granted Patent US 12,168,255
Granted Patent B2
US 12,168,255 · App. 17/040,255 · Granted Dec 17, 2024

Optimization of supports for the additive manufacturing of a component

Inventors: Nicolas Ovaere (Moissy-Cramayel, FR); Jacques Marcel Arthur Bunel (Moissy-Cramayel, FR); Thomas Gricourt (Moissy-Cramayel, FR); Paul André Somazzi (Moissy-Cramayel, FR); Sylvain Zambelli (Moissy-Cramayel, FR)
Assignee: SAFRAN AIRCRAFT ENGINES
B22F10/00B22F5/009B22F10/47B29C64/40B33Y10/00B33Y80/00F01D25/162B22F10/28B22F10/66F05D2240/50
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Quick Facts
Patent No.
US 12,168,255
App. No.
17/040,255
Granted
Dec 17, 2024
Kind
B2
Abstract

A method for producing, by additive manufacturing, a part including at least one surface that must be held during the manufacturing, the method including: a step of forming a raw part by additive manufacturing, the raw part including a support including a pillar and a head which is an alveolar element connecting the pillar to the surface to be held; and a step of detaching the support from the rest of the raw part.

Claims (23)

1. A method for: obtaining, by additive manufacturing, a component including at least one surface that has to be supported during manufacture, including:

a step of forming by additive manufacturing a one-piece blank component on a build plate comprising a support including:

a pillar comprising a foot from which the manufacture of this pillar starts,

wherein the foot is perpendicular to the plate,

the pillar being a block of material, and

wherein the pillar further comprises,

an inclined segment defining an acute angle with the build plate,

a head formed at a distal end of the inclined segment, wherein said head widens to form a support base corresponding along a longitudinal axis to the at least one surface to be supported, and

a cap formed on the support base, said cap comprising a cellular element connecting the pillar to the surface to be supported;

a step of detaching the support from the rest of the blank component comprising pulling on the foot in the manner of a lever by following an arc path.

2. The method according to claim 1 , wherein the step of detaching the support includes:

the removal of the pillar inducing a rupture at the cap, and

a finishing step to suppress residues from the cap remained attached to the surface to be supported.

3. The method according to claim 1 , wherein the foot is directly erected from the build plate from which the component starts the manufacture thereof.

4. The method according to claim 1 , wherein the component is a bearing support comprising at least one surface supported during the additive manufacturing thereof.

5. The method according to claim 1 , wherein the cap is formed on the head.

6. A method for producing a component on a build plate via additive manufacturing, said component defining an opening and at least one surface to be supported above said opening, the method comprising:

forming a pillar on said build plate, said pillar comprising a foot from which the manufacture of this pillar starts, wherein the foot is perpendicular to the build plate, said pillar further comprising an inclined segment defining an acute angle with said build plate and extending into said opening;

forming a head at a distal end of the inclined segment, wherein said head widens to form a support base corresponding along a longitudinal axis to the at least one surface to be supported, and

forming a cap on said support base, said cap connecting the at least one surface to be supported to said pillar and comprising a mechanical resistance that is lower than a mechanical resistance of said pillar.

7. The method of claim 6 , further comprising detaching the pillar from the component by pulling on the pillar.

8. The method according to claim 1 , wherein the head forms with the build plate at an angle greater than 40°.

9. The method according to claim 6 , wherein the head forms with the build plate at an angle greater than 40°.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 22, 2020
From: OVAERE, NICOLAS; BUNEL, JACQUES MARCEL ARTHUR; GRICOURT, THOMAS; SOMAZZI, PAUL ANDRÉ; ZAMBELLI, SYLVAIN
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 053846/0421 →
Priority Claims (1)
FR 1852559 · Mar 23, 2018 · national
Continuity (1)
Related Publication 20210008624A1 · Jan 14, 2021