IP Library Granted Patent US 9,522,486
Granted Patent B2
US 9,522,486 · App. 14/379,884 · Granted Dec 20, 2016

Method of producing tooling for resin transfer molding

Inventors: Emilie Lesizza (Courbevoie, FR); Dominique Magnaudeix (Yerres, FR)
Assignee: SNECMA
B29C33/38B29C33/3807B29C33/3842B29C33/40B29C70/443B29C67/0051B29K2307/04B29L2031/08B29L2031/757Y10T156/1028
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Quick Facts
Patent No.
US 9,522,486
App. No.
14/379,884
Granted
Dec 20, 2016
Kind
B2
Abstract

A method of producing tooling for molding a part by resin transfer molding, including: producing a model of the part; producing a countermold with an outside surface presenting an indentation complementary to a first side of the model; placing the model in the indentation of the countermold; draping a plurality of superposed textile layers that are impregnated with thermosetting resin on the model and on the outside surface of the countermold to shape a first half-shell; curing the first half-shell; separating the countermold from the model and from the first half-shell; draping a plurality of superposed textile layers on the first half-shell and the first side of the model, to shape a second half-shell; and curing the second half-shell.

Claims (18)

1. A method of producing tooling for molding a part by resin transfer molding, the method comprising:

producing a model of the part;

producing a countermold with an outside surface presenting an indentation complementary to a first side of the model;

placing the model in the indentation of the countermold;

draping a plurality of superposed textile layers that are impregnated with thermosetting resin on the model and on the outside surface of the countermold to shape a first half-shell;

curing the first half-shell;

separating the countermold from the model and from the first half-shell;

draping a plurality of superposed textile layers on the first half-shell and the first side of the model, to shape a second half-shell; and

curing the second half-shell.

2. A method according to claim 1 , wherein each half-shell presents at least one orifice in alignment with a corresponding orifice in the other half-shell for passing a device for clamping the first half-shell against the second half-shell.

3. A method according to claim 2 , wherein the model is produced by a rapid prototyping method.

4. A method according to claim 1 , further comprising:

casting a hardenable fluid material into concave rear faces of the first and second half-shells; and

hardening the hardenable fluid material in the concave rear faces.

5. A method according to claim 4 , wherein the hardenable fluid material includes thermally conductive particles.

6. A method according to claim 4 , wherein the hardenable fluid material is concrete.

7. A method according to claim 1 , wherein the textile layers comprise carbon fibers.

8. A method according to claim 1 , wherein the textile layers are impregnated with thermosetting resin before draping.

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 Aug 20, 2014
From: LESIZZA, EMILIE; MAGNAUDEIX, DOMINIQUE
To: SNECMA
Reel/Frame 033572/0838 →
Priority Claims (1)
FR 12 51652 · Feb 23, 2012 · national
Continuity (1)
Related Publication 20150020958A1 · Jan 22, 2015