IP Library Granted Patent US 9,555,566
Granted Patent B2
US 9,555,566 · App. 13/936,691 · Granted Jan 31, 2017

Composite material part having thermal protection based on resin, and its method of fabrication

Inventors: Lea Gani (Paris, FR); Benedicte Marie Le Borgne (Paris, FR); Gilbert Michel Marin Leconte (Ozoir la Ferriere, FR)
Assignee: SNECMA
B29C45/0003B29C45/1639B29C45/1671B29C70/086B29C70/462B29C70/48B29C70/68B29C70/70B29K2105/12B29K2995/0015B29L2023/00B29L2031/3082
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Quick Facts
Patent No.
US 9,555,566
App. No.
13/936,691
Granted
Jan 31, 2017
Kind
B2
Abstract

A method of making a structural part having a thermal protection barrier is provided. The method includes: making a fiber structure; introducing the fiber structure into an injection mold having first and second chambers, the fiber structure being placed in the second chamber; placing a movable separator partition between the first and second chambers; injecting a first resin into the first chamber; solidifying the resin injected into the first chamber; withdrawing the movable separator partition; injecting a second resin into the second chamber containing the fiber texture; and hardening the resins present in the first and second chambers of the injection mold in such a manner as to obtain a part having a structural core made of composite material constituted by fiber reinforcement densified by an organic matrix, and a thermal barrier constituted by a layer of hardened resin.

Claims (37)

1. A method of making a structural part having a thermal protection barrier, the method comprising at least the following steps:

making a fiber structure;

introducing the fiber structure into an injection mold having first and second chambers, the fiber structure being placed in the second chamber;

placing a movable separator partition between the first and second chambers;

injecting a first resin into the first chamber;

solidifying the resin injected into the first chamber;

withdrawing the movable separator partition;

injecting a second resin into the second chamber containing the fiber structure; and

hardening the resins present in the first and second chambers of the injection mold in such a manner as to obtain the structural part having a structural core made of composite material constituted by fiber reinforcement densified by an organic matrix, and a thermal barrier constituted by a layer of hardened resin,

wherein the injection mold includes a mandrel, the movable separator, and a stationary wall arranged coaxially, the first chamber being defined between an outside surface of the movable separator and an inside surface of the stationary wall, and the second chamber being defined between an outside surface of the mandrel and an inside surface of the movable separator such that the first chamber and second chamber are coaxial and the first chamber surrounds the second chamber.

2. A method according to claim 1 , wherein the first resin is a thermosetting resin or a thermoplastic resin, and the second resin is a thermosetting resin or a thermoplastic resin.

3. A method according to claim 2 , wherein the first and second resins are identical.

4. A method according to claim 2 , wherein the first and second resins are different.

5. A method according to claim 4 , wherein the first resin presents a glass transition or melting temperature higher than a glass transition or melting temperature of the second resin.

6. A method according to claim 5 , wherein the glass transition temperature of the first resin is higher than a determined temperature corresponding to a maximum utilization temperature of the structural part.

7. A method of making a structural part having a thermal protection barrier, the method comprising at least the following steps:

making a fiber structure;

introducing the fiber structure into an injection mold having first and second chambers, the fiber structure being placed in the second chamber;

placing a movable separator partition between the first and second chambers;

injecting a first resin into the first chamber;

solidifying the resin injected into the first chamber;

withdrawing the movable separator partition;

injecting a second resin into the second chamber containing the fiber structure; and

hardening the resins present in the first and second chambers of the injection mold in such a manner as to obtain the structural part having a structural core made of composite material constituted by fiber reinforcement densified by an organic matrix, and a thermal barrier constituted by a layer of hardened resin,

wherein the injection mold includes a mandrel, the movable separator, and a stationary wall arranged coaxially, the first chamber being defined between an outside surface of the movable separator and an inside surface of the stationary wall, and the second chamber being defined between an outside surface of the mandrel and an inside surface of the movable separator such that the first chamber and second chamber are coaxial and the first chamber surrounds the second chamber, and

wherein the fiber structure is placed on the mandrel.

8. A method of making a structural part having a thermal protection barrier, the method comprising at least the following steps:

making a fiber structure;

introducing the fiber structure into an injection mold having first and second chambers, the fiber structure being placed in the second chamber;

placing a movable separator partition between the first and second chambers;

injecting a first resin into the first chamber,

solidifying the resin injected into the first chamber;

withdrawing the movable separator partition;

injecting a second resin into the second chamber containing the fiber structure; and

hardening the resins present in the first and second chambers of the injection mold in such a manner as to obtain the structural part having a structural core made of composite material constituted by fiber reinforcement densified by an organic matrix, and a thermal barrier constituted by a layer of hardened resin,

wherein the injection mold includes a mandrel, the movable separator, and a stationary wall arranged coaxially, the first chamber being defined between an outside surface of the movable separator and an inside surface of the stationary wall, and the second chamber being defined between an outside surface of the mandrel and an inside surface of the movable separator such that the first chamber and second chamber are coaxial and the first chamber surrounds the second chamber, and

wherein the mandrel, the movable separator, the stationary wall, and the structural part are each cylindrical in shape.

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 5, 2013
From: GANI, LEA; LE BORGNE, BENEDICTE MARIE; LECONTE, GILBERT MICHEL MARIN
To: SNECMA
Reel/Frame 030942/0621 →
Priority Claims (1)
FR 12 56583 · Jul 9, 2012 · national
Continuity (1)
Related Publication 20140008838A1 · Jan 9, 2014