IP Library Granted Patent US 10,183,450
Granted Patent B2
US 10,183,450 · App. 15/100,551 · Granted Jan 22, 2019

Method for impregnation of a fibrous preform and device for implementation of the said method

Inventors: Philippe Henrio (Lisses, FR); Thierry Godon (Sevran, FR)
Assignees: SAFRAN AIRCRAFT ENGINES; SAFRAN
B29C70/443B29C43/10B30B1/003B29C2043/3238B29C2043/3652B29L2031/082
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 10,183,450
App. No.
15/100,551
Granted
Jan 22, 2019
Kind
B2
Abstract

A method of impregnating a fiber preform with an impregnation composition, includes applying a liquid on a structure, the structure including a chamber in which a fiber preform for impregnating is present, the chamber being defined between a rigid support on which the fiber preform is placed and a wall, the wall having a face situated facing the fiber preform; and an impregnation composition for impregnating the fiber preform, the impregnation composition being present in the chamber; the liquid being applied against the wall on its side opposite from the chamber, the wall being configured so that its face situated facing the fiber preform conserves its shape during the application of the liquid, the applied liquid enabling sufficient pressure to be created to move the wall towards the rigid support and impregnate the fiber preform with the impregnation composition.

Claims (19)

1. A method of impregnating a fiber preform with an impregnation composition, the method comprising:

a) applying a liquid on a structure, the structure comprising:

a chamber in which a fiber preform for impregnating is present, the chamber being defined between a rigid support on which the fiber preform is placed and a wall, the wall having a face situated facing the fiber preform; and

an impregnation composition, for impregnating the fiber preform, the impregnation composition being present in the chamber;

the liquid being applied against the wall on its side opposite from the chamber, the wall being sufficient rigid so that its face situated facing the fiber preform conserves its shape and avoid being deformed during the application of the liquid, the applied liquid enabling sufficient pressure to be created to move the wall towards the rigid support and impregnate the fiber preform with the impregnation composition.

2. A method according to claim 1 , wherein, prior to step a), the method further comprises injecting the impregnation composition into the chamber.

3. A method according to claim 2 , wherein the impregnation composition is injected into the chamber after placing the fiber preform on the support, and wherein the impregnation composition is injected between the fiber preform and the wall.

4. A method according to claim 1 , wherein, prior to applying the liquid, the impregnation composition is superposed on the fiber preform over at least half of a length of the fiber preform.

5. A method according to claim 1 , wherein the structure also includes an impermeable membrane covering the wall, and wherein the wall is situated between the chamber and the impermeable membrane, and wherein the liquid is applied against the impermeable membrane on its side opposite from the chamber.

6. A method of fabricating a part comprising a fiber preform densified by a matrix, the method comprising:

b) densifying a fiber preform that has been impregnated by an impregnation composition that is a densification matrix precursor in order to obtain a part comprising a fiber preform densified by a matrix, the impregnated preform being obtained by performing a method according to claim 1 .

7. A method according to claim 6 , wherein the densification is performed while maintaining the pressure exerted by the wall on the impregnated preform as a result of the application of the liquid.

8. A method according to claim 6 , wherein the part constitutes a turbine engine blade.

9. A device for performing a method according to claim 1 , the device comprising:

a structure including a chamber defined between a rigid support and a wall, the wall having a face situated facing the rigid support, the chamber defining an internal volume in which a fiber preform impregnated by a matrix precursor impregnation composition is to be present, the chamber being configured to be subjected to heat treatment for the purpose of densifying the fiber preform; and

a liquid injection device configured to apply a liquid against the wall on its side opposite from the chamber;

the device being configured so that the application of the liquid against the wall on its side opposite from the chamber does not change the shape of the face of the wall situated facing the rigid support and generates sufficient pressure on the wall to move it towards the support and reduce the internal volume of the chamber.

10. A device according to claim 9 , wherein the structure further includes an impermeable membrane covering the wall, and wherein the wall is situated between the chamber and the impermeable membrane, and wherein the liquid injection device is configured to apply the liquid against the impermeable membrane on its side opposite from the chamber.

11. A device according to claim 9 , further comprising a heater member configured to perform heat treatment on the impregnation composition enabling the fiber preform to be densified.

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 May 31, 2016
From: HENRIO, PHILIPPE; GODON, THIERRY
To: SNECMA; SAFRAN
Reel/Frame 038753/0096 →
Priority Claims (1)
FR 13 62102 · Dec 4, 2013 · national
Continuity (1)
Related Publication 20160297153A1 · Oct 13, 2016
Cited By (2)
US 12,370,759 US 12,629,869