IP Library Granted Patent US 9,452,562
Granted Patent B2
US 9,452,562 · App. 14/352,856 · Granted Sep 27, 2016

Impregnation clamping mandrel for making gas turbine casings made of composite material

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Quick Facts
Patent No.
US 9,452,562
App. No.
14/352,856
Granted
Sep 27, 2016
Kind
B2
Abstract

An impregnation mandrel for production of gas turbine casings made from composite material, the mandrel including: an annular wall with a profile of an outer surface that corresponds to that of an internal surface of the casing to be produced; two side plates, with profiles that correspond to those of external casing flanges to be produced; and a removable device for clamping a layer having a fibrous texture, which is wound around the mandrel.

Claims (21)

1. An impregnation mandrel for making a gas turbine casing made of composite material, the mandrel comprising:

an annular wall with a profile of an external surface that corresponds to that of an internal surface of the casing to be made;

two lateral flanges with profiles that correspond to those of external flanges of the casing to be made; and

a removable clamping device to clamp a layer of fibrous texture wound on the mandrel between two surfaces of the removable clamping device, the removable clamping device including;

a removable plate configured to be positioned in a corresponding recess made through the annular wall of the mandrel.

2. The mandrel according to claim 1 , wherein the removable plate of the removable clamping device comprises an external surface with a profile capable of reconstituting a profile of an external surface of the mandrel and a slot extending in position between the lateral flanges of the mandrel and configured to receive a free end of the layer of fibrous texture wound on the mandrel.

3. The mandrel according to claim 2 , wherein the removable clamping device further comprises a pad configured to exert a clamping force on the free end of the layer of fibrous texture wound on the mandrel by tightening screws.

4. The mandrel according to claim 3 , wherein the tightening screws are accessible from an interior of the mandrel.

5. The mandrel according to claim 2 , wherein the removable plate of the removable clamping device comprises fixing flanges which when in position are configured to be fixed on the annular wall of the mandrel by fixing screws.

6. The mandrel according to claim 2 , wherein the removable plate of the removable clamping device comprises a grip accessible from an interior of the mandrel when the removable plate is in position.

7. A winding machine of a fibrous texture on an impregnation mandrel, comprising:

a take-up mandrel on which a fibrous texture produced by three-dimensional weaving is configured to be stored, the take-up mandrel having a substantially horizontal axis of rotation;

the impregnation mandrel according to claim 1 on which the fibrous texture stored on the take-up mandrel is configured to be wound in superposed layers, the impregnation mandrel having a substantially horizontal axis of rotation parallel to the axis of rotation of the take-up mandrel;

electric motors to drive the mandrels in rotation about their respective axis of rotation; and

a control unit of the electric motors to drive the mandrels in rotation.

8. An impregnation method of a fibrous texture for making gas turbine casings made of material composite, comprising:

winding a first layer of fibrous texture on the impregnation mandrel according to claim 1 ;

maintaining a free end of the first layer of fibrous texture on the impregnation mandrel by the removable clamping device;

winding other layers of fibrous texture on the impregnation mandrel;

withdrawing the removable clamping device and replacing the removable clamping device with a sealing plug; and

impregnating the fibrous texture wounded on the mandrel by resin injection.

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 Apr 18, 2014
From: MATHON, RICHARD; PATRIGEON, OLIVIER
To: SNECMA
Reel/Frame 032708/0782 →