IP Library Granted Patent US 9,316,120
Granted Patent B2
US 9,316,120 · App. 14/232,514 · Granted Apr 19, 2016

Method for manufacturing a turbine-engine fan casing having an acoustic coating

Inventors: Benedicte Marie Le Borgne (Paris, FR); Erwan Camus (Melun, FR); Julien Schneider (Corbeil-Essonnes, FR)
Assignee: SNECMA
F01D25/24B29C70/088B29C70/48B29C70/86F01D11/122F02C7/045B29B11/16B29C70/462F05D2260/96F05D2300/44F05D2300/603F05D2300/614F05D2300/701F05D2300/702Y02T50/672Y10T29/49327
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Quick Facts
Patent No.
US 9,316,120
App. No.
14/232,514
Granted
Apr 19, 2016
Kind
B2
Abstract

A method for manufacturing a turbine engine fan casing includes placing a fiber structure constituting the fiber reinforcement of a composite material inside skin of an acoustic coating on a tooling element, and then shaping the fiber preform constituting the fiber reinforcement of an abradable casing on the tooling element with cellular structures of acoustic coating and abradable coating cartridges, if any, being interposed. Both the fiber preform of the casing as impregnated by a precursor resin for the matrix of the composite material of the casing, and also the fiber structure of the inside skin of the acoustic coating as impregnated with a precursor resin for the matrix of the composite material of the inside skin are subjected to resin polymerizing heat treatment, and the inside skin of the acoustic coating is multiply perforated so an assembly is obtained that comprises the casing with an incorporated acoustic coating.

Claims (15)

1. A method for manufacturing a turbine engine fan casing having an abradable coating on its inside face extending over a fraction of its axial dimension at a distance from upstream and downstream ends of the casing, and an acoustic coating arranged downstream and/or upstream of the abradable coating, the inside surfaces of the abradable coating and of the acoustic coating defining at least a portion of the wall of an air inlet passage, the casing being made of composite material comprising fiber reinforcement densified by a resin precursor matrix, the method comprising:

using a tooling element having a profile corresponding to the profile of the air inlet passage;

depositing a fiber structure that is to constitute fiber reinforcement of a composite material inside skin of the acoustic coating on the tooling element at a location corresponding to the location of the acoustic coating;

placing cellular structures of the acoustic coating in the form of sectors over said fiber structure;

shaping a fiber preform that is to constitute the fiber reinforcement of the casing on the tooling element with cellular structures of the acoustic coating being interposed between them;

subjecting both the fiber preform of the casing as held in its shape and impregnated with a precursor resin for the matrix of the composite material of the casing and also the fiber structure of the inside skin of the acoustic coating as impregnated with a precursor resin for the matrix of the composite material of said inside skin to common resin polymerizing heat treatment; and

multiply perforating the inside skin of the acoustic coating after the precursor resin for the matrix of the composite material of said inside skin has polymerized;

whereby an assembly is obtained that comprises the casing assembled together with an incorporated acoustic coating comprising said cellular structures and said multiply perforated inside skin.

2. The method according to claim 1 , wherein the fiber preform that is to constitute the fiber reinforcement of the casing is shaped on the tooling element with elements constituting abradable coating cartridges being interposed, such that after polymerization an assembly is obtained comprising the casing with the abradable coating cartridges and the acoustic coating incorporated therein.

3. The method according to claim 2 , wherein a layer of adhesive is interposed between firstly the fiber preform of the casing and secondly the cellular structures of the acoustic coating and also the abradable coating cartridges.

4. The method according to claim 2 , wherein an electrical isolation fiber layer is interposed between firstly the fiber preform of the casing and secondly the cellular structures of the acoustic coating and also the abradable coating cartridges.

5. The method according to claim 1 , wherein an adhesive coating is interposed between the fiber structure that is to constitute the fiber reinforcement of the inside skin of the acoustic coating and the cellular structures of the acoustic coating.

6. The method according to claim 1 , wherein the fiber preform forming the fiber reinforcement of the casing and the fiber structure forming the fiber reinforcement of the inside skin of the acoustic coating are both formed of fiber textures that are preimpregnated with resin.

7. The method according to claim 1 , wherein the fiber preform that is to form the fiber reinforcement of the casing is impregnated with resin after the fiber preform has been shaped.

8. The method according to claim 1 , wherein the fiber preform that is to form the fiber reinforcement of the casing and the fiber structure that is to form the fiber reinforcement of the inside skin of the acoustic coating are both impregnated with resin after the fiber preform has been shaped.

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 Jan 13, 2014
From: LE BORGNE, BENEDICTE MARIE; CAMUS, ERWAN; SCHNEIDER, JULIEN
To: SNECMA
Reel/Frame 031954/0212 →
Priority Claims (1)
FR 11 56446 · Jul 13, 2011 · national
Continuity (1)
Related Publication 20140150262A1 · Jun 5, 2014