IP Library Granted Patent US 8,424,921
Granted Patent B2
US 8,424,921 · App. 12/333,467 · Granted Apr 23, 2013

Composite coupling with a machining portion

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Quick Facts
Patent No.
US 8,424,921
App. No.
12/333,467
Granted
Apr 23, 2013
Kind
B2
Abstract

A coupling made of composite material including a polymer matrix reinforced by a fiber structure is disclosed. The coupling includes a structural portion reinforced by a main fiber structure, and a first machining portion reinforced by a first fiber structure that is distinct from the main fiber structure. The matrices of the structural portion and of the first machining portion are identical. The first machining portion is situated on at least a fraction of the main face of the structural portion and is machined in a first machining surface, and there is no intersection between the first machining surface and the fibers of the main fiber structure.

Claims (20)

1. A system comprising:

a coupling made of composite material comprising a polymer matrix reinforced by a fiber structure, said coupling comprising:

a structural layer reinforced by a main fiber structure; and

a first machining layer reinforced by a first fiber structure distinct from the main fiber structure; and

an adjacent part including a mating surface,

wherein matrices of said structural layer and of said first machining layer are identical,

wherein said first machining layer is situated on at least a fraction of a main face of said structural layer, and is machined so as to present a first machining exterior surface with fibers which have been cut,

wherein there is no intersection between said first machining exterior surface and fibers of said main fiber structure,

wherein the first machining exterior surface of the first machining layer is machined to correspond to the mating surface of the adjacent part, and

wherein the structural layer is not machined to correspond to the mating surface of the adjacent part.

2. The system according to claim 1 , wherein the coupling is annular.

3. The system according to claim 1 , wherein each of said first fiber structure and said main fiber structure is constituted by a preform selected from the group consisting of a woven preform and a braided preform.

4. The system according to claim 1 , wherein the coupling further comprises a second machining layer reinforced by a second fiber structure distinct from said main fiber structure and machined so as to present a second machining exterior surface with fibers which have been cut, there being no intersection between said second machining exterior surface and the fibers of said main fiber structure, the matrices of said structural layer and of said second machining layer being identical, said second machining layer being situated on at least a fraction of the face opposite said main face.

5. The system according to claim 4 , wherein each of said first fiber structure, said second fiber structure, and said main fiber structure is constituted by a preform selected from the group consisting of a woven preform and a braided preform.

6. The system according to claim 4 , further comprising a backing plate with a mating surface,

wherein the second machining exterior surface of the second machining layer is machined to correspond to the mating surface of the backing plate.

7. The system according to claim 1 , wherein the coupling further comprises an angled region, said first machining layer being situated on a convex face of said angled region.

8. The system according to claim 7 , wherein said angled region forms an angle lying in the range 90° to 180°.

9. The system according to claim 1 , wherein the coupling includes a cylindrical region, a radial region, and an angled region connecting said cylindrical and radial regions, wherein said first machining layer is situated on a fraction of said radial region, a fraction of said cylindrical region, and on a convex face of said angled region.

10. A turbomachine including a system according to claim 1 .

Assignments (2)
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 →