Method of using permeable membrane in the debulking of cmc prepreg material

Patent metadata

Field	Value
Publication number	US-12428349-B2
Application number	US-202217984579-A
Country	US
Kind code	B2
Filing date	Nov 10, 2022
Priority date	Nov 10, 2022
Publication date	Sep 30, 2025
Grant date	Sep 30, 2025

Abstract

A method used for forming ceramic matrix composite components includes several steps. The method comprises arranging a layup of a predetermined number of pre-impregnated ceramic plies on a layup too and a plurality of different stages to debulk and consolidate the layup.

First claim

What is claimed is:

1. A method comprising
arranging a layup of prepreg ceramic plies on a layup tool,
overlaying a bleeder membrane over an exposed surface of the layup of prepreg ceramic plies,
overlaying a disposable thick breather layer over the bleeder membrane,
overlaying a reusable thick breather layer over the disposable thick breather layer,
overlaying a vacuum stretch bag over the reusable thick breather layer,
sealing the edges of the vacuum stretch bag to the layup tool,
infiltrating the layup with a matrix material,
applying a vacuum pressure to withdraw air between the vacuum stretch bag and the layup to bleed excess matrix material over an entire surface of the layup to compact the layup thereby minimizing bulk of the layup,
wherein the disposable and reusable thick breather layers are configured to absorb excess matrix material and the bleeder membrane is configured to enable the matrix material to escape from the surface of the layup as the vacuum pressure is applied so that the excess matrix material is uniformly bled in a thickness direction from the layup to provide a homogenous distribution of the matrix material,
removing the vacuum stretch bag, the disposable thick breather layer, the reusable thick breather layer, and the bleeder membrane from the layup after applying the vacuum pressure,
overlaying a second bleeder membrane over an exposed surface of the layup of prepreg ceramic plies after removing the vacuum stretch bag, the disposable thick breather layer, the reusable thick breather layer, and the bleeder membrane from the layup,
overlaying a plurality of thin breather layers over the second bleeder membrane,
overlaying the reusable thick breather layer over the plurality of thin breather layers,
overlaying the vacuum stretch bag over the reusable thick breather layer,
sealing the edges of the vacuum stretch bag to the layup tool,
infiltrating the layup with the matrix material, and
applying the vacuum pressure to withdraw air between the vacuum stretch bag and the layup to bleed excess matrix material over the entire surface of the layup to compact the layup thereby minimizing bulk of the layup.

2. The method of claim 1 , wherein the bleeder membrane is an E-glass fiber cloth.

3. The method of claim 1 , wherein the bleeder membrane has a higher flexibility than the disposable and reusable thick breather layers.

4. The method of claim 1 , wherein the bleeder membrane has an excess length on all sides of the layup when the bleeder membrane is laid over the exposed surface of the layup of prepreg ceramic plies.

5. The method of claim 4 , wherein the excess length is about 20 millmeters.

6. The method of claim 1 , wherein bleeder membrane is free of a release agent so that the bleeder membrane maintains its flexibility.

7. A method comprising
arranging a layup of prepreg ceramic plies on a layup tool,
overlaying a first bleeder membrane over an exposed surface of the layup of prepreg ceramic plies,
overlaying a first thick breather layer over the first bleeder membrane,
overlaying a second thick breather layer over the first breather layer,
overlaying a vacuum stretch bag over the second breather layer,
sealing the edges of the vacuum stretch bag to the layup tool,
infiltrating the layup with a matrix material,
applying a vacuum pressure for a predetermined intermediate debulk period to withdraw air between the vacuum stretch bag and the layup to bleed excess matrix material over an entire surface of the layup,
removing the vacuum stretch bag, the first thick breather layer, the second thick breather layer, and the first bleeder membrane from the layup after applying the vacuum pressure,
adding a predetermined number of prepreg ceramic plies to the layup of prepreg ceramic plies after removing the vacuum stretch bag, the first thick breather layer, the second thick breather layer, and the first bleeder membrane from the layup,
overlaying a second bleeder membrane over an exposed surface of the layup of prepreg ceramic plies after adding the predetermined number of prepreg ceramic plies to the layup,
overlaying the first thick breather layer over the second bleeder membrane,
overlaying the second thick breather layer over the first thick breather layer,
overlaying the vacuum stretch bag over the second thick breather layer,
sealing the edges of the vacuum stretch bag to the layup tool,
infiltrating the layup with the matrix material,
applying the vacuum pressure for the predetermined intermediate debulk period to withdraw air between the vacuum stretch bag and the layup to bleed excess matrix material over the entire surface of the layup,
removing the vacuum stretch bag, the first thick breather layer, the second thick breather layer, and the second bleeder membrane from the layup after applying the vacuum pressure,
overlaying a third bleeder membrane over the exposed surface of the layup of prepreg ceramic plies after removing the vacuum stretch bag, the first thick breather layer, the second breather layer, and the second bleeder membrane from the layup,
overlaying a plurality of thin breather layers over the third bleeder membrane,
overlaying the reusable thick breather layer over the plurality of thin breather layers,
overlaying the vacuum stretch bag over the reusable thick breather layer,
sealing the edges of the vacuum stretch bag to the layup tool,
infiltrating the layup with the matrix material, and
applying the vacuum pressure for a predetermined extended debulk period that is greater than the predetermined intermediate debulk period to withdraw air between the vacuum stretch bag and the layup to bleed excess matrix material over the entire surface of the layup.

8. The method of claim 7 , wherein the first bleeder membrane and the second bleeder membranes are each an E-glass fiber cloth.

9. The method of claim 7 , wherein the first bleeder membrane and the second bleeder membrane each have a higher flexibility than any one of the thick breather layers.

10. The method of claim 7 , wherein the first bleeder membrane and the second bleeder membrane are each free of a release agent so that the first bleeder membrane and the second bleeder membrane maintain their flexibility.

Assignees

• Rolls Royce Plc

Inventors

• Rubio Diaz Virtudes

Classifications

• C04B35/82

  Asbestos; Glass; Fused silica · CPC title

• B28B3/006

  Pressing by atmospheric pressure, as a result of vacuum generation or by gas or liquid pressure acting directly upon the material, e.g. jets of compressed air (moulds for treating with gases or degassing B28B7/44; compacting concrete by means of vacuum in general E04G21/061) · CPC title

• C04B2235/604

  Pressing at temperatures other than sintering temperatures · CPC title

• B28B19/0015

  on multilayered articles · CPC title

• B29C70/76

  Moulding on edges or extremities of the preformed part · CPC title