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公开(公告)号:US11161792B2
公开(公告)日:2021-11-02
申请号:US16508562
申请日:2019-07-11
Applicant: Rolls-Royce High Temperature Composites Inc.
Inventor: Thomas E. Krause , Robert Shinavski , Kevin Mark Lukhard
Abstract: A method for infiltrating a porous preform for a gas turbine engine is provided, which comprises providing a chamber for infiltrating a porous preform. The porous preform is positioned within a slurry confinement fixture within the chamber. A vacuum is created in the chamber. A solvent is added to the slurry confinement fixture until a pressure in the chamber is substantially equal to an equilibrium partial pressure of the solvent. A slurry is added to the slurry confinement fixture. The slurry includes the solvent and a particulate. The pressure in the chamber is increased, and the slurry is urged into the porous preform.
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公开(公告)号:US20210009479A1
公开(公告)日:2021-01-14
申请号:US16508562
申请日:2019-07-11
Applicant: Rolls-Royce High Temperature Composites Inc.
Inventor: Thomas E. Krause , Robert Shinavski , Kevin Mark Lukhard
Abstract: A method for infiltrating a porous preform for a gas turbine engine is provided, which comprises providing a chamber for infiltrating a porous preform. The porous preform is positioned within a slurry confinement fixture within the chamber. A vacuum is created in the chamber. A solvent is added to the slurry confinement fixture until a pressure in the chamber is substantially equal to an equilibrium partial pressure of the solvent. A slurry is added to the slurry confinement fixture. The slurry includes the solvent and a particulate. The pressure in the chamber is increased, and the slurry is urged into the porous preform.
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