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Modified atmosphere melt infiltration
A ceramic matrix composite component for use in a gas turbine engine and method for making the same are described herein. The component includes a body and an outer region. The body includes a silicon containing ceramic composite. The outer region is on an outer surface of the body.
Modified atmosphere melt infiltration
A ceramic matrix composite component for use in a gas turbine engine and method for making the same are described herein. The component includes a body and an outer region. The body includes a silicon containing ceramic composite. The outer region is on an outer surface of the body.
Modified atmosphere melt infiltration
HARRIS STEPHEN I (author) / SHINAVSKI ROBERT J (author) / KIDD RICHARD W (author) / SHIM SUNGBO (author) / LEE KANG N (author)
2020-06-16
Patent
Electronic Resource
English