HIGH TEMPERATURE INTERFACES FOR CERAMIC COMPOSITES

    公开(公告)号:US20220348509A1

    公开(公告)日:2022-11-03

    申请号:US17302014

    申请日:2021-04-21

    Abstract: An article for a high temperature environment includes a first ceramic composite substrate, a second ceramic composite substrate, and a high temperature interface between a first surface of the first ceramic composite substrate and a second surface of the second ceramic composite substrate. The high temperature interface includes at least one high temperature interface layer that includes a ceramic matrix and a plurality of fibers distributed through the ceramic matrix.

    CORROSION AND OXIDATION RESISTANT COATINGS FOR GAS TURBINE ENGINES, AND METHODS FOR PRODUCING THE SAME

    公开(公告)号:US20220178263A1

    公开(公告)日:2022-06-09

    申请号:US17116426

    申请日:2020-12-09

    Abstract: Disclosed is a superalloy gas turbine engine component including a glass coating. The glass coating is configured for resistance to hot corrosion caused by molten salts of sodium, magnesium, vanadium, and/or sulfur dioxide. The glass coating includes a mixture of two or more metal oxides, which are preferably selected from: barium oxide, silicon oxide, strontium oxide, aluminum oxide, magnesium oxide, calcium oxide, cobalt oxide, boron oxide, iron oxide, zirconium oxide, nickel oxide, and titanium oxide. The glass coating is in fully crystalline form and/or a mixture of crystalline and glass phases, and it has a coefficient of thermal expansion of from about 10 to about 18 μm/m-° C. The glass coating has a thickness over the superalloy gas turbine engine component of about 0.5 mils to about 10 mils.

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