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CERAMIC MATRIX COMPOSITE COMPONENT, GAS TURBINE SEAL ASSEMBLY, AND METHOD OF FORMING CERAMIC MATRIX COMPOSITE COMPONENT

机译:陶瓷基复合材料组分,燃气轮机密封组件和形成陶瓷基复合材料组分的方法

摘要

A gas turbine seal assembly includes a gas turbine component and a gas turbine seal component contacting the gas turbine component to form a seal between the two components. The gas turbine seal component includes ceramic matrix composite plies bonded together to form the ceramic matrix composite component. A bond-inhibiting coating on a non-bonding portion of a first surface of one of the ceramic matrix composite plies prevents bonding between the non-bonding portion of the first surface and a second surface of a neighboring ceramic matrix composite ply. At least one bonding portion of the first surface lacking the bond-inhibiting coating is bonded to the second surface. A method of forming a ceramic matrix composite component includes selectively applying a bond-inhibiting coating to a non-bonding portion of a first surface of a ceramic matrix composite ply and bonding the ceramic matrix composite plies together.
机译:燃气轮机密封组件包括燃气轮机部件和与燃气轮机部件接触以在两个部件之间形成密封的燃气轮机密封部件。燃气轮机密封部件包括粘结在一起以形成陶瓷基复合材料部件的陶瓷基复合材料层。陶瓷基复合材料层中的一个的第一表面的非粘结部分上的抑制粘结的涂层防止第一表面的非粘结部分与相邻的陶瓷基复合材料层的第二表面之间的粘结。第一表面的至少一个没有结合抑制涂层的结合部分被结合到第二表面。形成陶瓷基复合材料组件的方法包括:将抑制粘结的涂层选择性地施加到陶瓷基复合材料层的第一表面的非粘结部分,并将陶瓷基复合材料层粘结在一起。

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