发明名称 TURBINE ENGINE ASSEMBLY AND METHOD OF ASSEMBLING THE SAME
摘要 A turbine assembly is provided. The turbine assembly includes a gas turbine engine including at least one hot gas path component formed at least partially from a ceramic matrix composite material. The turbine assembly also includes a treatment system positioned to receive a flow of exhaust gas from the gas turbine engine. The treatment system is configured to remove water from the flow of exhaust gas to form a flow of treated exhaust gas, and to channel the flow of treated exhaust gas towards the at least one hot gas path component. The at least one hot gas path component includes a plurality of cooling holes for channeling the flow of treated exhaust gas therethrough, such that a protective film is formed over the at least one hot gas path component.
申请公布号 US2017089205(A1) 申请公布日期 2017.03.30
申请号 US201514870853 申请日期 2015.09.30
申请人 General Electric Company 发明人 Joshi Narendra Digamber;Vandervort Christian Lee;Luthra Krishan Lal;Bunker Ronald Scott;Haynes Joel Meier;Tangirala Venkat Eswarlu
分类号 F01D5/18;F02C6/18;F01D25/08;F01D9/02;F23R3/00;F02C3/04;F02C7/14 主分类号 F01D5/18
代理机构 代理人
主权项 1. A turbine assembly comprising: a gas turbine engine comprising at least one hot gas path component formed at least partially from a ceramic matrix composite material; and a treatment system positioned to receive a flow of exhaust gas from said gas turbine engine, said treatment system configured to remove water from the flow of exhaust gas to form a flow of treated exhaust gas, and to channel the flow of treated exhaust gas towards said at least one hot gas path component, wherein said at least one hot gas path component comprises a plurality of cooling holes for channeling the flow of treated exhaust gas therethrough, such that a protective film is formed over said at least one hot gas path component.
地址 Schenectady NY US