Invention Grant
- Patent Title: Turbine engine assembly and method of assembling the same
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Application No.: US14870853Application Date: 2015-09-30
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Publication No.: US10280760B2Publication Date: 2019-05-07
- Inventor: Narendra Digamber Joshi , Christian Lee Vandervort , Krishan Lal Luthra , Ronald Scott Bunker , Joel Meier Haynes , Venkat Eswarlu Tangirala
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: GENERAL ELECTRIC COMPANY
- Current Assignee: GENERAL ELECTRIC COMPANY
- Current Assignee Address: US NY Schenectady
- Agency: GE Global Patent Operation
- Agent John Darling
- Main IPC: F02C1/00
- IPC: F02C1/00 ; F02C3/34 ; F02C1/08 ; F01D5/18 ; F23R3/00 ; F02C6/00 ; F02C7/18 ; F23C9/08 ; F01D25/32

Abstract:
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.
Public/Granted literature
- US20170089205A1 TURBINE ENGINE ASSEMBLY AND METHOD OF ASSEMBLING THE SAME Public/Granted day:2017-03-30
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