Invention Grant
- Patent Title: Combustor assembly for use in a gas turbine engine and method of assembling
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Application No.: US14801962Application Date: 2015-07-17
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Publication No.: US10712002B2Publication Date: 2020-07-14
- Inventor: Matthieu Marc Masquelet , Narendra Digamber Joshi , Venkat Eswarlu Tangirala , Sarah Marie Monahan
- 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: Armstrong Teasdale LLP
- Main IPC: F23R3/00
- IPC: F23R3/00 ; F23R3/28 ; F23R3/60 ; F23R3/10 ; F23R3/26 ; F23R3/20 ; F23R3/04

Abstract:
A combustor assembly for use in a gas turbine engine is provided. The combustor assembly includes a dome assembly, a fuel nozzle coupled to the dome assembly, and a cowl assembly. The cowl assembly includes a radially inner cowl coupled to the dome assembly, and a radially outer cowl including a first cowl member and a second cowl member each positioned about the fuel nozzle. The first and second cowl members substantially align to define a substantially continuous flow path configured to direct a flow of air about the dome assembly.
Public/Granted literature
- US20170016620A1 COMBUSTOR ASSEMBLY FOR USE IN A GAS TURBINE ENGINE AND METHOD OF ASSEMBLING Public/Granted day:2017-01-19
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