Invention Application
US20170016620A1 COMBUSTOR ASSEMBLY FOR USE IN A GAS TURBINE ENGINE AND METHOD OF ASSEMBLING
审中-公开
用于燃气涡轮发动机的燃烧器组件和组装方法
- Patent Title: COMBUSTOR ASSEMBLY FOR USE IN A GAS TURBINE ENGINE AND METHOD OF ASSEMBLING
- Patent Title (中): 用于燃气涡轮发动机的燃烧器组件和组装方法
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Application No.: US14801962Application Date: 2015-07-17
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Publication No.: US20170016620A1Publication Date: 2017-01-19
- Inventor: Matthieu Marc Masquelet , Narendra Digamber Joshi , Venkat Eswarlu Tangirala , Sarah Marie Monahan
- Applicant: General Electric Company
- Main IPC: F23R3/00
- IPC: F23R3/00 ; F23R3/28

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
- US10712002B2 Combustor assembly for use in a gas turbine engine and method of assembling Public/Granted day:2020-07-14
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