发明申请
- 专利标题: COMBUSTOR APPARATUS IN A GAS TURBINE ENGINE
- 专利标题(中): 燃气涡轮发动机中的燃烧器装置
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申请号: US13783857申请日: 2013-03-04
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公开(公告)号: US20140245740A1公开(公告)日: 2014-09-04
- 发明人: David J. Wiebe , Stephen A. Ramier , Robert H. Bartley , Daniel W. Garan , Erick J. Deane , Mark L. Adamson , Yadollah Naghian
- 申请人: David J. Wiebe , Stephen A. Ramier , Robert H. Bartley , Daniel W. Garan , Erick J. Deane , Mark L. Adamson , Yadollah Naghian
- 主分类号: F23R3/28
- IPC分类号: F23R3/28
摘要:
A combustor apparatus defines a combustion zone where air and fuel are burned to create high temperature combustion products. The combustor apparatus includes an outer wall, coupling structure on the outer wall adjacent to a fuel inlet opening thereof, a fuel injection system, a fuel feed assembly, and a fitting member. The fuel injection system provides fuel to be burned in the combustion zone. The fuel supply structure includes a threaded inner surface formed from a first material. The fuel feed assembly includes a fuel feed pipe that extends through the fuel inlet opening in the outer wall and has an outlet portion formed from the first material and that is threadedly engaged with the fuel supply structure, and an inlet portion affixed to the outlet portion and formed from a second material. The fitting member secures the fuel feed assembly relative to the outer wall.
公开/授权文献
- US09267689B2 Combustor apparatus in a gas turbine engine 公开/授权日:2016-02-23
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