Invention Grant
- Patent Title: Flow sleeve for a combustion module of a gas turbine
- Patent Title (中): 用于燃气轮机燃烧模块的流动套管
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Application No.: US13845485Application Date: 2013-03-18
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Publication No.: US09360217B2Publication Date: 2016-06-07
- Inventor: Richard Martin DiCintio , Patrick Benedict Melton , Lucas John Stoia , Christopher Paul Willis , Ronnie Ray Pentecost
- 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: Dority & Manning, PA
- Main IPC: F02C7/22
- IPC: F02C7/22 ; F23R3/20 ; F23R3/00 ; F23R3/46 ; F23R3/60 ; F23R3/34

Abstract:
A combustion module for a combustor of a gas turbine includes an annular fuel distribution manifold disposed at an upstream end of the combustion module. The fuel distribution manifold includes an annular support sleeve having an inner surface. The combustion module further includes a fuel injection assembly having an annular combustion liner that extends downstream from the fuel distribution manifold and that terminates at an aft frame, and an annular flow sleeve that circumferentially surrounds the combustion liner. The flow sleeve extends downstream from the fuel distribution manifold and terminates at the aft frame. The flow sleeve extends continuously between the support sleeve and the aft frame. A forward portion of the flow sleeve is positioned concentrically within the support sleeve where the forward portion is slidingly engaged with the inner surface of the support sleeve.
Public/Granted literature
- US20140260277A1 FLOW SLEEVE FOR A COMBUSTION MODULE OF A GAS TURBINE Public/Granted day:2014-09-18
Information query
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