Invention Grant
- Patent Title: Flow sleeve with tabbed direct combustion liner cooling air
- Patent Title (中): 流动套管带有标签式直接燃烧衬里冷却空气
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Application No.: US12169994Application Date: 2008-07-09
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Publication No.: US08109099B2Publication Date: 2012-02-07
- Inventor: John S. Tu , Jaisukhlal V. Chokshi , Christopher R. Brdar , Randal G. McKinney , Shakira A. Ramos
- Applicant: John S. Tu , Jaisukhlal V. Chokshi , Christopher R. Brdar , Randal G. McKinney , Shakira A. Ramos
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Carlson, Gaskey & Olds, PC
- Main IPC: F02C1/00
- IPC: F02C1/00

Abstract:
A combustion duct for a gas turbine engine has a combustion liner to receive products of combustion, and deliver the products of combustion downstream toward a turbine rotor. An outer housing is positioned radially outwardly of the combustion liner. A flow sleeve is positioned radially intermediate the outer housing and the combustion liner. A chamber radially outwardly of the flow sleeve receives cooling air. A plurality of holes through the flow sleeve deliver cooling air from the chamber against an outer periphery of the combustion liner. A plurality of tabs are associated with at least some of the holes in the flow sleeve. The tabs are positioned to extend radially inwardly on a downstream side of the holes.
Public/Granted literature
- US20100005805A1 FLOW SLEEVE WITH TABBED DIRECT COMBUSTION LINER COOLING AIR Public/Granted day:2010-01-14
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