Invention Grant
- Patent Title: Quench jet arrangement for annular rich-quench-lean gas turbine combustors
- Patent Title (中): 环形富燃冷式燃气轮机的淬火喷射装置
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Application No.: US11947337Application Date: 2007-11-29
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Publication No.: US08127554B2Publication Date: 2012-03-06
- Inventor: Frank J. Zupanc , Rodolphe Dudebout
- Applicant: Frank J. Zupanc , Rodolphe Dudebout
- Applicant Address: US NJ Morristown
- Assignee: Honeywell International Inc.
- Current Assignee: Honeywell International Inc.
- Current Assignee Address: US NJ Morristown
- Agency: Ingrassia Fisher & Lorenz, P.C.
- Main IPC: F02C1/00
- IPC: F02C1/00 ; F02G3/00
Abstract:
An outer liner of a combustor of a gas turbine engine includes a plurality of liner regions arranged adjacent one another and separated by boundary lines; and a plurality of air admission holes formed in the liner regions. The air admission holes within each liner region form a V-pattern.
Public/Granted literature
- US20090139239A1 QUENCH JET ARRANGEMENT FOR ANNULAR RICH-QUENCH-LEAN GAS TURBINE COMBUSTORS Public/Granted day:2009-06-04
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