Invention Grant
- Patent Title: Annular rich-quench-lean gas turbine combustors with plunged holes
- Patent Title (中): 环状富稀燃气涡轮燃烧器,带有漏洞
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Application No.: US12394725Application Date: 2009-02-27
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Publication No.: US08171740B2Publication Date: 2012-05-08
- Inventor: Thomas J. Bronson , Frank Joseph Zupanc
- Applicant: Thomas J. Bronson , Frank Joseph Zupanc
- 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: F23R3/06
- IPC: F23R3/06 ; F23R3/50

Abstract:
A combustor may include an outer liner having a first group of air admission holes and defining a plurality of outer liner regions. The combustor may further include an inner liner having a second group of air admission holes and defining a plurality of inner liner regions. The first group of air admission holes within a respective outer liner region may include a first plunged air admission hole approximately axially aligned with the respective fuel injector, a second plunged air admission hole approximately on the outer boundary line between the respective outer liner region and a first adjacent outer liner region, the first air admission hole being downstream of the second air admission hole, and a third plunged air admission hole approximately on the outer boundary line between the respective outer liner region and a second adjacent outer liner region.
Public/Granted literature
- US20100218504A1 ANNULAR RICH-QUENCH-LEAN GAS TURBINE COMBUSTORS WITH PLUNGED HOLES Public/Granted day:2010-09-02
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