Invention Grant
US09322554B2 Temperature mixing enhancement with locally co-swirling quench jet pattern for gas turbine engine combustor
有权
用于燃气轮机发动机燃烧器的局部共旋流淬火喷射模式的温度混合增强
- Patent Title: Temperature mixing enhancement with locally co-swirling quench jet pattern for gas turbine engine combustor
- Patent Title (中): 用于燃气轮机发动机燃烧器的局部共旋流淬火喷射模式的温度混合增强
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Application No.: US13194182Application Date: 2011-07-29
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Publication No.: US09322554B2Publication Date: 2016-04-26
- Inventor: Won-Wook Kim , James B. Hoke , Timothy S. Snyder
- Applicant: Won-Wook Kim , James B. Hoke , Timothy S. Snyder
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F02C1/00
- IPC: F02C1/00 ; F23R3/06 ; F23R3/08
Abstract:
A combustor for a turbine engine includes a first liner defined about an axis with a first row of first combustion air holes, one of the first combustion air holes is defined along each of a multiple of fuel injector zero pitch lines. A second liner defined about the axis with a second row of second combustion air holes, each of the second combustion air holes circumferentially offset relative to each of the multiple of fuel injector zero pitch lines.
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