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公开(公告)号：US20140083111A1
公开(公告)日：2014-03-27
申请号：US13626523
申请日：2012-09-25
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Shawn J. Gregg , Kevin K. Low
CPC classification number: F02C3/14 , F23R3/28 , F23R3/50 , F23R2900/00014
Abstract: A combustor of a gas turbine engine includes a multiple of fuel nozzles arranged asymmetrically
Abstract translation: 燃气涡轮发动机的燃烧器包括不对称排列的多个燃料喷嘴
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