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61.DUAL FUEL NOZZLE WITH SWIRLING AXIAL GAS INJECTION FOR A GAS TURBINE ENGINE 审中-公开
Title translation: 喷嘴轴向WIRBELUNGSGASINJEKTION的燃气涡轮发动机公开(公告)号:EP3039343A4
公开(公告)日:2017-04-12
申请号:EP14864668
申请日:2014-08-19
Applicant: UNITED TECHNOLOGIES CORP
Inventor: KOPP-VAUGHAN KRISTIN , SNYDER TIMOTHY S , SMITH RANDOLPH J , DAI ZHONGTAO
CPC classification number: F23R3/14 , F23C1/08 , F23D11/106 , F23D2900/11101 , F23R3/28 , F23R3/36 , Y02T50/675
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62.CONTOURED DILUTION PASSAGES FOR A GAS TURBINE ENGINE COMBUSTOR 审中-公开
Title translation: 用于燃气轮机燃烧室的轮廓式稀释通道公开(公告)号:EP3039346A4
公开(公告)日:2016-08-24
申请号:EP14840707
申请日:2014-06-30
Applicant: UNITED TECHNOLOGIES CORP
Inventor: KOSTKA JR STANISLAV , MCKINNEY RANDAL G , HOKE JAMES B , SNYDER TIMOTHY S , CUNHA FRANK J
CPC classification number: F23R3/06 , F02C7/18 , F23R3/002 , F23R3/04 , F23R3/045 , F23R3/26 , F23R2900/03041 , F23R2900/03044 , Y02T50/675
Abstract: A wall assembly for use in a combustor of a gas turbine engine includes a support shell with a first inner periphery along an axis and a liner panel with a second inner periphery along the axis. The second inner periphery is smaller than the first inner periphery. Another wall assembly for use in a combustor of a gas turbine engine includes an annular grommet mounted between the support shell and the liner panel. The annular grommet defines a contoured inner wall.
Abstract translation: 用于燃气涡轮发动机的燃烧器的壁组件包括具有沿着轴线的第一内周边的支撑壳体和具有沿轴线的第二内周边的衬板。 第二内周小于第一内周。 用于燃气涡轮发动机的燃烧器的另一个壁组件包括安装在支撑壳和衬板之间的环形垫圈。 环形垫圈限定了一个轮廓的内壁。
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63.GAS TURBINE ENGINE COMBUSTOR WITH TAILORED TEMPERATURE PROFILE 审中-公开
Title translation: 燃气涡轮燃烧器与定制的温度曲线公开(公告)号:EP2935997A4
公开(公告)日:2016-03-09
申请号:EP13864137
申请日:2013-12-20
Applicant: UNITED TECHNOLOGIES CORP
Inventor: SNYDER TIMOTHY S , MCKINNEY RANDAL G , HOKE JAMES B
CPC classification number: F23R3/002 , F02C7/2365 , F23R3/06 , F23R3/12 , F23R3/26 , F23R3/286 , Y02T50/675
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