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公开(公告)号：WO2014081492A3
公开(公告)日：2014-07-31
申请号：PCT/US2013057059
申请日：2013-08-28
Applicant: UNITED TECHNOLOGIES CORP
Inventor： CUNHA FRANK J , SNYDER TIMOTHY S , ERBAS-SEN NURHAK , WILLIAMS ALEXANDER W , MULE NICHOLAS
CPC classification number: F23R3/06 , F02C7/18 , F23R3/002 , F23R3/005 , F23R3/16 , F23R2900/03041 , F23R2900/03042 , F23R2900/03043 , F23R2900/03044 , F23R2900/03045 , Y02T50/675
Abstract: A combustor liner which reduces cooling flow to a combustion chamber and augments pressure drop split between impingement holes and effusion holes is disclosed. The combustor liner may further include accelerating channels, trip strips, pedestals, and cone-shaped effusion holes to provide further cooling of the liner. The combustor liner may reduce NOx production and the temperature of the combustion chamber of a gas turbine engine or the like.
Abstract translation: 公开了一种减少到燃烧室的冷却流量并增加冲击孔和渗出孔之间的压降分配的燃烧器衬套。 燃烧器衬套还可以包括加速通道，跳闸条，基座和锥形渗出孔，以提供衬套的进一步冷却。 燃烧器衬套可以减少燃气涡轮发动机等的NOx产生和燃烧室的温度。
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公开(公告)号：WO2014055887A3
公开(公告)日：2014-08-28
申请号：PCT/US2013063494
申请日：2013-10-04
Applicant: UNITED TECHNOLOGIES CORP
Inventor： BANGERTER JAMES P , WILLIAMS ALEXANDER W , MULE NICHOLAS , PACHECO-TOUGAS MONICA
CPC classification number: F23R3/06 , F23R3/10 , F23R3/50 , F23R2900/03041 , F23R2900/03043 , F23R2900/03044 , F23R2900/03045 , Y02T50/675
Abstract: A liner for a combustor of a turbine engine includes a cooling feature which projects from a backside and an effusion hole that communicates through the liner
Abstract translation: 用于涡轮发动机的燃烧器的衬套包括从后侧突出的冷却特征和通过衬套连通的渗出孔
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3.发明公开COOLING FOR COMBUSTOR LINERS WITH ACCELERATING CHANNELS 审中-公开KÜHLUNGFÜRBRENNKAMMERAUSKLEIDUNGEN MITBESCHLEUNIGUNGSKANÄLEN
公开(公告)号：EP2904238A4
公开(公告)日：2016-07-06
申请号：EP13856137
申请日：2013-08-28
Applicant: UNITED TECHNOLOGIES CORP
Inventor： CUNHA FRANK J , SNYDER TIMOTHY S , ERBAS-SEN NURHAK , WILLIAMS ALEXANDER W , MULE NICHOLAS
IPC: F23R3/06
CPC classification number: F23R3/06 , F02C7/18 , F23R3/002 , F23R3/005 , F23R3/16 , F23R2900/03041 , F23R2900/03042 , F23R2900/03043 , F23R2900/03044 , F23R2900/03045 , Y02T50/675
Abstract: A combustor liner which reduces cooling flow to a combustion chamber and augments pressure drop split between impingement holes and effusion holes is disclosed. The combustor liner may further include accelerating channels, trip strips, pedestals, and cone-shaped effusion holes to provide further cooling of the liner. The combustor liner may reduce NOx production and the temperature of the combustion chamber of a gas turbine engine or the like.
Abstract translation: 公开了一种减少到燃烧室的冷却流动并增加冲击孔和渗出孔之间的压降分配的燃烧器衬套。 燃烧器衬套还可以包括加速通道，跳闸条，基座和锥形排出孔，以提供衬套的进一步冷却。 燃烧器衬套可以减少燃气涡轮发动机等的NOx产生和燃烧室的温度。
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公开(公告)号：EP2904236A4
公开(公告)日：2015-12-09
申请号：EP13843296
申请日：2013-10-04
Applicant: UNITED TECHNOLOGIES CORP
Inventor： BANGERTER JAMES P , WILLIAMS ALEXANDER W , MULE NICHOLAS , PACHECO-TOUGAS MONICA
CPC classification number: F23R3/06 , F23R3/10 , F23R3/50 , F23R2900/03041 , F23R2900/03043 , F23R2900/03044 , F23R2900/03045 , Y02T50/675
Abstract: A liner for a combustor of a turbine engine includes a cooling feature which projects from a backside and an effusion hole that communicates through the liner
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