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11.GAS TURBINE ENGINE COMPONENT COOLING PASSAGE WITH ASYMMETRICAL PEDESTALS 审中-公开
Title translation: GASTURBINENMOTORKOMPONENTENKÜHLKANALMIT ASYMMETRISCHEN UNTERGESTELLEN公开(公告)号:EP3080416A4
公开(公告)日:2017-08-30
申请号:EP14869625
申请日:2014-12-02
Applicant: UNITED TECHNOLOGIES CORP
Inventor: THISTLE CHARLES , THORNTON LANE
IPC: F01D5/18
CPC classification number: F01D5/187 , F01D5/081 , F01D5/186 , F01D5/3007 , F01D25/12 , F05D2220/32 , F05D2230/50 , F05D2240/12 , F05D2240/35 , F05D2240/55 , F05D2260/202 , F05D2260/22141 , F23R3/002
Abstract: A gas turbine engine component includes spaced apart walls that provide a cooling passage that extends in a first direction. A pedestal is arranged in the cooling passage and interconnects the walls in a thickness direction that is transverse to the first direction. The pedestal is asymmetrical in the thickness direction.
Abstract translation: 燃气涡轮发动机部件包括间隔开的壁,其提供沿第一方向延伸的冷却通道。 基座布置在冷却通道中并且在与第一方向横切的厚度方向上将壁互连。 底座在厚度方向上是不对称的。
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12.GAS TURBINE ENGINE TURBINE BLADE LEADING EDGE TIP TRENCH COOLING 审中-公开
Title translation: 沟槽冷却燃气轮机叶片前缘公开(公告)号:EP2932043A4
公开(公告)日:2015-12-16
申请号:EP13863205
申请日:2013-11-14
Applicant: UNITED TECHNOLOGIES CORP
Inventor: QUACH SAN , THORNTON LANE
IPC: F01D5/18
CPC classification number: F01D5/186 , F01D5/20 , F05D2240/303 , F05D2240/307 , Y02T50/673 , Y02T50/676
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公开(公告)号:EP2898203A4
公开(公告)日:2015-11-25
申请号:EP13838225
申请日:2013-09-17
Applicant: UNITED TECHNOLOGIES CORP
Inventor: GAUTSCHI STEVEN BRUCE , THORNTON LANE
CPC classification number: F01D5/189 , F05D2240/126 , Y02T50/676
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