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公开(公告)号：US20160251969A1
公开(公告)日：2016-09-01
申请号：US14634006
申请日：2015-02-27
Applicant: United Technologies Corporation
Inventor： Mark A. Boeke , Richard M. Salzillo , Jeffrey J. DeGray , Shawn J. Gregg
CPC classification number: F01D5/189 , F01D5/141 , F01D5/147 , F01D9/041 , F01D9/065 , F01D25/12 , F05D2220/32 , F05D2230/20 , F05D2230/60 , F05D2240/126 , F05D2240/301 , F05D2240/81 , F05D2260/221 , Y02T50/676
Abstract: An airfoil includes an airfoil wall including an exterior airfoil surface and at least partially defines an airfoil cavity. A fillet is on the exterior airfoil surface. A recess is in an interior surface of the airfoil wall adjacent the fillet. A baffle tube is located in the airfoil cavity spaced from the recess.
Abstract translation: 翼型件包括包括外部翼型件表面的翼型件壁，并且至少部分地限定翼型腔。 一个圆角在外部翼面上。 凹槽位于靠近圆角的翼型壁的内表面。 挡板管位于与凹槽间隔开的翼型腔中。
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公开(公告)号：US20140219778A1
公开(公告)日：2014-08-07
申请号：US13630419
申请日：2012-09-28
Applicant: United Technologies Corporation
Inventor： Mark A. Boeke , Shawn J. Gregg , Sarah Riley , Jeffrey J. DeGray , Richard M. Salzillo
CPC classification number: F01D5/186 , F01D5/187 , F01D9/02 , F01D25/12 , F01D25/246 , F05D2240/12 , F05D2240/81 , F05D2260/204 , Y02T50/672 , Y02T50/676
Abstract: A stator vane for a gas turbine engine includes an airfoil extending in a radial direction and supported by a platform having a gas flowpath surface. A cooling passage is arranged in the platform and includes a circumferential passage that is fluidly connected to an inlet passage extending through and edge of the platform, and film cooling holes extending from the gas flowpath surface to the circumferential passage, radial extending passage through the edge of the platform. A void is interconnected to at least one of the radially extending passage and the inlet passage.
Abstract translation: 用于燃气涡轮发动机的定子叶片包括沿径向延伸并由具有气体流路表面的平台支撑的翼型件。 冷却通道布置在平台中，并且包括流体连接到延伸通过平台的边缘的入口通道的圆周通道，以及从气体流路表面延伸到周向通道的膜冷却孔，通过边缘的径向延伸通道 的平台。 空隙与径向延伸通道和入口通道中的至少一个相互连接。
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