公开(公告)号：US20160090846A1

公开(公告)日：2016-03-31

申请号：US14892713

申请日：2014-04-25

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Sarah Riley ,  Sasha M. Moore ,  Jeffrey R. Levine

IPC: F01D5/18 ,  F01D25/12 ,  F01D9/04

CPC classification number: F01D5/186 ,  F01D5/189 ,  F01D9/041 ,  F01D25/12 ,  F05D2220/32 ,  F05D2240/12 ,  F05D2240/122 ,  F05D2240/124 ,  F05D2240/30 ,  F05D2260/201 ,  F05D2260/202 ,  Y02T50/672 ,  Y02T50/676

Abstract: An airfoil for a gas turbine engine includes an outer airfoil wall that provides an exterior surface and multiple radially extending cooling passages. The exterior surface provides pressure and suctions sides joined by leading and trailing edges. The cooling passages include a supply passage arranged upstream from and in fluid communication with a trailing edge passage. A cooling hole extends through the outer airfoil wall from the supply passage to the exterior surface on the suction side.

Abstract translation: 用于燃气涡轮发动机的翼型件包括提供外表面和多个径向延伸的冷却通道的外翼型壁。 外表面提供由前缘和后缘连接的压力和吸力面。 冷却通道包括设置在后缘通道上游并与后缘通道流体连通的供给通道。 冷却孔从供气通道的外侧翼面壁延伸到吸入侧的外表面。

公开(公告)号：US20190218916A1

公开(公告)日：2019-07-18

申请号：US16365943

申请日：2019-03-27

Applicant: United Technologies Corporation

Inventor： Sarah Riley ,  Sasha M. Moore ,  Jeffrey R. Levine

IPC: F01D5/18 ,  F01D9/04 ,  F01D25/12

CPC classification number: F01D5/186 ,  F01D5/189 ,  F01D9/041 ,  F01D25/12 ,  F05D2220/32 ,  F05D2240/12 ,  F05D2240/122 ,  F05D2240/124 ,  F05D2240/30 ,  F05D2260/201 ,  F05D2260/202 ,  Y02T50/672 ,  Y02T50/676

Abstract: An airfoil for a gas turbine engine includes an outer airfoil wall that provides an exterior surface and multiple radially extending cooling passages. The exterior surface provides pressure and suctions sides joined by leading and trailing edges. The cooling passages include a supply passage arranged upstream from and in fluid communication with a trailing edge passage. A cooling hole extends through the outer airfoil wall from the supply passage to the exterior surface on the suction side.

公开(公告)号：US10294806B2

公开(公告)日：2019-05-21

申请号：US14770189

申请日：2014-03-11

Applicant: United Technologies Corporation

Inventor： Sarah Riley ,  Jeffrey R. Levine ,  Mark A. Boeke

IPC: F01D9/04 ,  C23C14/04 ,  C23C4/02 ,  C23C4/11 ,  C23C4/01 ,  C23C4/12 ,  C23C14/22 ,  C23C4/134 ,  F01D5/28 ,  C23C14/30

Abstract: An article includes a body that has a coating thereon. The coating has a first portion disposed on a first section of the body and a second portion disposed on a second, different section of the body. The first portion has a first microstructure and the second portion has a second, different microstructure.

公开(公告)号：US10253634B2

公开(公告)日：2019-04-09

申请号：US14892713

申请日：2014-04-25

Applicant: United Technologies Corporation

Inventor： Sarah Riley ,  Sasha M. Moore ,  Jeffrey R. Levine

IPC: F01D5/18 ,  F01D9/04 ,  F01D25/12

Abstract: An airfoil for a gas turbine engine includes an outer airfoil wall that provides an exterior surface and multiple radially extending cooling passages. The exterior surface provides pressure and suctions sides joined by leading and trailing edges. The cooling passages include a supply passage arranged upstream from and in fluid communication with a trailing edge passage. A cooling hole extends through the outer airfoil wall from the supply passage to the exterior surface on the suction side.

公开(公告)号：US10132168B2

公开(公告)日：2018-11-20

申请号：US15069738

申请日：2016-03-14

Applicant: United Technologies Corporation

Inventor： Jeffrey Leon ,  Daniel C. Nadeau ,  Jeffrey R. Levine ,  Eleanor D. Kaufman ,  Richard N. Allen ,  Evan P. Molony ,  Gregory Anselmi

IPC: F01D5/14 ,  F01D5/18 ,  F02C7/18 ,  B22C9/10

Abstract: An airfoil is disclosed, comprising an airfoil body and an internal cavity within the airfoil body. The internal cavity may comprise an outer edge comprising a first outer scallop and a second outer scallop, an inner edge opposite the outer edge, the inner edge comprising a first inner scallop and a second inner scallop, a leading edge spanning between the outer edge and the inner edge, and a trailing edge spanning between the outer edge and the inner edge and opposite the leading edge. Between the outer edge, the inner edge, the leading edge, and the trailing edge, the internal cavity may comprise eight columns of pedestals disposed axially relative to one another and axially between the leading edge and the trailing edge.

公开(公告)号：US09995147B2

公开(公告)日：2018-06-12

申请号：US14619343

申请日：2015-02-11

Applicant: United Technologies Corporation

Inventor： Dominic J. Mongillo, Jr. ,  Jeffrey R. Levine ,  Kyle C. Lana ,  Sasha M. Moore

IPC: F01D5/18 ,  F01D5/20

CPC classification number: F01D5/186 ,  F01D5/187 ,  F01D5/20 ,  F05D2240/307 ,  F05D2260/2214 ,  F05D2260/22141 ,  Y02T50/673 ,  Y02T50/676

Abstract: A turbine blade according to an example of the present disclosure includes, among other things, a platform, an airfoil tip, and an airfoil section between the platform and the airfoil tip. The airfoil section has a cavity spaced radially from the airfoil tip and a plurality of cooling passages radially between the cavity and the airfoil tip. Each of the plurality of cooling passages defines an exit port adjacent the airfoil tip. An internal feature within each of the plurality of cooling passages is configured to meter flow to the exit port.

公开(公告)号：US09938837B2

公开(公告)日：2018-04-10

申请号：US14390496

申请日：2013-03-12

Applicant: United Technologies Corporation

Inventor： Jeffrey R. Levine ,  Jeffrey S. Beattie ,  Malcolm C. Staddon

IPC: F01D5/18 ,  B22C9/10

CPC classification number: F01D5/188 ,  B22C9/103 ,  B22C9/108 ,  F01D5/187 ,  F05D2200/33 ,  F05D2230/211 ,  F05D2260/22141 ,  F05D2260/607 ,  F05D2300/13 ,  Y02E10/721

Abstract: An airfoil has a body that includes leading and trailing edges that adjoin pressure and suction sides to provide an exterior airfoil surface. A cooling passage extends in a radial direction from a root to a tip. A trailing edge cooling passage interconnects the cooling passage to the trailing edge. The trailing edge cooling passage includes first and second pedestals of different sizes that are arranged in a repeating pattern with respect to pedestals of the same size and with respect to pedestals of different sizes.

公开(公告)号：US20160208627A1

公开(公告)日：2016-07-21

申请号：US14599075

申请日：2015-01-16

Applicant: United Technologies Corporation

Inventor： Mark A. Boeke ,  Kristopher K. Anderson ,  Jeffrey J. De Gray ,  Jeffrey R. Levine ,  Sarah Riley ,  Richard M. Salzillo, JR.

IPC: F01D9/02

CPC classification number: F01D25/12 ,  F01D9/023 ,  F01D9/04 ,  F01D9/06 ,  F05D2240/81 ,  Y02T50/676

Abstract: An airfoil platform includes a platform body having an arcuate base defining a centerline axis. A rail extends radially outboard from a side of the arcuate base. A feed orifice is defined at least partially in the rail. The inner diameter edge of an axially facing opening of the feed orifice is spaced apart radially outboard of an outer diameter surface of the arcuate base. A method for manufacturing an airfoil platform includes providing an airfoil platform body and forming the feed orifice through the rail. Forming the feed orifice through the rail includes forming the feed orifice radially outboard of and spaced apart from the outer diameter surface of the arcuate base.

Abstract translation: 翼型平台包括具有限定中心线轴线的弓形基部的平台本体。 轨道从弓形底座的一侧沿径向外侧延伸。 进料口至少部分地限定在轨道中。 进料孔的轴向面向的开口的内径边缘在弧形底座的外径表面的径向外侧间隔开。 一种用于制造翼型平台的方法包括提供翼型平台本体并通过导轨形成进料口。 通过导轨形成进料孔包括在弓形底座的外径表面径向地形成进料孔并且间隔开。