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公开(公告)号：US09957894B2
公开(公告)日：2018-05-01
申请号：US14627915
申请日：2015-02-20
Applicant: United Technologies Corporation
Inventor： Russell Deibel , Matthew S. Gleiner
CPC classification number: F02C7/18 , F01D5/186 , F01D9/041 , F05D2240/81 , F05D2260/202 , Y02T50/676
Abstract: An airfoil component is described herein. The airfoil component may include an OD platform comprising a gaspath face and a non-gaspath face coupled together via a plurality of cooling holes. The airfoil component may include an airfoil extending in from the outer diameter platform. The plurality of cooling holes comprises a plurality of groups of cooling holes disposed in the outer diameter platform proximate a suction side of the airfoil and a pressure side of the airfoil.
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公开(公告)号：US20170022822A1
公开(公告)日：2017-01-26
申请号：US15039918
申请日：2014-11-20
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Steven Taffet , Brandon S. Donnell , Daniel C. Nadeau , Russell Deibel , San Quach
CPC classification number: F01D5/187 , B22C7/02 , B22C9/04 , B22C9/10 , B22C9/24 , F01D9/041 , F01D25/12 , F05D2220/323 , F05D2230/21 , F05D2230/211 , F05D2240/121 , F05D2240/122 , F05D2240/303 , F05D2240/304 , F05D2260/202 , Y02T50/676
Abstract: A lost core mold component comprises a first leg and a second leg with a plurality of crossover members connecting the first and second legs. The plurality of crossover members includes outermost crossover members spaced from each other. Adjacent ends of each of the first and second legs, and second crossover members are spaced closer to each other than are the outermost crossover members. Central crossover members extend between the first and second leg and between the second crossover members. The outermost crossover members extend for a first cross-sectional area. The second crossover members extend for a second cross-sectional area and the central crossover members extend for a third cross-sectional area. The first cross-sectional area is greater than the second cross-sectional area. The second cross-sectional area is greater than the third cross-sectional area. A gas turbine engine and component are also disclosed.
Abstract translation: 失去的芯模组件包括第一腿部和第二腿部，其具有连接第一和第二腿部的多个交叉构件。 多个交叉构件包括彼此间隔开的最外侧交叉构件。 第一和第二腿部和第二交叉构件中的每一个的相邻端部比最外面的交叉构件彼此更靠近地间隔开。 中央交叉构件在第一和第二腿之间以及第二交叉构件之间延伸。 最外面的交叉构件延伸到第一横截面积。 第二交叉构件延伸到第二横截面积，并且中心交叉构件延伸第三横截面积。 第一截面积大于第二横截面积。 第二横截面积大于第三横截面积。 还公开了一种燃气涡轮发动机和部件。
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公开(公告)号：US10053991B2
公开(公告)日：2018-08-21
申请号：US15790289
申请日：2017-10-23
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Lawrence J. Willey , Matthew S. Gleiner , Russell Deibel
CPC classification number: F01D5/187 , F01D5/188 , F01D9/041 , F01D9/06 , F01D25/12 , F04D29/324 , F04D29/542 , F04D29/582 , F05D2220/32 , F05D2230/21 , F05D2240/55 , F05D2240/81
Abstract: A component for a gas turbine engine includes a platform having an outer surface and an inner surface. A cover plate can be positioned adjacent to the outer surface of the platform. The outer surface of the platform can include a pocket and the cover plate is positioned relative to the pocket to establish a platform cooling channel therebetween.
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公开(公告)号：US09845687B2
公开(公告)日：2017-12-19
申请号：US15056116
申请日：2016-02-29
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Lawrence J. Willey , Matthew S. Gleiner , Russell Deibel
CPC classification number: F01D5/187 , F01D5/188 , F01D9/041 , F01D9/06 , F01D25/12 , F04D29/324 , F04D29/542 , F04D29/582 , F05D2220/32 , F05D2230/21 , F05D2240/55 , F05D2240/81
Abstract: A component for a gas turbine engine includes a platform having an outer surface and an inner surface. A cover plate can be positioned adjacent to the outer surface of the platform. The outer surface of the platform can include a pocket and the cover plate is positioned relative to the pocket to establish a platform cooling channel therebetween.
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公开(公告)号：US20190383153A1
公开(公告)日：2019-12-19
申请号：US16521854
申请日：2019-07-25
Applicant: United Technologies Corporation
Inventor： Scott D. Lewis , Dominic J. Mongillo, JR. , Mark F. Zelesky , Bret M. Teller , Russell Deibel , Matthew S. Gleiner
Abstract: A vane according to an exemplary aspect of the present disclosure includes, among other things, a platform extending from an edge face and between spaced apart lateral faces and an airfoil extending outwardly from the platform. The platform includes at least one ejection port in the edge face and at least one passage connected to the at least one ejection port. A method of cooling a component is also disclosed.
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Patent Agency Ranking
公开(公告)号：US20160245093A1
公开(公告)日：2016-08-25
申请号：US14627915
申请日：2015-02-20
Applicant: United Technologies Corporation
Inventor： Russell Deibel , Matthew S. Gleiner
CPC classification number: F02C7/18 , F01D5/186 , F01D9/041 , F05D2240/81 , F05D2260/202 , Y02T50/676
Abstract: An airfoil component is described herein. The airfoil component may include an OD platform comprising a gaspath face and a non-gaspath face coupled together via a plurality of cooling holes. The airfoil component may include an airfoil extending in from the outer diameter platform. The plurality of cooling holes comprises a plurality of groups of cooling holes disposed in the outer diameter platform proximate a suction side of the airfoil and a pressure side of the airfoil.
Abstract translation: 这里描述了翼型件。 机翼部件可以包括OD平台，该平台包括经由多个冷却孔连接在一起的气路面和非气道面。 机翼部件可以包括从外径平台延伸的翼型件。 多个冷却孔包括多个组的冷却孔，其设置在靠近翼型的吸力侧的外径平台和翼型的压力侧。
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公开(公告)号：US10815803B2
公开(公告)日：2020-10-27
申请号：US16521854
申请日：2019-07-25
Applicant: United Technologies Corporation
Inventor： Scott D. Lewis , Dominic J. Mongillo, Jr. , Mark F. Zelesky , Bret M. Teller , Russell Deibel , Matthew S. Gleiner
Abstract: A vane according to an exemplary aspect of the present disclosure includes, among other things, a platform extending from an edge face and between spaced apart lateral faces and an airfoil extending outwardly from the platform. The platform includes at least one ejection port in the edge face and at least one passage connected to the at least one ejection port. A method of cooling a component is also disclosed.
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公开(公告)号：US20160230577A1
公开(公告)日：2016-08-11
申请号：US15022725
申请日：2014-08-26
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Scott D. Lewis , Dominic J. Mongillo, JR. , Mark F. Zelesky , Bret M. Teller , Russell Deibel , Matthew S. Gleiner
CPC classification number: F01D9/041 , F01D5/02 , F01D11/08 , F01D11/24 , F02C3/04 , F04D29/321 , F05D2220/32 , F05D2240/11 , F05D2240/12 , F05D2240/35 , F05D2240/80 , F05D2240/81 , F05D2250/12 , F05D2260/201 , Y02T50/676
Abstract: A vane according to an exemplary aspect of the present disclosure includes, among other things, a platform extending from an edge face and between spaced apart lateral faces and an airfoil extending outwardly from the platform. The platform includes at least one ejection port in the edge face and at least one passage connected to the at least one ejection port.
Abstract translation: 根据本公开的示例性方面的叶片包括从边缘面和间隔开的侧面之间延伸的平台以及从平台向外延伸的翼型件。 平台包括边缘面中的至少一个喷射口和连接到至少一个喷射口的至少一个通道。
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公开(公告)号：US20200291790A1
公开(公告)日：2020-09-17
申请号：US16415199
申请日：2019-05-17
Applicant: United Technologies Corporation
Inventor： Steven Taffet , Brandon S. Donnell , Daniel C. Nadeau , Russell Deibel , San Quach
Abstract: A lost core mold component comprises a first leg and a second leg with a plurality of crossover members connecting the first and second legs. The plurality of crossover members includes outermost crossover members spaced from each other. Adjacent ends of each of the first and second legs, and second crossover members are spaced closer to each other than are the outermost crossover members. Central crossover members extend between the first and second leg and between the second crossover members. The outermost crossover members extend for a first cross-sectional area. The second crossover members extend for a second cross-sectional area and the central crossover members extend for a third cross-sectional area. The first cross-sectional area is greater than the second cross-sectional area. The second cross-sectional area is greater than the third cross-sectional area. A gas turbine engine and component are also disclosed.
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公开(公告)号：US10408071B2
公开(公告)日：2019-09-10
申请号：US15022725
申请日：2014-08-26
Applicant: United Technologies Corporation
Inventor： Scott D. Lewis , Dominic J. Mongillo, Jr. , Mark F. Zelesky , Bret M. Teller , Russell Deibel , Matthew S. Gleiner
Abstract: A vane according to an exemplary aspect of the present disclosure includes, among other things, a platform extending from an edge face and between spaced apart lateral faces and an airfoil extending outwardly from the platform. The platform includes at least one ejection port in the edge face and at least one passage connected to the at least one ejection port.
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