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公开(公告)号：WO2015041806A1
公开(公告)日：2015-03-26
申请号：PCT/US2014/052596
申请日：2014-08-26
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： LEWIS, Scott D. , MONGILLO, JR., Dominic J. , ZELESKY, Mark F. , TELLER, Bret M. , DEIBEL, Russell , GLEINER, Matthew S.
CPC classification number: F01D9/041 , F01D5/02 , F01D11/08 , F01D11/24 , F02C3/04 , F04D29/321 , F04D29/542 , F04D29/584 , 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：WO2015126488A2
公开(公告)日：2015-08-27
申请号：PCT/US2014/066495
申请日：2014-11-20
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： TAFFET, Steven , DONNELL, Brandon S. , NADEAU, Daniel C. , DEIBEL, Russell , QUACH, San
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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Patent Agency Ranking
公开(公告)号：WO2014008015A1
公开(公告)日：2014-01-09
申请号：PCT/US2013/047223
申请日：2013-06-24
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： WILLEY, Lawrence J. , GLEINER, Matthew S. , DEIBEL, Russell
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 according to an exemplary embodiment of the present disclosure can include 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.
Abstract translation: 根据本公开的示例性实施例的用于燃气涡轮发动机的部件可以包括具有外表面和内表面的平台。 盖板可以邻近平台的外表面定位。 平台的外表面可以包括一个口袋，盖板相对于口袋定位，以在它们之间建立平台冷却通道。
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公开(公告)号：EP3049640A1
公开(公告)日：2016-08-03
申请号：EP14845261.8
申请日：2014-08-26
Applicant: United Technologies Corporation
Inventor： LEWIS, Scott D. , MONGILLO, JR. Dominic J. , ZELESKY, Mark F. , TELLER, Bret M. , DEIBEL, Russell , GLEINER, Matthew S.
CPC classification number: F01D9/041 , F01D5/02 , F01D11/08 , F01D11/24 , F02C3/04 , F04D29/321 , F04D29/542 , F04D29/584 , 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.
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公开(公告)号：EP2867502A1
公开(公告)日：2015-05-06
申请号：EP13812464.9
申请日：2013-06-24
Applicant: United Technologies Corporation
Inventor： WILLEY, Lawrence J. , GLEINER, Matthew S. , DEIBEL, Russell
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 according to an exemplary embodiment can include 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.
Abstract translation: 根据本公开的示例性实施例的用于燃气涡轮发动机的部件可以包括具有外表面和内表面的平台。 盖板可以定位在平台的外表面附近。 平台的外表面可以包括袋子，并且盖板相对于袋子定位以在其间建立平台冷却通道。
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公开(公告)号：EP3086893B1
公开(公告)日：2019-07-24
申请号：EP14883263.7
申请日：2014-11-20
Applicant: United Technologies Corporation
Inventor： TAFFET, Steven , DONNELL, Brandon S. , NADEAU, Daniel C. , DEIBEL, Russell , QUACH, San
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公开(公告)号：EP3086893A2
公开(公告)日：2016-11-02
申请号：EP14883263.7
申请日：2014-11-20
Applicant: United Technologies Corporation
Inventor： TAFFET, Steven , DONNELL, Brandon S. , NADEAU, Daniel C. , DEIBEL, Russell , QUACH, San
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和第二腿，其具有连接第一和第二腿的多个交叉构件。 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。 第二交叉构件延伸第二横截面积，并且中心交叉构件延伸第三横截面积。 第一横截面积大于第二横截面积。 第二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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