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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：WO2020167598A1
公开(公告)日：2020-08-20
申请号：PCT/US2020/017174
申请日：2020-02-07
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： LORICCO, Nicholas M. , JARIWALA, Parth , SCHNEIDER, Alex J. , TELLER, Bret M. , GLEINER, Matthew S. , MORTON, Jeffrey T.
Abstract: A turbine blade has an attachment root and an airfoil. A cooling passageway system has a plurality of trunks extending from respective inlets along the root inner diameter end from a leading trunk near a first axial end to a trailing trunk near a second axial end; and a plurality of outlets along the airfoil including trailing edge outlets fed by the trailing trunk. Viewed normal to a root end-to-end centerplane: the trailing trunk has a turn passing forward and then rearward; an outside of the turn protrudes forward; and the outside of the turn has a tighter curvature than an inside of the turn.
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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：WO2013165509A3
公开(公告)日：2013-11-07
申请号：PCT/US2013/025711
申请日：2013-02-12
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： KOHLI, Atul , GLEINER, Matthew S.
Abstract: A gas turbine engine component subjected to a flow of high temperature gas includes a wall having first and second wall surfaces and a cooling hole extending through the wall. The cooling hole includes an inlet located at the first wall surface, an outlet located at the second wall surface, a metering section extending downstream from the inlet and a diffusing section extending from the metering section to the outlet. The diffusing section includes a first lobe, a second lobe and a transition region. The first lobe diverges longitudinally and laterally from the metering section and has a first shape. The second lobe is generally opposite the first lobe and diverges longitudinally and laterally from the metering section and has a second shape different from the first shape. The transition region is positioned between the first and second lobes and includes a downstream end adjacent the outlet.
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公开(公告)号：WO2013165510A2
公开(公告)日：2013-11-07
申请号：PCT/US2013/025715
申请日：2013-02-12
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： XU, JinQuan , ZELESKY, Mark F. , KOHLI, Atul , GLEINER, Matthew S.
CPC classification number: F01D5/186 , F01D9/065 , F05D2240/81 , F05D2260/202 , Y02T50/676 , Y10T29/49323
Abstract: A gas turbine engine component includes a wall having first and second wall surfaces and a cooling hole extending through the wall. The cooling hole includes an inlet at the first wall surface, an outlet at the second wall surface, a metering section extending downstream from the inlet and a diffusing section extending from the metering section to the outlet. The diffusing section includes a first lobe diverging longitudinally and laterally from the metering section, a second lobe adjacent the first lobe and diverging longitudinally from the metering section, a third lobe adjacent the second lobe and diverging longitudinally and laterally from the metering section, and a transition region having an end adjacent the outlet and a portion that extends between the lobes and the outlet. The first and third lobes each include a curved outer portion.
Abstract translation: 燃气涡轮发动机部件包括具有第一和第二壁表面的壁和延伸穿过壁的冷却孔。 冷却孔包括在第一壁表面处的入口，在第二壁表面处的出口，从入口下游延伸的计量部分和从计量部分延伸到出口的扩散部分。 扩散部分包括从计量部分纵向和横向分散的第一凸角，与第一凸角相邻并且从计量部分纵向发散的第二凸角，邻近第二凸角并从计量部分纵向和横向发散的第三凸角，以及 过渡区域具有邻近出口的端部和在凸角和出口之间延伸的部分。 第一和第三瓣每个包括弯曲的外部部分。
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Patent Agency Ranking
公开(公告)号：WO2013165507A2
公开(公告)日：2013-11-07
申请号：PCT/US2013/025705
申请日：2013-02-12
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： GLEINER, Matthew S. , KOHLI, Atul , ZELESKY, Mark F.
CPC classification number: F01D5/186 , F01D9/065 , F05D2240/81 , F05D2250/324 , F05D2250/73 , F05D2260/202 , F23R3/002 , F23R3/06 , F23R2900/00018 , F23R2900/03042 , Y02T50/676 , Y10T29/49323
Abstract: A gas turbine engine component includes a wall having first and second wall surfaces and a cooling hole extending through the wall. The cooling hole includes an inlet located at the first wall surface, an outlet located at the second wall surface, a metering section extending downstream from the inlet and a diffusing section extending from the metering section to the outlet. The diffusing section includes a first lobe diverging longitudinally from the metering section and a second lobe adjacent the first lobe and diverging longitudinally and laterally from the metering section.
Abstract translation: 燃气涡轮发动机部件包括具有第一和第二壁表面的壁和延伸穿过壁的冷却孔。 冷却孔包括位于第一壁表面的入口，位于第二壁表面处的出口，从入口下游延伸的计量部分和从计量部分延伸到出口的扩散部分。 漫射部分包括从计量部分纵向分散的第一凸角和邻近第一凸角的第二凸角并且从计量部分纵向和横向发散。
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公开(公告)号：WO2013122910A1
公开(公告)日：2013-08-22
申请号：PCT/US2013/025697
申请日：2013-02-12
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： XU, JinQuan , ZELESKY, Mark F. , KOHLI, Atul , GLEINER, Matthew S.
CPC classification number: F23R3/06 , F01D5/186 , F01D9/065 , F05D2240/81 , F23R2900/03042 , Y02T50/676
Abstract: A gas turbine engine component includes a cooling hole. The cooling hole includes an inlet, an outlet, a metering section and a diffusing section. The diffusing section extends from the metering section to the outlet and includes a first lobe diverging longitudinally and laterally from the metering section, a second lobe adjacent the first lobe and diverging longitudinally and laterally from the metering section, and a transition region having a portion that extends between the first and second lobes and an end adjacent the outlet.
Abstract translation: 燃气涡轮发动机部件包括冷却孔。 冷却孔包括入口，出口，计量部分和扩散部分。 扩散部分从计量部分延伸到出口并且包括从计量部分纵向和横向发散的第一凸角，邻近第一凸角并从计量部分纵向和横向发散的第二凸角，以及过渡区域，其具有 在第一和第二凸角之间延伸，并且邻近出口延伸。
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公开(公告)号：EP2815108B1
公开(公告)日：2020-11-25
申请号：EP13785027.7
申请日：2013-02-12
Applicant: United Technologies Corporation
Inventor： KOHLI, Atul , GLEINER, Matthew S.
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公开(公告)号：EP3088100B1
公开(公告)日：2020-01-01
申请号：EP16167665.5
申请日：2016-04-29
Applicant: United Technologies Corporation
Inventor： GLEINER, Matthew S. , TELLER, Bret M. , AUXIER, James T.
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公开(公告)号：EP2815107B1
公开(公告)日：2020-11-18
申请号：EP13784812.3
申请日：2013-02-12
Applicant: United Technologies Corporation
Inventor： GLEINER, Matthew S. , KOHLI, Atul , ZELESKY, Mark F.
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