公开(公告)号：WO2015126488A3

公开(公告)日：2015-11-05

申请号：PCT/US2014066495

申请日：2014-11-20

Applicant: UNITED TECHNOLOGIES CORP

Inventor： TAFFET STEVEN ,  DONNELL BRANDON S ,  NADEAU DANIEL C ,  DEIBEL RUSSELL ,  QUACH SAN

IPC: B22C9/10 ,  B22C9/22 ,  F01D5/18

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: 失芯模具部件包括第一腿部和第二腿部，第二腿部具有连接第一腿部和第二腿部的多个交叉部件。 多个交叉部件包括彼此间隔开的最外侧交叉部件。 第一支腿和第二支腿中的每一个的相邻末端以及第二交叉构件彼此间隔得比最外侧交叉构件更靠近彼此。 中央交叉部件在第一腿和第二腿之间以及第二交叉部件之间延伸。 最外面的跨接构件延伸第一横截面区域。 第二交叉部件延伸第二横截面区域，并且中央交叉部件延伸第三横截面区域。 第一横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。 燃气涡轮发动机和部件也被公开。

公开(公告)号：PL3086893T3

公开(公告)日：2020-01-31

申请号：PL14883263

申请日：2014-11-20

Applicant: UNITED TECHNOLOGIES CORP

Inventor： TAFFET STEVEN ,  DONNELL BRANDON S ,  NADEAU DANIEL C ,  DEIBEL RUSSELL ,  QUACH SAN

IPC: B22C9/10 ,  B22C7/02 ,  B22C9/04 ,  B22C9/22 ,  B22C9/24 ,  F01D5/18 ,  F01D9/04

公开(公告)号：EP2867502A4

公开(公告)日：2015-07-08

申请号：EP13812464

申请日：2013-06-24

Applicant: UNITED TECHNOLOGIES CORP

Inventor： WILLEY LAWRENCE J ,  GLEINER MATTHEW S ,  DEIBEL RUSSELL

IPC: F02C7/12 ,  F01D9/04 ,  F01D25/12 ,  F02K3/00

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.

公开(公告)号：EP3086893A4

公开(公告)日：2017-08-23

申请号：EP14883263

申请日：2014-11-20

Applicant: UNITED TECHNOLOGIES CORP

Inventor： TAFFET STEVEN ,  DONNELL BRANDON S ,  NADEAU DANIEL C ,  DEIBEL RUSSELL ,  QUACH SAN

IPC: B22C9/10 ,  B22C7/02 ,  B22C9/04 ,  B22C9/22 ,  B22C9/24 ,  F01D5/18 ,  F01D9/04

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: 失芯模具部件包括第一腿部和第二腿部，第二腿部具有连接第一腿部和第二腿部的多个交叉部件。 多个交叉部件包括彼此间隔开的最外侧交叉部件。 第一支腿和第二支腿中的每一个的相邻末端以及第二交叉构件彼此间隔得比最外侧交叉构件更靠近彼此。 中央交叉部件在第一腿和第二腿之间以及第二交叉部件之间延伸。 最外面的跨接构件延伸第一横截面区域。 第二交叉部件延伸第二横截面区域，并且中央交叉部件延伸第三横截面区域。 第一横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。 燃气涡轮发动机和部件也被公开。

公开(公告)号：EP3049640A4

公开(公告)日：2017-04-26

申请号：EP14845261

申请日：2014-08-26

Applicant: UNITED TECHNOLOGIES CORP

Inventor： LEWIS SCOTT D ,  MONGILLO JR DOMINIC J ,  ZELESKY MARK F ,  TELLER BRET M ,  DEIBEL RUSSELL ,  GLEINER MATTHEW S

IPC: F01D25/12 ,  F01D11/08 ,  F02C7/12 ,  F02C7/28 ,  F04D29/08 ,  F04D29/58

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: 除了别的以外，根据本公开的示例性方面的叶片包括从边缘面延伸并且在间隔开的侧面与从平台向外延伸的翼面之间的平台。 平台包括在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。