公开(公告)号：EP3074606A4

公开(公告)日：2017-11-29

申请号：EP14879571

申请日：2014-11-05

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SLAVENS THOMAS N ,  SNYDER BROOKS E

IPC: F01D5/18

CPC classification number: F01D5/187 ,  F01D5/18 ,  F01D5/186 ,  F01D9/02 ,  F01D25/12 ,  F05D2220/32 ,  F05D2230/31 ,  F05D2260/20 ,  F05D2260/201 ,  F05D2260/202 ,  Y02T50/673 ,  Y02T50/676

Abstract: A gas turbine engine airfoil includes an airfoil structure including an exterior surface that is provided by an exterior wall that has a leading edge. A radially extending interior wall within the airfoil structure separates first and second radial cooling passages. The first cooling passage is arranged near the leading edge. A radially extending trench is in the leading edge. An impingement hole is provided in the interior wall and is configured to direct a cooling fluid from the second cooling passage to the first cooling passage and onto the exterior wall at the leading edge.

公开(公告)号：EP3090129A4

公开(公告)日：2017-11-22

申请号：EP14871835

申请日：2014-11-05

Applicant: UNITED TECHNOLOGIES CORP

Inventor： AUXIER JAMES T ,  SLAVENS THOMAS N ,  DONNELL BRANDON S ,  GIRMA YAFET

IPC: F01D5/18 ,  F01D5/20 ,  F02C7/18

CPC classification number: F01D5/186 ,  F01D5/187 ,  F01D5/20 ,  F01D9/02 ,  F02C3/04 ,  F02C7/18 ,  F05D2220/32 ,  F05D2240/303 ,  F05D2240/305 ,  F05D2240/306 ,  F05D2240/307 ,  F05D2240/35 ,  F05D2250/71 ,  F05D2260/202 ,  Y02T50/676

Abstract: In a featured embodiment, a gas turbine engine component comprises an airfoil having a leading edge, a trailing edge, and pressure and suction side walls extending from the leading edge to the trailing edge. The airfoil extends from a base to a tip. A shelf is formed in the tip, and extends from the pressure side wall, around the leading edge, to the suction side wall.

公开(公告)号：EP3105425A4

公开(公告)日：2017-09-13

申请号：EP15748674

申请日：2015-01-26

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SLAVENS THOMAS N ,  SNYDER BROOKS E

IPC: F01D25/12 ,  F01D5/18

CPC classification number: F01D5/187 ,  F01D9/02 ,  F01D11/08 ,  F01D25/12 ,  F01D25/30 ,  F05D2220/32 ,  F05D2230/211 ,  F05D2240/35 ,  F05D2260/204 ,  F23R3/002 ,  Y02T50/676

Abstract: A component according to an exemplary aspect of the present disclosure includes, among other things, a pedestal that traverses a flow channel disposed between a first wall and a second wall. The pedestal includes at least one interior bore configured to communicate a cooling fluid inside of the pedestal.

Abstract translation: 除了别的之外，根据本公开的示例性方面的部件包括穿过布置在第一壁和第二壁之间的流动通道的基座。 该基座包括至少一个内孔，该至少一个内孔被构造成将基座内的冷却流体连通。

公开(公告)号：EP3090145A4

公开(公告)日：2017-09-13

申请号：EP14863499

申请日：2014-11-05

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SNYDER BROOKS E ,  SLAVENS THOMAS N ,  LORICCO NICHOLAS M ,  AUXIER JAMES T

IPC: F01D25/12 ,  F01D5/18 ,  F02C7/18

CPC classification number: F01D5/187 ,  F01D5/181 ,  F01D5/182 ,  F01D5/186 ,  F05D2240/127 ,  F05D2260/2212

Abstract: A gas turbine engine component includes opposing walls that provide an interior cooling passage. One of the walls has a turbulator with a hook that is enclosed within the walls.

Abstract translation: 燃气涡轮发动机部件包括提供内部冷却通道的相对壁。 其中一面墙壁上有一个带钩的湍流器。

公开(公告)号：EP3068975A4

公开(公告)日：2017-06-28

申请号：EP14860261

申请日：2014-10-10

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SNYDER BROOKS E ,  SLAVENS THOMAS N

IPC: F01D5/20 ,  B22F5/04 ,  B22F7/08

CPC classification number: F01D5/187 ,  B22D25/02 ,  B22F3/1055 ,  B22F5/04 ,  B22F7/08 ,  B23K15/0086 ,  B23K26/342 ,  B33Y10/00 ,  B33Y80/00 ,  F01D5/20 ,  F05D2220/32 ,  F05D2230/211 ,  F05D2230/22 ,  F05D2230/31 ,  F05D2240/307 ,  F05D2250/10 ,  F05D2260/201 ,  F05D2260/202 ,  Y02P10/295

Abstract: A gas turbine engine component includes a structure having a surface configured to be exposed to a hot working fluid. The surface includes a recessed pocket that is circumscribed by an overhang. At least one cooling groove is provided by the overhang.

Abstract translation: 燃气涡轮发动机部件包括具有构造成暴露于热工作流体的表面的结构。 该表面包括一个由悬垂物包围的凹穴。 突出部分提供至少一个冷却槽。

公开(公告)号：EP3025030A4

公开(公告)日：2017-03-15

申请号：EP14828912

申请日：2014-07-24

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SLAVENS THOMAS N ,  MOORE SASHA M ,  LORICCO NICHOLAS M

IPC: F01D11/00 ,  F01D9/02 ,  F02C7/28 ,  F04D29/08 ,  F16J15/06 ,  F16J15/08

CPC classification number: F01D11/008 ,  F01D11/006 ,  F04D29/083 ,  F04D29/542 ,  F05D2220/32 ,  F05D2240/55 ,  F05D2250/75 ,  F16J15/06 ,  F16J15/062 ,  F16J15/0887

Abstract: This disclosure relates to a gas turbine engine including a first engine component and a second engine component. The first engine component has a mate face adjacent a mate face of the second engine component. The engine further includes a seal provided between the mate face of the first engine component and the mate face of the second engine component. The seal includes least one trough.

Abstract translation: 本公开涉及一种包括第一发动机部件和第二发动机部件的燃气涡轮发动机。 第一发动机部件具有邻近第二发动机部件的配合面的配合面。 发动机还包括设置在第一发动机部件的配合面与第二发动机部件的配合面之间的密封件。 密封件包括至少一个槽。

公开(公告)号：EP3094411A4

公开(公告)日：2017-01-25

申请号：EP15737134

申请日：2015-01-15

Applicant: UNITED TECHNOLOGIES CORP

Inventor： MARTIN THOMAS J ,  STAROSELSKY ALEXANDER ,  MIRONETS SERGEY ,  SLAVENS THOMAS N ,  SNYDER BROOKS E

IPC: B03B4/00 ,  B01F5/06 ,  B07B4/02 ,  B07B7/01 ,  B07B7/08 ,  B07B7/083 ,  B07B13/04 ,  B22F3/105 ,  B23K15/00 ,  B23K26/342 ,  B29C67/00 ,  B29K105/00

CPC classification number: B07B7/08 ,  B07B4/025 ,  B07B7/083 ,  B07B13/04 ,  B22F3/1055 ,  B22F2003/1056 ,  B22F2003/1059 ,  B23K15/0086 ,  B23K26/342 ,  B29C64/153 ,  B29C64/20 ,  B29C64/35 ,  B29K2105/251 ,  B33Y10/00 ,  B33Y30/00 ,  B33Y40/00 ,  Y02P10/295

Abstract: A aerodynamic particle separator for an Additive Manufacturing System (AMS) has an air supply device to entrain a mixed powder in an airstream flowing through a housing. Each particle in the mixed powder is imparted with a momentum dependent upon the particle weight and size. Utilizing this momentum characteristic, the heavier particles are capable of crossing streamlines of the airstream at a bend portion of the housing and the lighter particles generally stay within the streamlines. Utilizing this dynamic characteristic, the particles of specific weight ranges are collected through respective offtake holes in the housing and controllably fed to a spreader of the AMS.

公开(公告)号：EP2954168A4

公开(公告)日：2016-12-21

申请号：EP14787682

申请日：2014-01-31

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BLAKE MOSHESHE CAMARA-KHARY ,  OSBORNE LISA K ,  SLAVENS THOMAS N

IPC: F01D5/14 ,  F01D5/18 ,  F01D25/08 ,  F02C7/12 ,  F04D29/38 ,  F04D29/58

CPC classification number: F01D5/141 ,  F01D5/18 ,  F01D5/181 ,  F01D5/187 ,  F01D9/065 ,  F01D25/08 ,  F05D2240/11 ,  F05D2240/127 ,  F05D2250/71 ,  F05D2260/2212 ,  F05D2260/22141

Abstract: A component for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a wall that forms a portion of an outer periphery of at least one cavity and at least one curved turbulator that extends from said wall.

公开(公告)号：EP2971567A4

公开(公告)日：2016-11-09

申请号：EP14768748

申请日：2014-03-11

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SLAVENS THOMAS N ,  ZELESKY MARK ,  BLAKE MOSHESHE CAMARA-KHARY

IPC: B23P15/04 ,  F01D5/14 ,  F01D9/04

CPC classification number: F01D5/147 ,  B22F3/1055 ,  B22F5/04 ,  B22F7/06 ,  B22F7/062 ,  B22F7/08 ,  B23K1/0018 ,  B23K31/02 ,  B23K2201/001 ,  B23P15/04 ,  F01D9/041 ,  F01D9/044 ,  F05D2220/32 ,  F05D2230/236 ,  F05D2230/237 ,  F05D2230/60 ,  F05D2300/175 ,  F05D2300/605 ,  F05D2300/606 ,  F05D2300/607 ,  Y02P10/295

公开(公告)号：EP3039269A4

公开(公告)日：2016-09-07

申请号：EP14838947

申请日：2014-08-29

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SNYDER BROOKS E ,  SLAVENS THOMAS N ,  BLAKE MOSHESHE CAMARA-KHARY

IPC: F02C7/28 ,  F01D11/00 ,  F04D29/08 ,  F16J15/08

CPC classification number: F01D11/20 ,  F01D5/12 ,  F01D5/22 ,  F01D9/04 ,  F01D9/041 ,  F01D11/005 ,  F01D11/008 ,  F01D25/24 ,  F05D2220/32 ,  F05D2230/60 ,  F05D2240/11 ,  F05D2240/57 ,  F05D2250/71 ,  F05D2250/75 ,  F05D2270/303 ,  F05D2270/306 ,  F16J15/0887

Abstract: One exemplary embodiment of this disclosure relates to a gas turbine engine including a first engine component and a second engine component. The first engine component has a mate face adjacent a mate face of the second engine component. The engine further includes a seal between the mate face of the first engine component and the mate face of the second engine component. The seal establishes three points of contact with each mate face in at least one condition.

Abstract translation: 本公开的一个示例性实施例涉及包括第一发动机部件和第二发动机部件的燃气涡轮发动机。 第一发动机部件具有邻近第二发动机部件的配合面的配合面。 发动机还包括在第一发动机部件的配合面和第二发动机部件的配合面之间的密封。 密封件在至少一个条件下与每个配合面建立三个接触点。