公开(公告)号：WO2014175937A3

公开(公告)日：2014-12-31

申请号：PCT/US2014013981

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 ,  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.

Abstract translation: 根据本公开的示例性方面的用于燃气涡轮发动机的部件尤其包括形成至少一个空腔的外周的一部分的壁和从所述壁延伸的至少一个弯曲的湍流器。

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。