公开(公告)号：EP2900983A4

公开(公告)日：2016-04-06

申请号：EP13866016

申请日：2013-09-25

Applicant: UNITED TECHNOLOGIES CORP

Inventor： CUNHA FRANK J ,  ERBAS-SEN NURHAK

IPC: F02C9/22 ,  F01D9/02 ,  F01D17/16 ,  F02C3/14 ,  F02C7/20 ,  F23R3/04 ,  F23R3/16 ,  F23R3/28

CPC classification number: F23R3/286 ,  F01D9/023 ,  F01D9/065 ,  F05D2260/202 ,  F23R3/04 ,  F23R3/16 ,  F23R3/26 ,  F23R2900/00018 ,  F23R2900/03044 ,  Y02T50/676

Abstract: A combustor section is provided for a gas turbine engine. The combustor section may include an outer liner panel, an inner liner panel and a bulkhead, which is arranged with the outer and the inner liner panels to form an annular combustion chamber. The combustor section may also include a swirler assembly and a combustor vane. The swirler assembly may be configured with the bulkhead. The combustor vane may extend at least partially into said combustion chamber, wherein the combustor vane is circumferentially aligned with the swirler assembly.

公开(公告)号：EP2932070A4

公开(公告)日：2015-12-23

申请号：EP13874386

申请日：2013-12-16

Applicant: UNITED TECHNOLOGIES CORP

Inventor： ERBAS-SEN NURHAK ,  HOKE JAMES B ,  CUNHA FRANK J

IPC: F02C7/24 ,  F02C7/12 ,  F23R3/00 ,  F23R3/06

CPC classification number: F23R3/002 ,  F23R3/06 ,  F23R2900/03042 ,  Y02T50/675

Abstract: A heat shield for a gas turbine engine includes a hot side with one or more raised features that extend therefrom.