公开(公告)号：EP3066387A4

公开(公告)日：2016-11-30

申请号：EP14880515

申请日：2014-10-31

Applicant: UNITED TECHNOLOGIES CORP

Inventor： MOURA DENNIS M ,  EASTWOOD JONATHAN J ,  BOULDIN LEE E ,  PACHECO-TOUGAS MONICA

IPC: F23M5/00 ,  F23M5/08 ,  F23R3/04 ,  F23R3/42

CPC classification number: F23R3/002 ,  F23R3/005 ,  F23R3/007 ,  F23R3/045 ,  F23R3/06 ,  F23R2900/03041 ,  F23R2900/03044

Abstract: An assembly for a turbine engine includes a combustor wall. The combustor wall includes a shell, a heat shield and an annular land. The heat shield is attached to the shell. The land extends vertically between the shell and the heat shield. The land extends laterally between a land outer surface and an inner surface, which at least partially defines a quench aperture in the combustor wall. A lateral distance between the land outer surface and the inner surface varies around the quench aperture.

公开(公告)号：EP2904236A4

公开(公告)日：2015-12-09

申请号：EP13843296

申请日：2013-10-04

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BANGERTER JAMES P ,  WILLIAMS ALEXANDER W ,  MULE NICHOLAS ,  PACHECO-TOUGAS MONICA

IPC: F23R3/06 ,  F23R3/10 ,  F23R3/50

CPC classification number: F23R3/06 ,  F23R3/10 ,  F23R3/50 ,  F23R2900/03041 ,  F23R2900/03043 ,  F23R2900/03044 ,  F23R2900/03045 ,  Y02T50/675

Abstract: A liner for a combustor of a turbine engine includes a cooling feature which projects from a backside and an effusion hole that communicates through the liner

公开(公告)号：EP3044439A4

公开(公告)日：2017-05-10

申请号：EP14843869

申请日：2014-08-05

Applicant: UNITED TECHNOLOGIES CORP

Inventor： TU JOHN S ,  BANGERTER JAMES P ,  SZE ROBERT ,  HOKE JAMES B ,  PACHECO-TOUGAS MONICA

IPC: F02C7/12 ,  F02C7/18 ,  F23R3/42

CPC classification number: F23R3/06 ,  F02C7/18 ,  F23R3/002 ,  F23R3/005 ,  F23R2900/03041 ,  F23R2900/03042 ,  F23R2900/03044 ,  Y02T50/675

公开(公告)号：EP3084307A4

公开(公告)日：2016-12-21

申请号：EP14887012

申请日：2014-12-19

Applicant: UNITED TECHNOLOGIES CORP

Inventor： EASTWOOD JONATHAN J ,  MOURA DENNIS M ,  BOULDIN LEE E ,  PACHECO-TOUGAS MONICA

IPC: F23R3/02 ,  F23M5/00 ,  F23R3/04 ,  F23R3/26

CPC classification number: F23R3/06 ,  F23R3/002 ,  F23R3/007 ,  F23R3/60 ,  F23R2900/00012 ,  F23R2900/00017 ,  F23R2900/03041 ,  Y02T50/675

Abstract: A liner panel is provided for use in a combustor of a gas turbine engine. The liner panel includes a major dilution passage having a lip and a first seal boss. The liner panel also includes a minor dilution passage having a second seal boss adjacent the first seal boss.

公开(公告)号：EP3066388A4

公开(公告)日：2016-11-02

申请号：EP14879939

申请日：2014-11-04

Applicant: UNITED TECHNOLOGIES CORP

Inventor： MOURA DENNIS M ,  PACHECO-TOUGAS MONICA ,  EASTWOOD JONATHAN J ,  BOULDIN LEE E

IPC: F23M5/08 ,  F23M5/04 ,  F23R3/00 ,  F23R3/06 ,  F23R3/42

CPC classification number: F23R3/002 ,  F02C7/18 ,  F02C7/24 ,  F05D2220/32 ,  F05D2240/35 ,  F05D2260/202 ,  F23R3/005 ,  F23R3/007 ,  F23R3/04 ,  F23R3/06 ,  F23R2900/03041 ,  F23R2900/03044

公开(公告)号：EP2971668A4

公开(公告)日：2016-03-02

申请号：EP14807114

申请日：2014-03-11

Applicant: UNITED TECHNOLOGIES CORP

Inventor： ERBAS-SEN NURHAK ,  HOKE JAMES B ,  TU JOHN S ,  PACHECO-TOUGAS MONICA

IPC: F02C7/12 ,  F02C3/14 ,  F23M5/04 ,  F23R3/00 ,  F23R3/42

CPC classification number: F23R3/002 ,  F02C7/18 ,  F23R3/005 ,  F23R3/007 ,  F23R3/06 ,  F23R2900/03041 ,  F23R2900/03042 ,  F23R2900/03044 ,  Y02T50/675

Abstract: A liner assembly for a combustor of a gas turbine engine according to one disclosed non-limiting embodiment of the present disclosure includes a grommet with a multiple of grommet cooling passages.

Abstract translation: 根据本公开的一个公开的非限制性实施例的用于燃气涡轮发动机的燃烧器的衬套组件包括具有多个索环冷却通道的索环。