公开(公告)号：NO20060939A

公开(公告)日：2006-10-30

申请号：NO20060939

申请日：2006-02-27

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SADIL ANDREAS ,  ENGLEHART JOSEPH F

IPC: F02C7/057 ,  F02K1/16

CPC classification number: F01D17/105 ,  F01D17/141 ,  F02C7/12 ,  F05D2250/411 ,  F05D2260/20 ,  Y02T50/675

公开(公告)号：EP2901082A4

公开(公告)日：2015-10-14

申请号：EP13842492

申请日：2013-09-27

Applicant: UNITED TECHNOLOGIES CORP

Inventor： NIGGEMEIER CHRIS ,  MOSLEY JOHN H ,  SADIL ANDREAS ,  BLUME KARL D

IPC: F23R3/50 ,  F01D9/06 ,  F01D25/28 ,  F02C3/13 ,  F02C6/08 ,  F02C7/00 ,  F23R3/02

CPC classification number: F02C7/20 ,  F01D9/065 ,  F01D25/24 ,  F01D25/28 ,  F02C3/13 ,  F02C6/08 ,  F02C7/04 ,  F23R3/02 ,  F23R3/50

Abstract: An inner diffuser case for use in a combustor of a gas turbine engine includes a multiple of struts across an annular flow path between an outer shroud and an inner shroud, at least one of the multiple of struts is an open strut.

公开(公告)号：EP3052785A4

公开(公告)日：2016-11-02

申请号：EP14851349

申请日：2014-10-01

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SADIL ANDREAS ,  TRINKS STEVEN W ,  JAUSE JONATHAN M

IPC: F02C7/22 ,  F23R3/28

CPC classification number: F23R3/286 ,  F02C7/2365 ,  F23R3/14 ,  F23R2900/00018

Abstract: A swirler is provided for a turbine engine. The swirler includes a swirler housing and a swirler nozzle that is attached to the housing. The housing defines a first inlet and a second inlet. The housing and the nozzle form an inner passage and an outer passage. The inner passage is radially within the nozzle and coupled with the first inlet. The outer passage is radially between the housing and the nozzle and coupled with the second inlet.

Abstract translation: 为涡轮发动机提供旋流器。 旋流器包括旋流器壳体和附接到壳体的旋流器喷嘴。 壳体限定第一入口和第二入口。 壳体和喷嘴形成内部通道和外部通道。 内部通道径向地在喷嘴内并与第一入口连接。 外部通道在壳体和喷嘴之间径向地与第二入口连接。

公开(公告)号：EP3027869A4

公开(公告)日：2016-07-27

申请号：EP14832080

申请日：2014-07-22

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SADIL ANDREAS ,  JAUSE JONATHAN M ,  BROULIDAKIS ALEXANDER

IPC: F02C7/24 ,  F02C7/12 ,  F23R3/42

CPC classification number: F23R3/007 ,  F02C7/18 ,  F02C7/24 ,  F05D2220/32 ,  F05D2240/35 ,  F05D2260/30 ,  F16B21/16 ,  F23R3/10 ,  F23R3/50 ,  F23R3/60 ,  Y02T50/675

Abstract: A turbine engine includes a compressor section, a combustor in fluid communication with the compressor section, and a turbine section in fluid communication with the combustor section. The combustor includes a combustor region defined by at least one bulkhead panel and at least one heat shielding panel inside the combustor region. The at least one heat shielding panel is connected to the bulkhead panel via at least one cooled fastener.