公开(公告)号：CA2581033A1

公开(公告)日：2008-02-10

申请号：CA2581033

申请日：2007-03-07

Applicant: UNITED TECHNOLOGIES CORP

Inventor： LEVASSEUR GLENN N ,  SHI JUN ,  BUTLER SHAOLUO L ,  GREEN KEVIN E ,  SRINIVASAN GAJAWALLI V

IPC: F01D5/18 ,  F01D5/28 ,  F01D9/02 ,  F01D25/12

Abstract: A shroud suitable for use in a gas turbine engine exhibits substantially uniform thermal growth.

公开(公告)号：CA2578648A1

公开(公告)日：2008-02-10

申请号：CA2578648

申请日：2007-02-15

Applicant: UNITED TECHNOLOGIES CORP

Inventor： GREEN KEVIN E ,  SHI JUN ,  BUTLER SHAOLUO L

IPC: F01D9/02 ,  F01D5/28

Abstract: A ceramic shroud assembly suitable for use in a gas turbine engine comprises a metal clamp ring shrink fitted around a ceramic shroud ring and an insulatin g and compliant interlayer. The interlayer is positioned between the metal clamp ring and th e ceramic shroud ring.

公开(公告)号：SG11201405495PA

公开(公告)日：2014-11-27

申请号：SG11201405495P

申请日：2013-02-23

Applicant: UNITED TECHNOLOGIES CORP

Inventor： DAI ZHONGTAO ,  COHEN JEFFREY M ,  GREEN KEVIN E

IPC: F23R3/14 ,  F02C7/22 ,  F02K99/00 ,  F23R3/42

Abstract: A fuel-air premixer for a combustor of a turbine engine includes a central passage along an axis. The central passage is operable to communicate an unswirled airflow. An outer annular passage is located around the axis and includes a multiple of first swirl vanes that are operable to communicate a first swirled airflow in a first direction. An inner annular passage is located around the axis between the central passage and the outer annular passage. The inner annular passage includes a multiple of second swirl vanes that are operable to communicate a second swirled airflow in a second direction different than the first direction.

公开(公告)号：EP2825824A4

公开(公告)日：2015-10-28

申请号：EP13760976

申请日：2013-02-23

Applicant: UNITED TECHNOLOGIES CORP

Inventor： DAI ZHONGTAO ,  COHEN JEFFREY M ,  GREEN KEVIN E

IPC: F23R3/28 ,  F02C7/22 ,  F02K3/00 ,  F02K99/00 ,  F23R3/14 ,  F23R3/42

CPC classification number: F23R3/14 ,  F23R3/28 ,  Y02T50/675

Abstract: A fuel-air premixer for a combustor of a turbine engine includes a central passage along an axis. The central passage is operable to communicate an unswirled airflow. An outer annular passage is located around the axis and includes a multiple of first swirl vanes that are operable to communicate a first swirled airflow in a first direction. An inner annular passage is located around the axis between the central passage and the outer annular passage. The inner annular passage includes a multiple of second swirl vanes that are operable to communicate a second swirled airflow in a second direction different than the first direction.

公开(公告)号：EP2872756A4

公开(公告)日：2015-07-29

申请号：EP13817240

申请日：2013-06-27

Applicant: UNITED TECHNOLOGIES CORP

Inventor： COHEN JEFFREY M ,  DAI ZHONGTAO ,  GREEN KEVIN E

IPC: F02C3/32 ,  F02C7/00 ,  F02C7/22 ,  F23R3/28

CPC classification number: F23R3/28 ,  F23D2900/11101