JPH09112205A5 - - Google Patents

Info

Publication number
JPH09112205A5
JPH09112205A5 JP1996281569A JP28156996A JPH09112205A5 JP H09112205 A5 JPH09112205 A5 JP H09112205A5 JP 1996281569 A JP1996281569 A JP 1996281569A JP 28156996 A JP28156996 A JP 28156996A JP H09112205 A5 JPH09112205 A5 JP H09112205A5
Authority
JP
Japan
Prior art keywords
support
disposed
outer periphery
vane
aft
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
JP1996281569A
Other languages
English (en)
Japanese (ja)
Other versions
JPH09112205A (ja
Filing date
Publication date
Priority claimed from US08/541,854 external-priority patent/US5645397A/en
Application filed filed Critical
Publication of JPH09112205A publication Critical patent/JPH09112205A/ja
Publication of JPH09112205A5 publication Critical patent/JPH09112205A5/ja
Ceased legal-status Critical Current

Links

JP8281569A 1995-10-10 1996-10-04 ガスタービンエンジン用静翼装置 Ceased JPH09112205A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/541,854 US5645397A (en) 1995-10-10 1995-10-10 Turbine vane assembly with multiple passage cooled vanes
US08/541,854 1995-10-10

Publications (2)

Publication Number Publication Date
JPH09112205A JPH09112205A (ja) 1997-04-28
JPH09112205A5 true JPH09112205A5 (enExample) 2004-10-14

Family

ID=24161366

Family Applications (1)

Application Number Title Priority Date Filing Date
JP8281569A Ceased JPH09112205A (ja) 1995-10-10 1996-10-04 ガスタービンエンジン用静翼装置

Country Status (5)

Country Link
US (1) US5645397A (enExample)
EP (1) EP0768448B1 (enExample)
JP (1) JPH09112205A (enExample)
KR (1) KR100456491B1 (enExample)
DE (1) DE69613307T2 (enExample)

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WO2009016744A1 (ja) * 2007-07-31 2009-02-05 Mitsubishi Heavy Industries, Ltd. タービン用翼
US8197209B2 (en) * 2007-12-19 2012-06-12 United Technologies Corp. Systems and methods involving variable throat area vanes
US8016547B2 (en) * 2008-01-22 2011-09-13 United Technologies Corporation Radial inner diameter metering plate
US8257015B2 (en) * 2008-02-14 2012-09-04 General Electric Company Apparatus for cooling rotary components within a steam turbine
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US8096772B2 (en) * 2009-03-20 2012-01-17 Siemens Energy, Inc. Turbine vane for a gas turbine engine having serpentine cooling channels within the inner endwall
CN102224322B (zh) 2009-05-11 2013-08-14 三菱重工业株式会社 涡轮静叶及燃气轮机
JP4841678B2 (ja) * 2010-04-15 2011-12-21 川崎重工業株式会社 ガスタービンのタービン静翼
US8858159B2 (en) 2011-10-28 2014-10-14 United Technologies Corporation Gas turbine engine component having wavy cooling channels with pedestals
EP2626519A1 (en) 2012-02-09 2013-08-14 Siemens Aktiengesellschaft Turbine assembly, corresponding impingement cooling tube and gas turbine engine
US9435259B2 (en) 2012-02-27 2016-09-06 United Technologies Corporation Gas turbine engine cooling system
US9347374B2 (en) 2012-02-27 2016-05-24 United Technologies Corporation Gas turbine engine buffer cooling system
US8863531B2 (en) * 2012-07-02 2014-10-21 United Technologies Corporation Cooling apparatus for a mid-turbine frame
US20140003920A1 (en) * 2012-07-02 2014-01-02 United Technologies Corporation Flow metering anti-rotation outer diameter (od) hex nut
EP2900968B1 (en) * 2012-09-28 2018-10-31 United Technologies Corporation Split-zone flow metering t-tube
GB2524443B (en) * 2012-12-31 2020-02-12 United Technologies Corp Turbine exhaust case multi-piece frame
JP6249499B2 (ja) * 2012-12-31 2017-12-20 ユナイテッド テクノロジーズ コーポレイションUnited Technologies Corporation タービン排気ケースのマルチピース型フレーム
US10132193B2 (en) 2013-08-19 2018-11-20 United Technologies Corporation Gas turbine engine duct assembly
US10240470B2 (en) * 2013-08-30 2019-03-26 United Technologies Corporation Baffle for gas turbine engine vane
US9927123B2 (en) * 2013-10-24 2018-03-27 United Technologies Corporation Fluid transport system having divided transport tube
US10094229B2 (en) 2014-07-28 2018-10-09 United Technologies Corporation Cooling system of a stator assembly for a gas turbine engine having a variable cooling flow mechanism and method of operation
US10443498B2 (en) 2014-08-15 2019-10-15 United Technologies Corporation Gas turbine engine cooling fluid metering system
US10436113B2 (en) * 2014-09-19 2019-10-08 United Technologies Corporation Plate for metering flow
US10767562B2 (en) * 2014-12-10 2020-09-08 Pratt & Whitney Canada Corp. Modulated cooled P3 air for impeller
US9938842B2 (en) 2015-01-20 2018-04-10 United Technologies Corporation Leakage air systems for turbomachines
EP3124743B1 (en) 2015-07-28 2021-04-28 Rolls-Royce Deutschland Ltd & Co KG Nozzle guide vane and method for forming a nozzle guide vane
US10107126B2 (en) * 2015-08-19 2018-10-23 United Technologies Corporation Non-contact seal assembly for rotational equipment
US10100736B2 (en) * 2015-10-30 2018-10-16 General Electric Company Gas turbine engine sump heat exchanger
US10030538B2 (en) * 2015-11-05 2018-07-24 General Electric Company Gas turbine engine with a vane having a cooling air turning nozzle
US10233842B2 (en) 2016-01-08 2019-03-19 United Technologies Corporation Tangential on-board injectors for gas turbine engines
CA2954785A1 (en) * 2016-01-25 2017-07-25 Rolls-Royce Corporation Forward flowing serpentine vane
US10513947B2 (en) * 2017-06-05 2019-12-24 United Technologies Corporation Adjustable flow split platform cooling for gas turbine engine
US11021962B2 (en) * 2018-08-22 2021-06-01 Raytheon Technologies Corporation Turbulent air reducer for a gas turbine engine
KR101950922B1 (ko) 2018-09-06 2019-02-21 터보파워텍(주) 가스터빈용 베인조립체
FR3087839B1 (fr) * 2018-10-30 2020-10-23 Safran Aircraft Engines Turbine
CN110043328B (zh) * 2018-12-17 2021-10-22 中国航发沈阳发动机研究所 一种冷却式变几何低压涡轮导向叶片
KR102175198B1 (ko) * 2019-05-28 2020-11-05 두산중공업 주식회사 터빈 스테이터, 터빈 및 이를 포함하는 가스터빈
KR102212880B1 (ko) * 2019-05-31 2021-02-05 두산중공업 주식회사 가스터빈
US11788470B2 (en) 2021-03-01 2023-10-17 General Electric Company Gas turbine engine thermal management
US11603770B2 (en) 2021-04-21 2023-03-14 Raytheon Technologies Corporation Vane assembly with integrated nozzle tube
US12410752B2 (en) 2021-09-23 2025-09-09 General Electric Company System and method of detecting an airflow fault condition
US11702958B2 (en) 2021-09-23 2023-07-18 General Electric Company System and method of regulating thermal transport bus pressure
US12215606B2 (en) * 2022-05-27 2025-02-04 Rtx Corporation Turbine engine with TOBI supporting vanes

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