JP2011027109A5 - - Google Patents

Download PDF

Info

Publication number
JP2011027109A5
JP2011027109A5 JP2010165415A JP2010165415A JP2011027109A5 JP 2011027109 A5 JP2011027109 A5 JP 2011027109A5 JP 2010165415 A JP2010165415 A JP 2010165415A JP 2010165415 A JP2010165415 A JP 2010165415A JP 2011027109 A5 JP2011027109 A5 JP 2011027109A5
Authority
JP
Japan
Prior art keywords
coolant
turbine
radial
hook
insert
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.)
Granted
Application number
JP2010165415A
Other languages
English (en)
Japanese (ja)
Other versions
JP2011027109A (ja
JP5457965B2 (ja
Filing date
Publication date
Priority claimed from US12/511,005 external-priority patent/US8342798B2/en
Application filed filed Critical
Publication of JP2011027109A publication Critical patent/JP2011027109A/ja
Publication of JP2011027109A5 publication Critical patent/JP2011027109A5/ja
Application granted granted Critical
Publication of JP5457965B2 publication Critical patent/JP5457965B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

JP2010165415A 2009-07-28 2010-07-23 回転機械におけるクリアランス制御用のシステム及び方法 Active JP5457965B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/511,005 2009-07-28
US12/511,005 US8342798B2 (en) 2009-07-28 2009-07-28 System and method for clearance control in a rotary machine

Publications (3)

Publication Number Publication Date
JP2011027109A JP2011027109A (ja) 2011-02-10
JP2011027109A5 true JP2011027109A5 (enExample) 2013-02-14
JP5457965B2 JP5457965B2 (ja) 2014-04-02

Family

ID=43402901

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2010165415A Active JP5457965B2 (ja) 2009-07-28 2010-07-23 回転機械におけるクリアランス制御用のシステム及び方法

Country Status (5)

Country Link
US (1) US8342798B2 (enExample)
JP (1) JP5457965B2 (enExample)
CN (1) CN101985889B (enExample)
CH (1) CH701542B8 (enExample)
DE (1) DE102010036494A1 (enExample)

Families Citing this family (48)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8267649B2 (en) * 2009-05-15 2012-09-18 General Electric Company Coupling for rotary components
US8439636B1 (en) * 2009-10-20 2013-05-14 Florida Turbine Technologies, Inc. Turbine blade outer air seal
US8662824B2 (en) * 2010-01-28 2014-03-04 Pratt & Whitney Canada Corp. Rotor containment structure for gas turbine engine
US8668431B2 (en) * 2010-03-29 2014-03-11 United Technologies Corporation Seal clearance control on non-cowled gas turbine engines
FR2971291B1 (fr) 2011-02-08 2013-02-22 Snecma Unite de commande et procede de pilotage de jeu en sommet d'aubes
FR2971543B1 (fr) * 2011-02-11 2013-03-08 Snecma Procede de pilotage de jeu en sommet d'aubes de rotor de turbine
DE112012000789T5 (de) * 2011-03-14 2013-11-07 Borgwarner Inc. Turbinengehäuse eines Abgasturboladers
US8973373B2 (en) * 2011-10-31 2015-03-10 General Electric Company Active clearance control system and method for gas turbine
JP5650674B2 (ja) * 2012-01-11 2015-01-07 三菱日立パワーシステムズ株式会社 ガスタービンの間隙制御装置、間隙制御方法及び間隙制御装置を備えたガスタービン
US20130251500A1 (en) * 2012-03-23 2013-09-26 Kin-Leung Cheung Gas turbine engine case with heating layer and method
US9719372B2 (en) * 2012-05-01 2017-08-01 General Electric Company Gas turbomachine including a counter-flow cooling system and method
US20130318996A1 (en) * 2012-06-01 2013-12-05 General Electric Company Cooling assembly for a bucket of a turbine system and method of cooling
US9238971B2 (en) * 2012-10-18 2016-01-19 General Electric Company Gas turbine casing thermal control device
US9850780B2 (en) 2012-12-29 2017-12-26 United Technologies Corporation Plate for directing flow and film cooling of components
US9206742B2 (en) * 2012-12-29 2015-12-08 United Technologies Corporation Passages to facilitate a secondary flow between components
JP6265318B2 (ja) * 2013-01-31 2018-01-24 三菱重工業株式会社 クリアランスコントロールシステム、クリアランスコントロール方法、制御装置、プログラム及び記録媒体
US9279339B2 (en) * 2013-03-13 2016-03-08 Siemens Aktiengesellschaft Turbine engine temperature control system with heating element for a gas turbine engine
US9828880B2 (en) * 2013-03-15 2017-11-28 General Electric Company Method and apparatus to improve heat transfer in turbine sections of gas turbines
EP3044427B8 (en) * 2013-09-12 2021-04-07 Raytheon Technologies Corporation Gas turbine engine and corresponding method for regulating blade tip clearance
US9945248B2 (en) 2014-04-01 2018-04-17 United Technologies Corporation Vented tangential on-board injector for a gas turbine engine
US9963994B2 (en) * 2014-04-08 2018-05-08 General Electric Company Method and apparatus for clearance control utilizing fuel heating
JP6492737B2 (ja) * 2015-02-19 2019-04-03 中国電力株式会社 ガスタービン、及びガスタービンの制御方法
US10612408B2 (en) * 2015-05-06 2020-04-07 United Technologies Corporation Control rings
US10316696B2 (en) 2015-05-08 2019-06-11 General Electric Company System and method for improving exhaust energy recovery
US20160326915A1 (en) * 2015-05-08 2016-11-10 General Electric Company System and method for waste heat powered active clearance control
CN106555618B (zh) * 2015-09-30 2019-09-13 中国航发商用航空发动机有限责任公司 燃气轮机的叶尖间隙控制系统及其方法
GB201518641D0 (en) * 2015-10-21 2015-12-02 Rolls Royce Plc A system and method
JP6563312B2 (ja) * 2015-11-05 2019-08-21 川崎重工業株式会社 ガスタービンエンジンの抽気構造
JP6589211B2 (ja) 2015-11-26 2019-10-16 三菱日立パワーシステムズ株式会社 ガスタービン、及びその部品温度調節方法
US10822972B2 (en) 2015-12-08 2020-11-03 General Electric Company Compliant shroud for gas turbine engine clearance control
PL232314B1 (pl) * 2016-05-06 2019-06-28 Gen Electric Maszyna przepływowa zawierająca system regulacji luzu
US10309246B2 (en) 2016-06-07 2019-06-04 General Electric Company Passive clearance control system for gas turbomachine
US10392944B2 (en) 2016-07-12 2019-08-27 General Electric Company Turbomachine component having impingement heat transfer feature, related turbomachine and storage medium
US10605093B2 (en) 2016-07-12 2020-03-31 General Electric Company Heat transfer device and related turbine airfoil
CN106286011A (zh) * 2016-08-11 2017-01-04 南昌航空大学 一种涵道壁面与桨尖间隙可调的涵道风扇
JP6925862B2 (ja) 2017-05-16 2021-08-25 三菱パワー株式会社 ガスタービン、及び翼環部の製造方法
EP3421733B1 (en) * 2017-06-30 2020-02-26 Ansaldo Energia IP UK Limited Vane carrier for a gas turbine plant and gas turbine plant comprising said vane carrier
GB201712025D0 (en) * 2017-07-26 2017-09-06 Rolls Royce Plc Gas turbine engine
FR3073007B1 (fr) * 2017-10-27 2019-09-27 Safran Aircraft Engines Dispositif de maintien d'un tube de refroidissement pour carter de turbomachine
US10941706B2 (en) 2018-02-13 2021-03-09 General Electric Company Closed cycle heat engine for a gas turbine engine
US11143104B2 (en) 2018-02-20 2021-10-12 General Electric Company Thermal management system
EP3540182A1 (de) * 2018-03-14 2019-09-18 Siemens Aktiengesellschaft Verfahren zur steuerung einer spaltminimierung einer gasturbine
US11015534B2 (en) 2018-11-28 2021-05-25 General Electric Company Thermal management system
FR3099798B1 (fr) * 2019-08-09 2021-12-03 Safran Aircraft Engines Ensemble pour une turbine de turbomachine
US11319833B2 (en) * 2020-04-24 2022-05-03 General Electric Company Fan case with crack-arresting backsheet structure and removable containment cartridge
CN114278401B (zh) * 2020-09-28 2024-04-26 中国航发商用航空发动机有限责任公司 涡轮式发动机的涡轮机匣和涡轮式发动机
US11434777B2 (en) 2020-12-18 2022-09-06 General Electric Company Turbomachine clearance control using magnetically responsive particles
DE102023121051A1 (de) * 2023-08-08 2025-02-13 MTU Aero Engines AG Kühlbares Turbinenmodul und erwärmbares Verdichtermodul für eine Strömungsmaschine, sowie Strömungsmaschine

Family Cites Families (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5601402A (en) 1986-06-06 1997-02-11 The United States Of America As Represented By The Secretary Of The Air Force Turbo machine shroud-to-rotor blade dynamic clearance control
GB8903000D0 (en) 1989-02-10 1989-03-30 Rolls Royce Plc A blade tip clearance control arrangement for a gas turbine engine
US5076050A (en) 1989-06-23 1991-12-31 United Technologies Corporation Thermal clearance control method for gas turbine engine
FR2653171B1 (fr) * 1989-10-18 1991-12-27 Snecma Carter de compresseur de turbomachine muni d'un dispositif de pilotage de son diametre interne.
US5056988A (en) 1990-02-12 1991-10-15 General Electric Company Blade tip clearance control apparatus using shroud segment position modulation
US5035573A (en) 1990-03-21 1991-07-30 General Electric Company Blade tip clearance control apparatus with shroud segment position adjustment by unison ring movement
US5281085A (en) * 1990-12-21 1994-01-25 General Electric Company Clearance control system for separately expanding or contracting individual portions of an annular shroud
US5219268A (en) * 1992-03-06 1993-06-15 General Electric Company Gas turbine engine case thermal control flange
US5399066A (en) 1993-09-30 1995-03-21 General Electric Company Integral clearance control impingement manifold and environmental shield
US5403158A (en) 1993-12-23 1995-04-04 United Technologies Corporation Aerodynamic tip sealing for rotor blades
US5685693A (en) 1995-03-31 1997-11-11 General Electric Co. Removable inner turbine shell with bucket tip clearance control
US5593277A (en) * 1995-06-06 1997-01-14 General Electric Company Smart turbine shroud
US6116852A (en) 1997-12-11 2000-09-12 Pratt & Whitney Canada Corp. Turbine passive thermal valve for improved tip clearance control
DE19756734A1 (de) 1997-12-19 1999-06-24 Bmw Rolls Royce Gmbh Passives Spalthaltungssystem einer Gasturbine
US6368054B1 (en) 1999-12-14 2002-04-09 Pratt & Whitney Canada Corp. Split ring for tip clearance control
US6435823B1 (en) 2000-12-08 2002-08-20 General Electric Company Bucket tip clearance control system
FR2819010B1 (fr) * 2001-01-04 2004-05-28 Snecma Moteurs Secteur d'entretoise de support d'anneau de stator de la turbine haute pression d'une turbomachine avec rattrapage de jeux
US6702550B2 (en) * 2002-01-16 2004-03-09 General Electric Company Turbine shroud segment and shroud assembly
GB2388407B (en) 2002-05-10 2005-10-26 Rolls Royce Plc Gas turbine blade tip clearance control structure
US6935836B2 (en) 2002-06-05 2005-08-30 Allison Advanced Development Company Compressor casing with passive tip clearance control and endwall ovalization control
FR2858652B1 (fr) * 2003-08-06 2006-02-10 Snecma Moteurs Dispositif de controle de jeu dans une turbine a gaz
US7125223B2 (en) 2003-09-30 2006-10-24 General Electric Company Method and apparatus for turbomachine active clearance control
US7079957B2 (en) 2003-12-30 2006-07-18 General Electric Company Method and system for active tip clearance control in turbines
FR2865237B1 (fr) 2004-01-16 2006-03-10 Snecma Moteurs Perfectionnements apportes aux dispositifs de controle de jeu dans une turbine a gaz
US7722310B2 (en) 2004-12-17 2010-05-25 General Electric Company System and method for measuring clearance between two objects
US7434402B2 (en) * 2005-03-29 2008-10-14 Siemens Power Generation, Inc. System for actively controlling compressor clearances
US7333913B2 (en) 2005-06-27 2008-02-19 General Electric Company Clearance measurement system and method of operation
US7652489B2 (en) 2005-12-06 2010-01-26 General Electric Company Multi-range clearance measurement system and method of operation
US7597537B2 (en) 2005-12-16 2009-10-06 General Electric Company Thermal control of gas turbine engine rings for active clearance control
US8121813B2 (en) 2009-01-28 2012-02-21 General Electric Company System and method for clearance estimation between two objects
US8177476B2 (en) 2009-03-25 2012-05-15 General Electric Company Method and apparatus for clearance control
US8186945B2 (en) 2009-05-26 2012-05-29 General Electric Company System and method for clearance control

Similar Documents

Publication Publication Date Title
JP2011027109A5 (enExample)
JP5433560B2 (ja) タービンスクロール部構造
US9347460B2 (en) Rotary machine
CN106677903B (zh) 肋板控涡结构、旋转盘腔系统、燃气轮机
JP5145117B2 (ja) 圧縮機のハウジング
CN104246170B (zh) 带有集成隔热屏的涡轮增压器轴承壳体
CN102628375B (zh) 涡轮发动机的旋转部件和形成旋转部件的方法
CN103782011A (zh) 用于流体机械的冷却装置
JP2013139809A5 (enExample)
JP2012122398A5 (enExample)
CN107407192B (zh) 用于涡轮增压器的轴承
CN103097664B (zh) 用于燃气轮机的燃气轮机转子、压缩机转子轴及涡轮转子轴
CN102959183A (zh) 用于涡轮机盘的组合式密封和平衡装置
US10890109B2 (en) Turbocharger
JP6120003B2 (ja) ターボチャージャの軸受構造
KR101246337B1 (ko) 축 냉각장치
US9803495B2 (en) Assembly
JP2010127279A (ja) エンジン構成要素を冷却するための方法及びシステム
JP6110035B2 (ja) 熱ターボ機械のロータ
JP2012067746A5 (enExample)
JP6317352B2 (ja) タービンホイール
WO2017072843A1 (ja) 回転機械
CN102216570A (zh) 燃气涡轮机
CN201528230U (zh) 一种发电机及其转轴
US9382807B2 (en) Non-axisymmetric rim cavity features to improve sealing efficiencies