NO912924D0 - Termisk lineaeraktuator for styring av en rotors luftstroemi en gassturbin. - Google Patents
Termisk lineaeraktuator for styring av en rotors luftstroemi en gassturbin.Info
- Publication number
- NO912924D0 NO912924D0 NO912924A NO912924A NO912924D0 NO 912924 D0 NO912924 D0 NO 912924D0 NO 912924 A NO912924 A NO 912924A NO 912924 A NO912924 A NO 912924A NO 912924 D0 NO912924 D0 NO 912924D0
- Authority
- NO
- Norway
- Prior art keywords
- linea
- actuator
- thermal
- air flow
- control
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/107—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with two or more rotors connected by power transmission
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/08—Heating, heat-insulating or cooling means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
- F01D11/16—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means
- F01D11/18—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means using stator or rotor components with predetermined thermal response, e.g. selective insulation, thermal inertia, differential expansion
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Control Of Turbines (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/558,450 US5054996A (en) | 1990-07-27 | 1990-07-27 | Thermal linear actuator for rotor air flow control in a gas turbine |
Publications (2)
Publication Number | Publication Date |
---|---|
NO912924D0 true NO912924D0 (no) | 1991-07-26 |
NO912924L NO912924L (no) | 1992-01-28 |
Family
ID=24229590
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
NO91912924A NO912924L (no) | 1990-07-27 | 1991-07-26 | Termisk lineaeraktuator for styring av en rotors luftstroemi en gassturbin. |
Country Status (6)
Country | Link |
---|---|
US (1) | US5054996A (no) |
EP (1) | EP0468782A3 (no) |
JP (1) | JPH04232335A (no) |
KR (1) | KR920002912A (no) |
CN (1) | CN1058449A (no) |
NO (1) | NO912924L (no) |
Families Citing this family (44)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5271711A (en) * | 1992-05-11 | 1993-12-21 | General Electric Company | Compressor bore cooling manifold |
FR2712029B1 (fr) * | 1993-11-03 | 1995-12-08 | Snecma | Turbomachine pourvue d'un moyen de réchauffage des disques de turbines aux montées en régime. |
DE19531290A1 (de) * | 1995-08-25 | 1997-02-27 | Abb Management Ag | Rotor für thermische Turbomaschinen |
JP3149774B2 (ja) * | 1996-03-19 | 2001-03-26 | 株式会社日立製作所 | ガスタービンロータ |
WO1997049901A1 (de) * | 1996-06-21 | 1997-12-31 | Siemens Aktiengesellschaft | Turbinenwelle sowie verfahren zur kühlung einer turbinenwelle |
JP3621523B2 (ja) * | 1996-09-25 | 2005-02-16 | 株式会社東芝 | ガスタービンの動翼冷却装置 |
US5704764A (en) * | 1996-10-07 | 1998-01-06 | Westinghouse Electric Corporation | Turbine inter-disk cavity cooling air compressor |
SE508085C2 (sv) * | 1996-12-12 | 1998-08-24 | Abb Carbon Ab | Förfarande för luftflödesstyrning av förbränningsluft samt spärrluftanordning |
CN1143945C (zh) | 1997-06-27 | 2004-03-31 | 西门子公司 | 内冷却式汽轮机的透平轴以及冷却透平轴的方法 |
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 |
US6053697A (en) * | 1998-06-26 | 2000-04-25 | General Electric Company | Trilobe mounting with anti-rotation apparatus for an air duct in a gas turbine rotor |
US6626635B1 (en) * | 1998-09-30 | 2003-09-30 | General Electric Company | System for controlling clearance between blade tips and a surrounding casing in rotating machinery |
JP3475838B2 (ja) * | 1999-02-23 | 2003-12-10 | 株式会社日立製作所 | タービンロータ及びタービンロータのタービン動翼冷却方法 |
EP1033476B1 (en) | 1999-03-03 | 2006-09-13 | General Electric Company | Heat exchange flow circuit for a turbine rotor |
JP3593488B2 (ja) | 2000-02-25 | 2004-11-24 | 株式会社日立製作所 | ガスタービン |
KR100401183B1 (ko) * | 2001-01-18 | 2003-10-10 | 바이오리플라 주식회사 | 폴리스티렌계 생붕괴성 캡슐 및 그 제조방법 |
JP3481596B2 (ja) * | 2001-02-14 | 2003-12-22 | 株式会社日立製作所 | ガスタービン |
ITMI20011961A1 (it) * | 2001-09-20 | 2003-03-20 | Nuovo Pignone Spa | Flangia migliorata di accoppiamento tra compressore assiale e gruppo di dischi rotorici di alta pressione in una turbina a gas |
US6854736B2 (en) | 2003-03-26 | 2005-02-15 | Siemens Westinghouse Power Corporation | Seal assembly for a rotary machine |
ITMI20032607A1 (it) * | 2003-12-29 | 2005-06-30 | Nuovo Pignone Spa | Disco di un rotore a dischi per una turbina a gas |
EP1577493A1 (de) * | 2004-03-17 | 2005-09-21 | Siemens Aktiengesellschaft | Strömungsmaschine und Rotor für eine Strömungsmaschine |
FR2884867B1 (fr) * | 2005-04-21 | 2007-08-03 | Snecma Moteurs Sa | Dispositif de regulation du debit d'air circulant dans un arbre rotatif d'une turbomachine |
US20150083281A1 (en) * | 2007-12-26 | 2015-03-26 | General Electric Company | High temperature shape memory alloy actuators |
US8061971B2 (en) * | 2008-09-12 | 2011-11-22 | General Electric Company | Apparatus and method for cooling a turbine |
FR2937372B1 (fr) * | 2008-10-22 | 2010-12-10 | Snecma | Aube de turbine equipee de moyens de reglage de son debit de fluide de refroidissement |
US8137054B2 (en) * | 2008-12-23 | 2012-03-20 | General Electric Company | Supersonic compressor |
US8087871B2 (en) * | 2009-05-28 | 2012-01-03 | General Electric Company | Turbomachine compressor wheel member |
US8818684B2 (en) * | 2010-04-15 | 2014-08-26 | General Electric Company | Systems, methods, and apparatus for detecting failure in gas turbine hardware |
CA2760454C (en) | 2010-12-03 | 2019-02-19 | Pratt & Whitney Canada Corp. | Gas turbine rotor containment |
ITCO20110037A1 (it) * | 2011-09-09 | 2013-03-10 | Nuovo Pignone Spa | Sistema di tenuta per attuatore e metodo |
US8893507B2 (en) * | 2011-11-04 | 2014-11-25 | General Electric Company | Method for controlling gas turbine rotor temperature during periods of extended downtime |
US9540940B2 (en) * | 2012-03-12 | 2017-01-10 | General Electric Company | Turbine interstage seal system |
US20130327061A1 (en) * | 2012-06-06 | 2013-12-12 | General Electric Company | Turbomachine bucket assembly and method of cooling a turbomachine bucket assembly |
EP2971518B1 (en) * | 2013-03-11 | 2019-11-20 | United Technologies Corporation | Tie shaft flow trip |
EP3058176B1 (en) | 2013-10-02 | 2020-08-26 | United Technologies Corporation | Gas turbine engine with compressor disk deflectors |
US9683462B2 (en) * | 2013-12-10 | 2017-06-20 | General Electric Company | Cooling fluid flow control system for steam turbine system and program product |
US10006364B2 (en) * | 2014-08-20 | 2018-06-26 | United Technologies Corporation | Gas turbine rotors |
EP3023583A1 (de) | 2014-11-20 | 2016-05-25 | Siemens Aktiengesellschaft | Gasturbine mit einer kühlung der letzten turbinenstufe |
US10337345B2 (en) | 2015-02-20 | 2019-07-02 | General Electric Company | Bucket mounted multi-stage turbine interstage seal and method of assembly |
FR3072724A1 (fr) * | 2017-10-24 | 2019-04-26 | Airbus Operations (S.A.S.) | Turbomachine d'aeronef comprenant un compartiment muni d'un ensemble de ventilation |
IT202000004585A1 (it) * | 2020-03-04 | 2021-09-04 | Nuovo Pignone Tecnologie Srl | Turbina e pala perfezionate per la protezione della radice dai gas caldi del percorso del flusso. |
JP7341969B2 (ja) * | 2020-09-30 | 2023-09-11 | 三菱重工業株式会社 | タービンの設計及び製造方法 |
US11946460B1 (en) | 2022-12-23 | 2024-04-02 | Raytheon Company | Thermal-mechanical linear actuator |
Family Cites Families (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1823624A (en) * | 1923-03-23 | 1931-09-15 | Allis Chalmers Mfg Co | Hydraulic apparatus |
US1557197A (en) * | 1924-01-24 | 1925-10-13 | Delco Light Co | Engine |
US2657901A (en) * | 1945-06-08 | 1953-11-03 | Power Jets Res & Dev Ltd | Construction of turbine rotors |
US2837893A (en) * | 1952-12-12 | 1958-06-10 | Phillips Petroleum Co | Automatic primary and secondary air flow regulation for gas turbine combustion chamber |
US2811833A (en) * | 1953-06-05 | 1957-11-05 | Gen Motors Corp | Turbine cooling |
DE1070880B (de) * | 1956-12-19 | 1959-12-10 | Rolls-Royce Limited, Derby (Großbritannien) | Gasturbinenaggregat mit Turboverdichter |
US3663118A (en) * | 1970-06-01 | 1972-05-16 | Gen Motors Corp | Turbine cooling control |
US3834831A (en) * | 1973-01-23 | 1974-09-10 | Westinghouse Electric Corp | Blade shank cooling arrangement |
FR2280791A1 (fr) * | 1974-07-31 | 1976-02-27 | Snecma | Perfectionnements au reglage du jeu entre les aubes et le stator d'une turbine |
US3966354A (en) * | 1974-12-19 | 1976-06-29 | General Electric Company | Thermal actuated valve for clearance control |
US3966352A (en) * | 1975-06-30 | 1976-06-29 | United Technologies Corporation | Variable area turbine |
US4109864A (en) * | 1976-12-23 | 1978-08-29 | General Electric Company | Coolant flow metering device |
US4213738A (en) * | 1978-02-21 | 1980-07-22 | General Motors Corporation | Cooling air control valve |
US4217755A (en) * | 1978-12-04 | 1980-08-19 | General Motors Corporation | Cooling air control valve |
US4337016A (en) * | 1979-12-13 | 1982-06-29 | United Technologies Corporation | Dual wall seal means |
US4487016A (en) * | 1980-10-01 | 1984-12-11 | United Technologies Corporation | Modulated clearance control for an axial flow rotary machine |
FR2514408B1 (fr) * | 1981-10-14 | 1985-11-08 | Snecma | Dispositif pour controler les dilatations et les contraintes thermiques dans un disque de turbine a gaz |
JPS5877127A (ja) * | 1981-11-02 | 1983-05-10 | Hitachi Ltd | 回転体の流体導入装置 |
US4541775A (en) * | 1983-03-30 | 1985-09-17 | United Technologies Corporation | Clearance control in turbine seals |
JPS60252105A (ja) * | 1984-05-28 | 1985-12-12 | Fuji Electric Co Ltd | タ−ビンのロ−タ冷却装置 |
DE3428892A1 (de) * | 1984-08-04 | 1986-02-13 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Schaufel- und dichtspaltoptimierungseinrichtung fuer verdichter von gasturbinentriebwerken, insbesondere gasturbinenstrahltriebwerken |
US4708588A (en) * | 1984-12-14 | 1987-11-24 | United Technologies Corporation | Turbine cooling air supply system |
DE3540943A1 (de) * | 1985-11-19 | 1987-05-21 | Mtu Muenchen Gmbh | Gasturbinenstrahltriebwerk in mehr-wellen-zweistrom-bauweise |
DE3606597C1 (de) * | 1986-02-28 | 1987-02-19 | Mtu Muenchen Gmbh | Schaufel- und Dichtspaltoptimierungseinrichtung fuer Verdichter von Gasturbinentriebwerken |
FR2600377B1 (fr) * | 1986-06-18 | 1988-09-02 | Snecma | Dispositif de controle des debits d'air de refroidissement d'une turbine de moteur |
FR2604750B1 (fr) * | 1986-10-01 | 1988-12-02 | Snecma | Turbomachine munie d'un dispositif de commande automatique des debits de ventilation de turbine |
US4815272A (en) * | 1987-05-05 | 1989-03-28 | United Technologies Corporation | Turbine cooling and thermal control |
JP2756117B2 (ja) * | 1987-11-25 | 1998-05-25 | 株式会社日立製作所 | ガスタービンロータ |
US4893984A (en) * | 1988-04-07 | 1990-01-16 | General Electric Company | Clearance control system |
-
1990
- 1990-07-27 US US07/558,450 patent/US5054996A/en not_active Expired - Fee Related
-
1991
- 1991-03-20 KR KR1019910004367A patent/KR920002912A/ko not_active Application Discontinuation
- 1991-07-03 JP JP3188310A patent/JPH04232335A/ja not_active Withdrawn
- 1991-07-24 CN CN91104947A patent/CN1058449A/zh not_active Withdrawn
- 1991-07-25 EP EP19910306780 patent/EP0468782A3/en not_active Withdrawn
- 1991-07-26 NO NO91912924A patent/NO912924L/no unknown
Also Published As
Publication number | Publication date |
---|---|
EP0468782A3 (en) | 1992-05-13 |
NO912924L (no) | 1992-01-28 |
JPH04232335A (ja) | 1992-08-20 |
CN1058449A (zh) | 1992-02-05 |
KR920002912A (ko) | 1992-02-28 |
US5054996A (en) | 1991-10-08 |
EP0468782A2 (en) | 1992-01-29 |
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