DE69926594D1 - Axiale Gasturbine - Google Patents
Axiale GasturbineInfo
- Publication number
- DE69926594D1 DE69926594D1 DE69926594T DE69926594T DE69926594D1 DE 69926594 D1 DE69926594 D1 DE 69926594D1 DE 69926594 T DE69926594 T DE 69926594T DE 69926594 T DE69926594 T DE 69926594T DE 69926594 D1 DE69926594 D1 DE 69926594D1
- Authority
- DE
- Germany
- Prior art keywords
- gas turbine
- axial gas
- axial
- turbine
- gas
- 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.)
- Expired - Lifetime
Links
Classifications
-
- 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
- F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
- F01D11/122—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material
-
- 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
- F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
- F01D11/025—Seal clearance control; Floating assembly; Adaptation means to differential thermal dilatations
-
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/218,704 US6203273B1 (en) | 1998-12-22 | 1998-12-22 | Rotary machine |
US218704 | 1998-12-22 |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69926594D1 true DE69926594D1 (de) | 2005-09-15 |
DE69926594T2 DE69926594T2 (de) | 2006-05-18 |
Family
ID=22816147
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE1999626594 Expired - Lifetime DE69926594T2 (de) | 1998-12-22 | 1999-12-22 | Axiale Gasturbine |
Country Status (4)
Country | Link |
---|---|
US (1) | US6203273B1 (de) |
EP (1) | EP1013889B1 (de) |
JP (1) | JP2000186507A (de) |
DE (1) | DE69926594T2 (de) |
Families Citing this family (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6425736B1 (en) * | 1999-08-09 | 2002-07-30 | United Technologies Corporation | Stator assembly for a rotary machine and method for making the stator assembly |
JP4496650B2 (ja) * | 2001-01-10 | 2010-07-07 | 富士電機システムズ株式会社 | 蒸気タービン |
US6899339B2 (en) * | 2001-08-30 | 2005-05-31 | United Technologies Corporation | Abradable seal having improved durability |
FR2832191B1 (fr) | 2001-11-14 | 2004-10-08 | Snecma Moteurs | Aube de soufflante a sommet fragilise |
GB0128662D0 (en) * | 2001-11-30 | 2002-01-23 | Rolls Royce Plc | Improvements in or relating to generator arrangements |
US6935836B2 (en) * | 2002-06-05 | 2005-08-30 | Allison Advanced Development Company | Compressor casing with passive tip clearance control and endwall ovalization control |
FR2898641B1 (fr) * | 2006-03-17 | 2008-05-02 | Snecma Sa | Habillage de carter dans un turboreacteur |
US8979491B2 (en) | 2009-05-15 | 2015-03-17 | Pratt & Whitney Canada Corp. | Turbofan mounting arrangement |
GB0911500D0 (en) * | 2009-07-03 | 2009-08-12 | Rolls Royce Plc | Rotor blade over-tip leakage control |
US9091172B2 (en) | 2010-12-28 | 2015-07-28 | Rolls-Royce Corporation | Rotor with cooling passage |
DE102011009770B4 (de) * | 2011-01-28 | 2017-06-29 | Lufthansa Technik Ag | Verfahren und Vorrichtung zum Wechseln einer Dichtungsplatte und/oder einer Lagereinheit in einem Flugzeugtriebwerk |
US8777793B2 (en) | 2011-04-27 | 2014-07-15 | United Technologies Corporation | Fan drive planetary gear system integrated carrier and torque frame |
US20120301275A1 (en) * | 2011-05-26 | 2012-11-29 | Suciu Gabriel L | Integrated ceramic matrix composite rotor module for a gas turbine engine |
US8985938B2 (en) | 2011-12-13 | 2015-03-24 | United Technologies Corporation | Fan blade tip clearance control via Z-bands |
US9102397B2 (en) | 2011-12-20 | 2015-08-11 | General Electric Company | Airfoils including tip profile for noise reduction and method for fabricating same |
US9038366B2 (en) | 2012-01-31 | 2015-05-26 | United Technologies Corporation | LPC flowpath shape with gas turbine engine shaft bearing configuration |
US20130192198A1 (en) | 2012-01-31 | 2013-08-01 | Lisa I. Brilliant | Compressor flowpath |
US10400629B2 (en) | 2012-01-31 | 2019-09-03 | United Technologies Corporation | Gas turbine engine shaft bearing configuration |
US8863491B2 (en) | 2012-01-31 | 2014-10-21 | United Technologies Corporation | Gas turbine engine shaft bearing configuration |
US20130202424A1 (en) * | 2012-02-06 | 2013-08-08 | Darin S. Lussier | Conformal liner for gas turbine engine fan section |
US9322337B2 (en) | 2012-06-20 | 2016-04-26 | United Technologies Corporation | Aerodynamic intercompressor bleed ports |
US20140212261A1 (en) * | 2012-12-19 | 2014-07-31 | United Technologies Corporation | Lightweight shrouded fan |
EP2971600B1 (de) * | 2013-03-13 | 2019-07-03 | United Technologies Corporation | Verzahnter architektur zum schutz kritischer hardware während des ausfalls einer gebläseschaufel |
EP2886804B1 (de) * | 2013-12-20 | 2017-08-16 | Safran Aero Boosters SA | Dichtungsanordnung für einen Verdicther eines Turbotriebwerks |
FR3024492B1 (fr) * | 2014-07-29 | 2019-08-23 | Safran Aircraft Engines | Element comprenant un stator et un rotor de turbomachine avec un joint d'etancheite et test de ce joint |
US9777593B2 (en) | 2015-02-23 | 2017-10-03 | General Electric Company | Hybrid metal and composite spool for rotating machinery |
FR3065482B1 (fr) * | 2017-04-20 | 2019-07-05 | Safran Aircraft Engines | Element d'anneau d'etancheite pour turbine comportant une cavite inclinee dans un materiau abradable |
US10934943B2 (en) | 2017-04-27 | 2021-03-02 | General Electric Company | Compressor apparatus with bleed slot and supplemental flange |
CN112747037B (zh) * | 2019-10-31 | 2023-04-07 | 新疆金风科技股份有限公司 | 轴系结构、密封组件以及风力发电机组 |
Family Cites Families (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2762559A (en) * | 1954-09-23 | 1956-09-11 | Westinghouse Electric Corp | Axial flow compressor with axially adjustable rotor |
DE1128708B (de) * | 1960-07-08 | 1962-04-26 | Kloeckner Humboldt Deutz Ag | Gasturbine |
US3183007A (en) | 1961-05-15 | 1965-05-11 | Tann Corp | Seal employing oil-impregnated wicking material and method of making |
BE789908A (fr) * | 1972-02-29 | 1973-02-01 | Federal Mogul Corp | Palier pour vitesses elevees equipe d'un dispositif d'etancheite sensible a la pression de l'air |
US4016636A (en) * | 1974-07-23 | 1977-04-12 | United Technologies Corporation | Compressor construction |
JPS5223531A (en) | 1975-08-18 | 1977-02-22 | Nissan Motor | Abrasionnresistant sliding member and its production method |
FR2370171A1 (fr) | 1976-11-05 | 1978-06-02 | Snecma | Procede et dispositif pour la diminution du bruit des turbomachines |
US4257735A (en) | 1978-12-15 | 1981-03-24 | General Electric Company | Gas turbine engine seal and method for making same |
US4349313A (en) * | 1979-12-26 | 1982-09-14 | United Technologies Corporation | Abradable rub strip |
US4426191A (en) * | 1980-05-16 | 1984-01-17 | United Technologies Corporation | Flow directing assembly for a gas turbine engine |
US4532054A (en) | 1982-12-28 | 1985-07-30 | General Electric Company | Polyetherimide bearing compositions |
DE3315914A1 (de) * | 1983-05-02 | 1984-11-08 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Gasturbinentriebwerk mit einrichtungen zur schaufelspaltminimierung |
US4611464A (en) * | 1984-05-02 | 1986-09-16 | United Technologies Corporation | Rotor assembly for a gas turbine engine and method of disassembly |
JPS61171607A (ja) | 1985-01-24 | 1986-08-02 | Tokai Kogyo Kk | 自動車用密封構成部材 |
US4897021A (en) | 1988-06-02 | 1990-01-30 | United Technologies Corporation | Stator vane asssembly for an axial flow rotary machine |
US4826397A (en) | 1988-06-29 | 1989-05-02 | United Technologies Corporation | Stator assembly for a gas turbine engine |
US5536022A (en) * | 1990-08-24 | 1996-07-16 | United Technologies Corporation | Plasma sprayed abradable seals for gas turbine engines |
US5127794A (en) * | 1990-09-12 | 1992-07-07 | United Technologies Corporation | Compressor case with controlled thermal environment |
JP2970945B2 (ja) * | 1991-01-24 | 1999-11-02 | ユナイテッド テクノロジーズ コーポレイション | ガスタービンケースに対する冷却流量の制御方法 |
US5304032A (en) | 1991-07-22 | 1994-04-19 | Bosna Alexander A | Abradable non-metallic seal for rotating turbine engines |
US5299910A (en) * | 1992-01-23 | 1994-04-05 | General Electric Company | Full-round compressor casing assembly in a gas turbine engine |
US5380155A (en) * | 1994-03-01 | 1995-01-10 | United Technologies Corporation | Compressor stator assembly |
US5456327A (en) | 1994-03-08 | 1995-10-10 | Smith International, Inc. | O-ring seal for rock bit bearings |
US5575145A (en) * | 1994-11-01 | 1996-11-19 | Chevron U.S.A. Inc. | Gas turbine repair |
JP3435945B2 (ja) * | 1995-11-02 | 2003-08-11 | エヌオーケー株式会社 | 密封装置の初期潤滑剤塗布方法 |
-
1998
- 1998-12-22 US US09/218,704 patent/US6203273B1/en not_active Expired - Lifetime
-
1999
- 1999-12-15 JP JP35530799A patent/JP2000186507A/ja active Pending
- 1999-12-22 DE DE1999626594 patent/DE69926594T2/de not_active Expired - Lifetime
- 1999-12-22 EP EP19990310420 patent/EP1013889B1/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP1013889A1 (de) | 2000-06-28 |
DE69926594T2 (de) | 2006-05-18 |
US6203273B1 (en) | 2001-03-20 |
EP1013889B1 (de) | 2005-08-10 |
JP2000186507A (ja) | 2000-07-04 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |