DE69305326D1 - Ejektor für kühlfluid - Google Patents
Ejektor für kühlfluidInfo
- Publication number
- DE69305326D1 DE69305326D1 DE69305326T DE69305326T DE69305326D1 DE 69305326 D1 DE69305326 D1 DE 69305326D1 DE 69305326 T DE69305326 T DE 69305326T DE 69305326 T DE69305326 T DE 69305326T DE 69305326 D1 DE69305326 D1 DE 69305326D1
- Authority
- DE
- Germany
- Prior art keywords
- ejector
- coolant
- 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 - Fee Related
Links
- 239000002826 coolant Substances 0.000 title 1
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
- F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US83325692A | 1992-02-10 | 1992-02-10 | |
| PCT/US1993/001081 WO1993016275A1 (en) | 1992-02-10 | 1993-02-08 | Improved cooling fluid ejector |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| DE69305326D1 true DE69305326D1 (de) | 1996-11-14 |
| DE69305326T2 DE69305326T2 (de) | 1997-05-07 |
Family
ID=25263885
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE69305326T Expired - Fee Related DE69305326T2 (de) | 1992-02-10 | 1993-02-08 | Ejektor für kühlfluid |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US5352087A (de) |
| EP (1) | EP0626036B1 (de) |
| JP (1) | JP2640783B2 (de) |
| DE (1) | DE69305326T2 (de) |
| WO (1) | WO1993016275A1 (de) |
Families Citing this family (45)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5639212A (en) * | 1996-03-29 | 1997-06-17 | General Electric Company | Cavity sealed compressor |
| JP3416447B2 (ja) * | 1997-03-11 | 2003-06-16 | 三菱重工業株式会社 | ガスタービンの翼冷却空気供給システム |
| JPH10252412A (ja) * | 1997-03-12 | 1998-09-22 | Mitsubishi Heavy Ind Ltd | ガスタービンシール装置 |
| GB9723268D0 (en) * | 1997-11-05 | 1998-01-07 | Rolls Royce Plc | Turbine |
| KR20000071653A (ko) * | 1999-04-15 | 2000-11-25 | 제이 엘. 차스킨, 버나드 스나이더, 아더엠. 킹 | 육상용 가스 터빈 및 가스 터빈의 하나의 단을 냉각시키는방법 |
| US6220815B1 (en) * | 1999-12-17 | 2001-04-24 | General Electric Company | Inter-stage seal retainer and assembly |
| US6435816B1 (en) * | 2000-11-03 | 2002-08-20 | General Electric Co. | Gas injector system and its fabrication |
| JP4494658B2 (ja) * | 2001-02-06 | 2010-06-30 | 三菱重工業株式会社 | ガスタービンの静翼シュラウド |
| US6884023B2 (en) * | 2002-09-27 | 2005-04-26 | United Technologies Corporation | Integral swirl knife edge injection assembly |
| US7052231B2 (en) * | 2003-04-28 | 2006-05-30 | General Electric Company | Methods and apparatus for injecting fluids in gas turbine engines |
| US6899520B2 (en) * | 2003-09-02 | 2005-05-31 | General Electric Company | Methods and apparatus to reduce seal rubbing within gas turbine engines |
| DE102007027427A1 (de) * | 2007-06-14 | 2008-12-18 | Rolls-Royce Deutschland Ltd & Co Kg | Schaufeldeckband mit Überstand |
| US20090074589A1 (en) * | 2007-09-18 | 2009-03-19 | Biao Fang | Cooling Circuit for Enhancing Turbine Performance |
| US8500394B2 (en) | 2008-02-20 | 2013-08-06 | United Technologies Corporation | Single channel inner diameter shroud with lightweight inner core |
| US20100000219A1 (en) * | 2008-07-02 | 2010-01-07 | General Electric Company | Systems and Methods for Supplying Cooling Air to a Gas Turbine |
| US8162598B2 (en) * | 2008-09-25 | 2012-04-24 | Siemens Energy, Inc. | Gas turbine sealing apparatus |
| US8038399B1 (en) * | 2008-11-22 | 2011-10-18 | Florida Turbine Technologies, Inc. | Turbine rim cavity sealing |
| 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 |
| US8177495B2 (en) * | 2009-03-24 | 2012-05-15 | General Electric Company | Method and apparatus for turbine interstage seal ring |
| US9068469B2 (en) * | 2011-09-01 | 2015-06-30 | Honeywell International Inc. | Gas turbine engines with abradable turbine seal assemblies |
| US9017013B2 (en) * | 2012-02-07 | 2015-04-28 | Siemens Aktiengesellschaft | Gas turbine engine with improved cooling between turbine rotor disk elements |
| EP2636849B1 (de) * | 2012-03-05 | 2017-11-01 | MTU Aero Engines GmbH | Verdichter |
| US9540940B2 (en) * | 2012-03-12 | 2017-01-10 | General Electric Company | Turbine interstage seal system |
| FR2988428B1 (fr) * | 2012-03-26 | 2017-07-07 | Snecma | Aubage de turbomachine avec couronne interne rapportee et elements de renfort. |
| US9279339B2 (en) | 2013-03-13 | 2016-03-08 | Siemens Aktiengesellschaft | Turbine engine temperature control system with heating element for a gas turbine engine |
| DE102013209746B4 (de) * | 2013-05-27 | 2014-12-18 | MTU Aero Engines AG | Turbinenstufe mit einer Ausblasanordnung und Verfahren zum Ausblasen einer Sperrgasströmung |
| US9404376B2 (en) * | 2013-10-28 | 2016-08-02 | General Electric Company | Sealing component for reducing secondary airflow in a turbine system |
| WO2015112227A2 (en) | 2013-11-12 | 2015-07-30 | United Technologies Corporation | Multiple injector holes for gas turbine engine vane |
| FR3027343B1 (fr) * | 2014-10-15 | 2019-08-09 | Safran Aircraft Engines | Ensemble rotatif pour turbomachine comprenant un anneau de stator auto-porte |
| US9771817B2 (en) | 2014-11-04 | 2017-09-26 | General Electric Company | Methods and system for fluidic sealing in gas turbine engines |
| US10161250B2 (en) * | 2015-02-10 | 2018-12-25 | United Technologies Corporation | Rotor with axial arm having protruding ramp |
| US10145269B2 (en) | 2015-03-04 | 2018-12-04 | General Electric Company | System and method for cooling discharge flow |
| EP3091178A1 (de) * | 2015-05-07 | 2016-11-09 | MTU Aero Engines GmbH | Rotortrommel für eine strömungsmaschine und verdichter |
| DE102015111750A1 (de) * | 2015-07-20 | 2017-01-26 | Rolls-Royce Deutschland Ltd & Co Kg | Gekühltes Turbinenlaufrad für ein Flugtriebwerk |
| US9970299B2 (en) | 2015-09-16 | 2018-05-15 | General Electric Company | Mixing chambers for turbine wheel space cooling |
| US10132195B2 (en) | 2015-10-20 | 2018-11-20 | General Electric Company | Wheel space purge flow mixing chamber |
| US10125632B2 (en) | 2015-10-20 | 2018-11-13 | General Electric Company | Wheel space purge flow mixing chamber |
| US10519873B2 (en) | 2016-04-06 | 2019-12-31 | General Electric Company | Air bypass system for rotor shaft cooling |
| US10494936B2 (en) * | 2016-05-23 | 2019-12-03 | United Technologies Corporation | Fastener retention mechanism |
| US10400618B2 (en) * | 2017-05-02 | 2019-09-03 | Rolls-Royce Corporation | Shaft seal crack obviation |
| FR3084396B1 (fr) * | 2018-07-27 | 2020-08-21 | Safran Aircraft Engines | Dispositif d'etancheite entre un etage d'aubes fixes et un etage d'aubes mobiles |
| EP3788236B1 (de) * | 2018-08-02 | 2023-06-21 | Siemens Energy Global GmbH & Co. KG | Rotor mit zwischen zwei rotorscheiben angeordnetem rotorbauteil |
| US10753208B2 (en) | 2018-11-30 | 2020-08-25 | General Electric Company | Airfoils including plurality of nozzles and venturi |
| US10815828B2 (en) | 2018-11-30 | 2020-10-27 | General Electric Company | Hot gas path components including plurality of nozzles and venturi |
| KR20200113593A (ko) * | 2019-03-26 | 2020-10-07 | 이태준 | 배관 직결형 터보압축기 |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2963307A (en) * | 1954-12-28 | 1960-12-06 | Gen Electric | Honeycomb seal |
| US3135215A (en) * | 1963-03-05 | 1964-06-02 | Mechanical Tech Inc | Regenerative devices |
| US3295823A (en) * | 1965-10-13 | 1967-01-03 | Raymond G H Waugh | Gas turbine cooling distribution system using the blade ring principle |
| FR1548541A (de) | 1967-10-24 | 1968-12-06 | ||
| US4265590A (en) * | 1978-05-20 | 1981-05-05 | Rolls-Royce Limited | Cooling air supply arrangement for a gas turbine engine |
| US4627233A (en) * | 1983-08-01 | 1986-12-09 | United Technologies Corporation | Stator assembly for bounding the working medium flow path of a gas turbine engine |
| US4553901A (en) * | 1983-12-21 | 1985-11-19 | United Technologies Corporation | Stator structure for a gas turbine engine |
| US4645424A (en) * | 1984-07-23 | 1987-02-24 | United Technologies Corporation | Rotating seal for gas turbine engine |
| US4659289A (en) * | 1984-07-23 | 1987-04-21 | United Technologies Corporation | Turbine side plate assembly |
| WO1987004224A1 (en) | 1985-12-29 | 1987-07-16 | Központi Bányászati Fejlesztési Intézet | Actuating device for pipe-chamber feeders of hydraulic transport equipments |
| US4666368A (en) * | 1986-05-01 | 1987-05-19 | General Electric Company | Swirl nozzle for a cooling system in gas turbine engines |
| US4752185A (en) * | 1987-08-03 | 1988-06-21 | General Electric Company | Non-contacting flowpath seal |
| US4869640A (en) * | 1988-09-16 | 1989-09-26 | United Technologies Corporation | Controlled temperature rotating seal |
| US4846628A (en) | 1988-12-23 | 1989-07-11 | United Technologies Corporation | Rotor assembly for a turbomachine |
-
1993
- 1993-02-08 DE DE69305326T patent/DE69305326T2/de not_active Expired - Fee Related
- 1993-02-08 WO PCT/US1993/001081 patent/WO1993016275A1/en active IP Right Grant
- 1993-02-08 EP EP93904957A patent/EP0626036B1/de not_active Expired - Lifetime
- 1993-02-08 JP JP5514220A patent/JP2640783B2/ja not_active Expired - Lifetime
- 1993-06-23 US US08/081,902 patent/US5352087A/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| EP0626036B1 (de) | 1996-10-09 |
| EP0626036A1 (de) | 1994-11-30 |
| JPH07500399A (ja) | 1995-01-12 |
| DE69305326T2 (de) | 1997-05-07 |
| US5352087A (en) | 1994-10-04 |
| JP2640783B2 (ja) | 1997-08-13 |
| WO1993016275A1 (en) | 1993-08-19 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 8364 | No opposition during term of opposition | ||
| 8339 | Ceased/non-payment of the annual fee |