PL396519A1 - Uklad wydechowej sekcji turbiny gazowej - Google Patents
Uklad wydechowej sekcji turbiny gazowejInfo
- Publication number
- PL396519A1 PL396519A1 PL396519A PL39651911A PL396519A1 PL 396519 A1 PL396519 A1 PL 396519A1 PL 396519 A PL396519 A PL 396519A PL 39651911 A PL39651911 A PL 39651911A PL 396519 A1 PL396519 A1 PL 396519A1
- Authority
- PL
- Poland
- Prior art keywords
- exhaust
- external
- internal
- flow channel
- turbine
- Prior art date
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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/08—Cooling; Heating; Heat-insulation
- F01D25/12—Cooling
- F01D25/125—Cooling of bearings
-
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/08—Cooling; Heating; Heat-insulation
- F01D25/14—Casings modified therefor
-
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/30—Exhaust heads, chambers, or the like
-
- 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
-
- 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
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)
- Supercharger (AREA)
- Support Of The Bearing (AREA)
Abstract
Ujawniono uklad, zawierajacy sekcje wydechowa turbiny, która zawiera wydechowy kanal przeplywowy. Wydechowa sekcja turbiny zawiera równiez zewnetrzna konstrukcje (42), majaca oslone (108), zewnetrzna scianke wydechowa (106) umieszczona wzdluz wydechowego kanalu przeplywowego, oraz zewnetrzna wneke (110) umieszczona miedzy zewnetrzna scianka wydechowa (106), a zewnetrzna oslona (108). Wydechowa sekcja turbiny zawiera ponadto wewnetrzna konstrukcje (38), majaca wewnetrzna scianke wydechowa (80) usytuowana wzdluz wydechowego kanalu przeplywowego, wewnetrzna wneke (91) usytuowana miedzy wewnetrzna scianka wydechowa (80) i wewnetrzna oslona (92) oraz wneke (82) lozyska usytuowana miedzy wewnetrzna oslona (92), a obudowa (85) lozyska. Dodatkowo, wydechowa sekcja turbiny zawiera rozpórke (40) rozposcierajaca sie miedzy zewnetrzna konstrukcja (42) i wewnetrzna konstrukcja (38). Rozpórka (40) zawiera pierwszy kanal przeplywowy (52), skonfigurowany do prowadzenia plynu z wewnetrznej wneki (91) do zewnetrznej wneki (110).
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL396519A PL220729B1 (pl) | 2011-10-03 | 2011-10-03 | Układ turbiny gazowej |
EP12186207.2A EP2578816B1 (en) | 2011-10-03 | 2012-09-27 | Gas turbine exhaust section structures with internal flow passages |
CN201210368930.3A CN103032116B (zh) | 2011-10-03 | 2012-09-27 | 用于冷却涡轮排气部分的系统 |
US13/633,625 US9546567B2 (en) | 2011-10-03 | 2012-10-02 | Turbine exhaust section structures with internal flow passages |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL396519A PL220729B1 (pl) | 2011-10-03 | 2011-10-03 | Układ turbiny gazowej |
Publications (2)
Publication Number | Publication Date |
---|---|
PL396519A1 true PL396519A1 (pl) | 2013-04-15 |
PL220729B1 PL220729B1 (pl) | 2015-12-31 |
Family
ID=46963589
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL396519A PL220729B1 (pl) | 2011-10-03 | 2011-10-03 | Układ turbiny gazowej |
Country Status (4)
Country | Link |
---|---|
US (1) | US9546567B2 (pl) |
EP (1) | EP2578816B1 (pl) |
CN (1) | CN103032116B (pl) |
PL (1) | PL220729B1 (pl) |
Families Citing this family (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2679780B8 (en) * | 2012-06-28 | 2016-09-14 | General Electric Technology GmbH | Diffuser for the exhaust section of a gas turbine and gas turbine with such a diffuser |
US10167782B2 (en) | 2013-09-10 | 2019-01-01 | Siemens Aktiengesellschaft | Cooling air line for removing cooling air from a manhole of a gas turbine |
CN105960511B (zh) * | 2013-11-08 | 2018-03-13 | 通用电气公司 | 涡轮机排气框架 |
JP5876894B2 (ja) * | 2014-04-07 | 2016-03-02 | 川崎重工業株式会社 | タービンの換気構造 |
US20150354382A1 (en) * | 2014-06-06 | 2015-12-10 | General Electric Company | Exhaust frame cooling via strut cooling passages |
EP3155233B1 (en) * | 2014-06-10 | 2019-01-02 | Siemens Energy, Inc. | Gas turbine engine with rotor centering cooling system in an exhaust diffuser |
US9903215B2 (en) * | 2014-06-11 | 2018-02-27 | General Electric Company | Cooling passages for inner casing of a turbine exhaust |
US20170067365A1 (en) * | 2015-09-09 | 2017-03-09 | General Electric Company | Exhaust frame strut with cooling fins |
JP6580494B2 (ja) | 2016-01-22 | 2019-09-25 | 三菱日立パワーシステムズ株式会社 | 排気フレーム |
ITUA20161748A1 (it) | 2016-03-17 | 2017-09-17 | I M A Industria Macch Automatiche S P A In Sigla Ima S P A | Gruppo per la regolarizzazione e laminazione di un flusso gassoso |
US20180149085A1 (en) * | 2016-11-28 | 2018-05-31 | General Electric Company | Exhaust frame cooling via cooling flow reversal |
KR101882104B1 (ko) | 2016-12-20 | 2018-07-25 | 두산중공업 주식회사 | 가스터빈 |
GB2566498B (en) * | 2017-09-15 | 2021-02-17 | Gkn Aerospace Sweden Ab | Turbine exhaust case cooling |
US11286882B2 (en) * | 2018-11-28 | 2022-03-29 | Pratt & Whitney Canada Corp. | Exhaust casing for a gas turbine engine |
US11391179B2 (en) | 2019-02-12 | 2022-07-19 | Pratt & Whitney Canada Corp. | Gas turbine engine with bearing support structure |
US11346249B2 (en) | 2019-03-05 | 2022-05-31 | Pratt & Whitney Canada Corp. | Gas turbine engine with feed pipe for bearing housing |
GB2589125B (en) * | 2019-11-21 | 2022-10-19 | Gkn Aerospace Sweden Ab | Heat exchanger integration |
US11578621B2 (en) * | 2020-04-08 | 2023-02-14 | General Electric Company | System for cooling turbine shaft coupling |
DE102020122588A1 (de) | 2020-08-28 | 2022-03-03 | Rolls-Royce Deutschland Ltd & Co Kg | Ölsystem eines Gasturbinentriebwerkes und Gasturbinentriebwerk |
JP2023100250A (ja) * | 2022-01-05 | 2023-07-18 | ゼネラル・エレクトリック・カンパニイ | 排気フレーム差動冷却システム |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4076452A (en) * | 1974-04-09 | 1978-02-28 | Brown, Boveri-Sulzer Turbomaschinen Ag | Gas turbine plant |
GB2234035B (en) | 1989-07-21 | 1993-05-12 | Rolls Royce Plc | A reduction gear assembly and a gas turbine engine |
JP2954797B2 (ja) | 1992-10-05 | 1999-09-27 | 株式会社東芝 | 蒸気タ−ビンの強制冷却装置 |
US6406254B1 (en) | 1999-05-10 | 2002-06-18 | General Electric Company | Cooling circuit for steam and air-cooled turbine nozzle stage |
US6266954B1 (en) | 1999-12-15 | 2001-07-31 | General Electric Co. | Double wall bearing cone |
US6438938B1 (en) * | 2000-11-28 | 2002-08-27 | Rolls-Royce Corporation | Bearing compartment self cooling vent system |
JP4410425B2 (ja) | 2001-03-05 | 2010-02-03 | 三菱重工業株式会社 | 冷却型ガスタービン排気車室 |
DE50301055D1 (de) * | 2002-05-22 | 2005-09-29 | Alstom Technology Ltd Baden | Kühlbares bauteil und verfahren zur herstellung einer durchtrittsöffnung in einem kühlbarem bauteil |
WO2004090291A1 (de) | 2003-04-07 | 2004-10-21 | Alstom Technology Ltd | Turbomaschine |
EP1777378A3 (en) | 2003-07-29 | 2011-03-09 | Pratt & Whitney Canada Corp. | Turbofan case and method of making |
JP4040556B2 (ja) | 2003-09-04 | 2008-01-30 | 株式会社日立製作所 | ガスタービン設備及び冷却空気供給方法 |
US7493769B2 (en) * | 2005-10-25 | 2009-02-24 | General Electric Company | Assembly and method for cooling rear bearing and exhaust frame of gas turbine |
EP1793091A1 (de) | 2005-12-01 | 2007-06-06 | Siemens Aktiengesellschaft | Dampfturbine mit Lagerstreben |
JP4681458B2 (ja) | 2006-01-17 | 2011-05-11 | 三菱重工業株式会社 | ガスタービン排気部の冷却構造及び該構造を備えたガスタービン設備 |
JP5118496B2 (ja) * | 2008-01-10 | 2013-01-16 | 三菱重工業株式会社 | ガスタービンの排気部の構造およびガスタービン |
US8371812B2 (en) * | 2008-11-29 | 2013-02-12 | General Electric Company | Turbine frame assembly and method for a gas turbine engine |
JP5398405B2 (ja) | 2009-07-30 | 2014-01-29 | 三菱重工業株式会社 | 流路構造及びガスタービン排気ディフューザ |
US8511969B2 (en) * | 2009-10-01 | 2013-08-20 | Pratt & Whitney Canada Corp. | Interturbine vane with multiple air chambers |
US8500392B2 (en) * | 2009-10-01 | 2013-08-06 | Pratt & Whitney Canada Corp. | Sealing for vane segments |
US8979477B2 (en) * | 2011-03-09 | 2015-03-17 | General Electric Company | System for cooling and purging exhaust section of gas turbine engine |
US8641362B1 (en) * | 2011-09-13 | 2014-02-04 | Florida Turbine Technologies, Inc. | Turbine exhaust cylinder and strut cooling |
-
2011
- 2011-10-03 PL PL396519A patent/PL220729B1/pl unknown
-
2012
- 2012-09-27 EP EP12186207.2A patent/EP2578816B1/en active Active
- 2012-09-27 CN CN201210368930.3A patent/CN103032116B/zh active Active
- 2012-10-02 US US13/633,625 patent/US9546567B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
US20130084172A1 (en) | 2013-04-04 |
EP2578816A2 (en) | 2013-04-10 |
PL220729B1 (pl) | 2015-12-31 |
CN103032116A (zh) | 2013-04-10 |
EP2578816A3 (en) | 2017-05-31 |
EP2578816B1 (en) | 2020-03-04 |
US9546567B2 (en) | 2017-01-17 |
CN103032116B (zh) | 2016-12-07 |
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