BR112013015184A2 - sistema de turbina a gás aquecida indiretamente - Google Patents
sistema de turbina a gás aquecida indiretamenteInfo
- Publication number
- BR112013015184A2 BR112013015184A2 BR112013015184A BR112013015184A BR112013015184A2 BR 112013015184 A2 BR112013015184 A2 BR 112013015184A2 BR 112013015184 A BR112013015184 A BR 112013015184A BR 112013015184 A BR112013015184 A BR 112013015184A BR 112013015184 A2 BR112013015184 A2 BR 112013015184A2
- Authority
- BR
- Brazil
- Prior art keywords
- gas turbine
- turbine system
- combustion chamber
- indirectly heated
- heat exchanger
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 abstract 6
- 239000007789 gas Substances 0.000 abstract 5
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 abstract 2
- 239000003546 flue gas Substances 0.000 abstract 2
- 239000000446 fuel Substances 0.000 abstract 1
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
- F02C1/00—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
- F02C1/04—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid the working fluid being heated indirectly
-
- 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
- F02C1/00—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
- F02C1/04—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid the working fluid being heated indirectly
- F02C1/05—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid the working fluid being heated indirectly characterised by the type or source of heat, e.g. using nuclear or solar energy
-
- 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
- F02C1/00—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
- F02C1/04—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid the working fluid being heated indirectly
- F02C1/05—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid the working fluid being heated indirectly characterised by the type or source of heat, e.g. using nuclear or solar energy
- F02C1/06—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid the working fluid being heated indirectly characterised by the type or source of heat, e.g. using nuclear or solar energy using reheated exhaust gas
-
- 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
- F02C1/00—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
- F02C1/04—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid the working fluid being heated indirectly
- F02C1/10—Closed cycles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/80—Size or power range of the machines
- F05D2250/82—Micromachines
-
- 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)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Life Sciences & Earth Sciences (AREA)
- High Energy & Nuclear Physics (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Abstract
sistema de turbina a gás indiretamente aquecido a presente invenção refere-se a um sistema de turbina a gás aquecido que compreende uma câmara de combustão (3), que se estende ao longo de um eixo central do sistema de turbina a gás para a combustão do combustível e do ar comprimido fornecido através do qual o gás de combustão é formado, uma turbinas (2) acionada por um meio de trabalho, um compressor (1), ligada rotativamente à turbina para comprimir o meio de trabalho e / ou de ar para a câmara de combustão, e um primeiro dispositivo permutador de calor (8) para a transferência de calor entre o gás de combustão e a trabalhar médio. o primeiro dispositivo permutador de calor e a câmara de combustão são integralmente formados como uma unidade monolítica, o primeiro dispositivo permutador de calor ser substancialmente disposta no interior da extensão axial da câmara de combustão ao longo do eixo central. pela concepção integrada da câmara de combustão e o primeiro dispositivo permutador de calor, um sistema de turbina compacto, sistema de turbina a gás indiretamente aquecido indiretamente aquecido alcançando uma alta eficiência.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE1051322-4 | 2010-12-15 | ||
SE1051322A SE535434C2 (sv) | 2010-12-15 | 2010-12-15 | Indirekt eldat gasturbinsystem |
PCT/SE2011/051519 WO2012082062A1 (en) | 2010-12-15 | 2011-12-15 | Indirectly heated gas turbine system |
Publications (2)
Publication Number | Publication Date |
---|---|
BR112013015184A2 true BR112013015184A2 (pt) | 2016-09-13 |
BR112013015184B1 BR112013015184B1 (pt) | 2020-12-22 |
Family
ID=46244975
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112013015184-6A BR112013015184B1 (pt) | 2010-12-15 | 2011-12-15 | sistema de turbina a gás aquecida indiretamente e veículo com sistema de turbina a gás |
Country Status (5)
Country | Link |
---|---|
US (1) | US9181871B2 (pt) |
JP (1) | JP5955858B2 (pt) |
BR (1) | BR112013015184B1 (pt) |
SE (1) | SE535434C2 (pt) |
WO (1) | WO2012082062A1 (pt) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20150128557A1 (en) * | 2013-11-08 | 2015-05-14 | Gnc Galileo S.A. | Microscale distributed energy cogeneration method and system |
US11952903B2 (en) | 2013-11-08 | 2024-04-09 | Galileo Technologies Corp. | Microturbine and method of manufacture |
ES2575352B1 (es) * | 2014-11-28 | 2017-04-11 | Abengoa Solar New Technologies, S.A. | Planta híbrida solar-fósil de alto rendimiento |
US10443495B2 (en) * | 2017-04-14 | 2019-10-15 | Enexor Energy | Combined heat and power system and method of operation |
CN110514052A (zh) * | 2019-09-25 | 2019-11-29 | 江苏恒军动力科技有限公司 | 一种微型燃气轮发电机使用的回热器 |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4492085A (en) * | 1982-08-09 | 1985-01-08 | General Electric Company | Gas turbine power plant |
US4827723A (en) * | 1988-02-18 | 1989-05-09 | A. Ahlstrom Corporation | Integrated gas turbine power generation system and process |
US5165239A (en) * | 1991-06-03 | 1992-11-24 | The United States Of America As Represented By The United States Department Of Energy | Water augmented indirectly-fired gas turbine systems and method |
US6066898A (en) * | 1998-08-14 | 2000-05-23 | Alliedsignal Inc. | Microturbine power generating system including variable-speed gas compressor |
US6951110B2 (en) * | 2000-11-06 | 2005-10-04 | Capstone Turbine Corporation | Annular recuperator design |
GB0100601D0 (en) | 2001-01-10 | 2001-02-21 | Talbotts Heating Ltd | Power generating system |
AU2003229524A1 (en) | 2002-04-27 | 2003-11-17 | Oko-Insel Maschinenbau Gmbh | Micro gas turbine, method for the operation thereof, and use of a micro gas turbine |
JP2004084575A (ja) * | 2002-08-27 | 2004-03-18 | Honda Motor Co Ltd | ガスタービン発電装置 |
GB2402172A (en) | 2003-05-30 | 2004-12-01 | Bowman Power Systems Ltd | Generator system |
GB0425369D0 (en) * | 2004-11-18 | 2004-12-22 | Talbotts Heating Ltd | Power generating system |
SE531220C2 (sv) * | 2005-04-21 | 2009-01-20 | Compower Ab | Energiåtervinninssystem för en processanordning |
US7603860B2 (en) | 2006-08-15 | 2009-10-20 | Mark Odell Thomas | High efficiency flexfuel internal combustion engine |
FR2913724B1 (fr) | 2007-03-15 | 2009-05-08 | Compte R Soc Par Actions Simpl | Utilisation de fumees chaudes issues de la combustion de matieres combustibles pour produire de l'energie mecanique, et installation correspondante |
US8176724B2 (en) * | 2008-09-18 | 2012-05-15 | Smith Douglas W P | Hybrid Brayton cycle with solid fuel firing |
WO2010064921A1 (en) * | 2008-11-24 | 2010-06-10 | Kleven Ole Bjoern | Gas turbine with external combustion, applying a rotating regenerating heat exchanger |
-
2010
- 2010-12-15 SE SE1051322A patent/SE535434C2/sv unknown
-
2011
- 2011-12-15 US US13/994,987 patent/US9181871B2/en active Active
- 2011-12-15 BR BR112013015184-6A patent/BR112013015184B1/pt active IP Right Grant
- 2011-12-15 JP JP2013544431A patent/JP5955858B2/ja active Active
- 2011-12-15 WO PCT/SE2011/051519 patent/WO2012082062A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
SE1051322A1 (sv) | 2012-06-16 |
SE535434C2 (sv) | 2012-08-07 |
US20130269344A1 (en) | 2013-10-17 |
US9181871B2 (en) | 2015-11-10 |
BR112013015184B1 (pt) | 2020-12-22 |
WO2012082062A1 (en) | 2012-06-21 |
JP2013545938A (ja) | 2013-12-26 |
JP5955858B2 (ja) | 2016-07-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B06F | Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette] | ||
B06U | Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette] | ||
B09A | Decision: intention to grant [chapter 9.1 patent gazette] | ||
B16A | Patent or certificate of addition of invention granted [chapter 16.1 patent gazette] |
Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 15/12/2011, OBSERVADAS AS CONDICOES LEGAIS. |