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MX2011005355A - Turbina de gas con combustion externa, aplicando un intercambiador de calor de regeneracion de rotacion. - Google Patents

Turbina de gas con combustion externa, aplicando un intercambiador de calor de regeneracion de rotacion.

Info

Publication number
MX2011005355A
MX2011005355A MX2011005355A MX2011005355A MX2011005355A MX 2011005355 A MX2011005355 A MX 2011005355A MX 2011005355 A MX2011005355 A MX 2011005355A MX 2011005355 A MX2011005355 A MX 2011005355A MX 2011005355 A MX2011005355 A MX 2011005355A
Authority
MX
Mexico
Prior art keywords
gas turbine
heat exchanger
applying
rotating
external combustion
Prior art date
Application number
MX2011005355A
Other languages
English (en)
Inventor
Ole Bjoern Kleven
Original Assignee
Ares Turbine As
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=42233422&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=MX2011005355(A) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Ares Turbine As filed Critical Ares Turbine As
Publication of MX2011005355A publication Critical patent/MX2011005355A/es

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
    • 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • 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
    • F02C7/08—Heating air supply before combustion, e.g. by exhaust gases
    • F02C7/10—Heating air supply before combustion, e.g. by exhaust gases by means of regenerative heat-exchangers
    • F02C7/105—Heating air supply before combustion, e.g. by exhaust gases by means of regenerative heat-exchangers of the rotary type
    • 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
    • F05D2220/00—Application
    • F05D2220/60—Application making use of surplus or waste energy
    • 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
    • F05D2220/00—Application
    • F05D2220/70—Application in combination with
    • F05D2220/75—Application in combination with equipment using fuel having a low calorific value, e.g. low BTU fuel, waste end, syngas, biomass fuel or flare gas
    • 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
    • F05D2220/00—Application
    • F05D2220/70—Application in combination with
    • F05D2220/76—Application in combination with an electrical generator
    • F05D2220/768—Application in combination with an electrical generator equipped with permanent magnets
    • 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
    • F05D2260/00—Function
    • F05D2260/60—Fluid transfer
    • F05D2260/606—Bypassing the fluid
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D19/00—Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium
    • F28D19/04—Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium using rigid bodies, e.g. mounted on a movable carrier
    • F28D19/041—Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium using rigid bodies, e.g. mounted on a movable carrier with axial flow through the intermediate heat-transfer medium
    • F28D19/042—Rotors; Assemblies of heat absorbing masses

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
  • Air Supply (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)

Abstract

La invención se refiere a una turbina de gas (10) para transformar energía térmica, por ejemplo de carbón, biomasa o similar, a trabajo mecánico, que comprende una unidad compresora (11), una unidad de turbina (13), una cámara de combustión (15) y un intercambiador de calor (14) con sistema de tubería asociado. La turbina de gas (10) está configurada de tal modo que el calor es suministrado al flujo de aire entre la unidad compresora (11) y la unidad de turbina (13) por medio de gas de escape caliente desde la cámara de combustión (15) y es introducido en una cámara de compresión (12) dispuesta entre la unidad compresora (11) y la unidad de turbina (13).
MX2011005355A 2008-11-24 2009-11-24 Turbina de gas con combustion externa, aplicando un intercambiador de calor de regeneracion de rotacion. MX2011005355A (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
NO20084943 2008-11-24
PCT/NO2009/000404 WO2010064921A1 (en) 2008-11-24 2009-11-24 Gas turbine with external combustion, applying a rotating regenerating heat exchanger

Publications (1)

Publication Number Publication Date
MX2011005355A true MX2011005355A (es) 2011-09-01

Family

ID=42233422

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2011005355A MX2011005355A (es) 2008-11-24 2009-11-24 Turbina de gas con combustion externa, aplicando un intercambiador de calor de regeneracion de rotacion.

Country Status (16)

Country Link
US (1) US20110227346A1 (es)
EP (1) EP2368031B1 (es)
JP (1) JP5394503B2 (es)
CN (1) CN102224332B (es)
AP (1) AP3165A (es)
AU (1) AU2009323069B2 (es)
BR (1) BRPI0920949B1 (es)
CA (1) CA2744474C (es)
CO (1) CO6362067A2 (es)
EA (1) EA020476B1 (es)
MX (1) MX2011005355A (es)
NZ (1) NZ593624A (es)
PE (1) PE20120245A1 (es)
UA (1) UA103346C2 (es)
WO (1) WO2010064921A1 (es)
ZA (1) ZA201103845B (es)

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US9631815B2 (en) 2012-12-28 2017-04-25 General Electric Company System and method for a turbine combustor
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US9581081B2 (en) 2013-01-13 2017-02-28 General Electric Company System and method for protecting components in a gas turbine engine with exhaust gas recirculation
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TW201502356A (zh) 2013-02-21 2015-01-16 Exxonmobil Upstream Res Co 氣渦輪機排氣中氧之減少
US9938861B2 (en) 2013-02-21 2018-04-10 Exxonmobil Upstream Research Company Fuel combusting method
RU2637609C2 (ru) 2013-02-28 2017-12-05 Эксонмобил Апстрим Рисерч Компани Система и способ для камеры сгорания турбины
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US9617914B2 (en) 2013-06-28 2017-04-11 General Electric Company Systems and methods for monitoring gas turbine systems having exhaust gas recirculation
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Also Published As

Publication number Publication date
ZA201103845B (en) 2012-07-25
EP2368031B1 (en) 2019-07-03
EA201190014A1 (ru) 2012-02-28
JP5394503B2 (ja) 2014-01-22
NZ593624A (en) 2012-10-26
UA103346C2 (ru) 2013-10-10
BRPI0920949B1 (pt) 2020-10-27
PE20120245A1 (es) 2012-04-21
HK1162634A1 (en) 2012-08-31
JP2012510020A (ja) 2012-04-26
CO6362067A2 (es) 2012-01-20
WO2010064921A1 (en) 2010-06-10
BRPI0920949A2 (pt) 2015-12-29
EP2368031A1 (en) 2011-09-28
AU2009323069B2 (en) 2012-02-02
CA2744474C (en) 2018-05-01
CN102224332B (zh) 2013-11-13
US20110227346A1 (en) 2011-09-22
CA2744474A1 (en) 2010-06-10
AP2011005748A0 (en) 2011-06-30
EP2368031A4 (en) 2017-12-27
AP3165A (en) 2015-03-31
CN102224332A (zh) 2011-10-19
EA020476B1 (ru) 2014-11-28
AU2009323069A1 (en) 2011-07-14

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