ES2721183T3 - Disposición de turbina de gas multicuerpo - Google Patents

Disposición de turbina de gas multicuerpo Download PDF

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Publication number
ES2721183T3
ES2721183T3 ES16718383T ES16718383T ES2721183T3 ES 2721183 T3 ES2721183 T3 ES 2721183T3 ES 16718383 T ES16718383 T ES 16718383T ES 16718383 T ES16718383 T ES 16718383T ES 2721183 T3 ES2721183 T3 ES 2721183T3
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Spain
Prior art keywords
pressure
generators
turbine
compressor
gas
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Active
Application number
ES16718383T
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English (en)
Inventor
Matti Malkamäki
Jari Backman
Juha Honkatukia
Ahti Jaatinen-Värri
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AURELIA TURBINES Oy
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AURELIA TURBINES Oy
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Application filed by AURELIA TURBINES Oy filed Critical AURELIA TURBINES Oy
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Publication of ES2721183T3 publication Critical patent/ES2721183T3/es
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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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • 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
    • F01D13/00—Combinations of two or more machines or engines
    • F01D13/003—Combinations of two or more machines or engines with at least two independent shafts, i.e. cross-compound
    • 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
    • F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/10—Adaptations for driving, or combinations with, electric generators
    • 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
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/08—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising at least one radial stage
    • F02C3/085—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising at least one radial stage the turbine being of the radial-flow type (radial-radial)
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/003—Gas-turbine plants with heaters between turbine stages
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/02—Plural gas-turbine plants having a common power output
    • 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
    • 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
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02K—DYNAMO-ELECTRIC MACHINES
    • H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
    • H02K7/18—Structural association of electric generators with mechanical driving motors, e.g. with turbines
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02K—DYNAMO-ELECTRIC MACHINES
    • H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
    • H02K7/18—Structural association of electric generators with mechanical driving motors, e.g. with turbines
    • H02K7/1807—Rotary generators
    • H02K7/1823—Rotary generators structurally associated with turbines or similar engines
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H21/00—Use of propulsion power plant or units on vessels
    • B63H21/12—Use of propulsion power plant or units on vessels the vessels being motor-driven
    • B63H21/16—Use of propulsion power plant or units on vessels the vessels being motor-driven relating to gas turbines
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/20—Adaptations of gas-turbine plants for driving vehicles
    • F02C6/203—Adaptations of gas-turbine plants for driving vehicles the vehicles being waterborne vessels
    • 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
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • 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
    • F05D2220/764—Application in combination with an electrical generator of the alternating current (A.C.) 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
    • F05D2240/00—Components
    • F05D2240/60—Shafts

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Power Engineering (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Control Of Eletrric Generators (AREA)
  • Supply And Distribution Of Alternating Current (AREA)

Abstract

Una disposición de turbina de gas multicuerpo, terrestre o marina, para generar energía eléctrica y de rotación para suministrar a una carga (200), en la que dicha carga (200) es externa con respecto a la disposición, comprendiendo la disposición: al menos tres cuerpos (10a, 10b, 10c), incluyendo cada uno de los al menos tres cuerpos (10a, 10b, 10c) un árbol (11a, 11b, 11c), un compresor (C1, C2, C3) y una turbina (T1, T2, T3) montados en el árbol (11a, 11b, 11c); un compresor de la presión máxima (C1) que es el compresor montado en el árbol (11a) del cuerpo (10a) cuya turbina se dispone para tener la presión más alta entre las turbinas (T1), es decir, una turbina de la presión más alta (T1), también se montan en él; una primera cámara de combustión (Comb1) operativa para quemar o hacer reaccionar una mezcla de combustible de modo que el gas comprimido del compresor de la presión más alta (C1) pasa a un gas con una temperatura elevada que se expande en la turbina de la presión más alta (T1) para producir energía mecánica para impulsar el compresor de la presión más alta (C1) en donde la turbina de la presión más alta (T1) es la primera turbina dispuesta para recibir dicho gas con temperatura elevada desde la primera cámara de combustión (Comb1); los al menos tres cuerpos (10a, 10b, 10c) están en comunicación de fluidos entre sí, en donde cada una de las turbinas corriente abajo está dispuesta para recibir gas a una presión más alta desde una turbina inmediatamente dispuesta corriente arriba para operar a una presión más alta que la de las turbinas corriente abajo que reciben gas a presión más alta, y disponiéndose para funcionar, cada uno de los compresores para recibir gas a una presión más baja desde un compresor inmediatamente anterior, a una presión más baja que la del compresor que recibe gas a una presión más baja; y al menos tres generadores (G1, G2, G3), estando acoplado directamente mecánicamente cada uno de ellos a uno de los árboles predefinidos para ser impulsado de manera giratoria, teniendo así cada uno de los árboles (11a, 11b, 11 c) un generador acoplado mecánicamente y un número de los al menos tres generadores (G1, G2, G3) que es igual a un número de los árboles (11a, 11b, 11c), rotando cada uno de los al menos tres generadores (G1, G2, G3) a la misma velocidad que el árbol al que se acopla el generador, siendo operativos los al menos tres generadores (G1, G2, G3) para generar una corriente eléctrica alterna dispuesta para ser suministrada a dicha carga (200) y siendo las salidas de energía eléctrica de los al menos tres generadores (G1, G2, G3) independientemente controlables entre sí, y los al menos tres generadores (G1, G2, G3) tienen niveles de potencia nominal sustancialmente iguales, y las partes giratorias de los al menos tres generadores (G1, G2, G3) tienen velocidades de rotación nominal sustancialmente iguales, y estando configurada la disposición de modo que durante el uso, al menos el 60 por ciento de la potencia de salida total suministrada a dicha carga (200) se dispone para ser generada por los al menos tres generadores (G1, G2, G3) en forma de energía eléctrica, en el que la potencia de salida total es una suma de la potencia eléctrica y de rotación suministrada a dicha carga (200) por la disposición.
ES16718383T 2015-03-23 2016-03-23 Disposición de turbina de gas multicuerpo Active ES2721183T3 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB1504839.0A GB2536878A (en) 2015-03-23 2015-03-23 Multi-spool gas turbine arrangement
PCT/FI2016/050182 WO2016151198A1 (en) 2015-03-23 2016-03-23 Multi-spool gas turbine arrangement

Publications (1)

Publication Number Publication Date
ES2721183T3 true ES2721183T3 (es) 2019-07-29

Family

ID=53052210

Family Applications (1)

Application Number Title Priority Date Filing Date
ES16718383T Active ES2721183T3 (es) 2015-03-23 2016-03-23 Disposición de turbina de gas multicuerpo

Country Status (7)

Country Link
US (1) US10458269B2 (es)
EP (1) EP3274562B1 (es)
ES (1) ES2721183T3 (es)
GB (1) GB2536878A (es)
HK (1) HK1249158B (es)
RU (1) RU2704386C2 (es)
WO (1) WO2016151198A1 (es)

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GB2536876A (en) * 2015-03-23 2016-10-05 Aurelia Turbines Oy Two-spool gas turbine arrangement
GB2536878A (en) * 2015-03-23 2016-10-05 Aurelia Turbines Oy Multi-spool gas turbine arrangement
US10450080B1 (en) * 2016-03-28 2019-10-22 United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration Variable frequency power system for hybrid electric aircraft propulsion
US10003239B1 (en) * 2016-12-16 2018-06-19 General Electric Company Doubly-fed induction generator system for a gas turbine
US10207592B1 (en) * 2017-11-01 2019-02-19 GM Global Technology Operations LLC Autonomous hybrid power generation platform
GB201804128D0 (en) * 2018-03-15 2018-05-02 Rolls Royce Plc Electrical power generator system
JP2020183733A (ja) * 2019-05-09 2020-11-12 三菱重工業株式会社 ターボクラスターガスタービンシステム及びその起動方法
FR3107558B1 (fr) * 2020-02-26 2024-08-23 Psa Automobiles Sa Systeme thermodynamique comportant deux turbomachines presentant chacune un arbre de transmission et une machine electrique
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Also Published As

Publication number Publication date
GB201504839D0 (en) 2015-05-06
EP3274562A1 (en) 2018-01-31
US10458269B2 (en) 2019-10-29
GB2536878A (en) 2016-10-05
EP3274562B1 (en) 2019-01-23
US20180058242A1 (en) 2018-03-01
HK1249158B (en) 2019-12-06
WO2016151198A1 (en) 2016-09-29
RU2704386C2 (ru) 2019-10-28
RU2017136584A (ru) 2019-04-23
RU2017136584A3 (es) 2019-08-22

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