RU2747655C2 - Горелка промежуточного подогрева для газовой турбины и газовая турбина, содержащая такую горелку промежуточного подогрева - Google Patents

Горелка промежуточного подогрева для газовой турбины и газовая турбина, содержащая такую горелку промежуточного подогрева Download PDF

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Publication number
RU2747655C2
RU2747655C2 RU2017140045A RU2017140045A RU2747655C2 RU 2747655 C2 RU2747655 C2 RU 2747655C2 RU 2017140045 A RU2017140045 A RU 2017140045A RU 2017140045 A RU2017140045 A RU 2017140045A RU 2747655 C2 RU2747655 C2 RU 2747655C2
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RU
Russia
Prior art keywords
burner
gas
gas flow
petal
gas turbine
Prior art date
Application number
RU2017140045A
Other languages
English (en)
Russian (ru)
Other versions
RU2017140045A (ru
RU2017140045A3 (zh
Inventor
Ян Ян
Александр Сергеевич МЯТЛЕВ
Эриберт БЕНЦ
Original Assignee
Ансальдо Энергия Свитзерленд Аг
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Publication date
Application filed by Ансальдо Энергия Свитзерленд Аг filed Critical Ансальдо Энергия Свитзерленд Аг
Priority to RU2017140045A priority Critical patent/RU2747655C2/ru
Priority to EP18206809.8A priority patent/EP3486569B1/en
Priority to CN201811366161.7A priority patent/CN110030582B/zh
Publication of RU2017140045A publication Critical patent/RU2017140045A/ru
Publication of RU2017140045A3 publication Critical patent/RU2017140045A3/ru
Application granted granted Critical
Publication of RU2747655C2 publication Critical patent/RU2747655C2/ru

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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • F23R3/346—Feeding into different combustion zones for staged combustion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46—Details, e.g. noise reduction means
    • F23D14/62—Mixing devices; Mixing tubes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46—Details, e.g. noise reduction means
    • F23D14/70—Baffles or like flow-disturbing devices
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/36—Supply of different fuels
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/38—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising rotary fuel injection means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C2900/00—Special features of, or arrangements for combustion apparatus using fluid fuels or solid fuels suspended in air; Combustion processes therefor
    • F23C2900/07001—Air swirling vanes incorporating fuel injectors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2204/00—Burners adapted for simultaneous or alternative combustion having more than one fuel supply
    • F23D2204/10—Burners adapted for simultaneous or alternative combustion having more than one fuel supply gaseous and liquid fuel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2900/00—Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
    • F23D2900/21—Burners specially adapted for a particular use
    • F23D2900/21003—Burners specially adapted for a particular use for heating or re-burning air or gas in a duct
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03341—Sequential combustion chambers or burners

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)
RU2017140045A 2017-11-17 2017-11-17 Горелка промежуточного подогрева для газовой турбины и газовая турбина, содержащая такую горелку промежуточного подогрева RU2747655C2 (ru)

Priority Applications (3)

Application Number Priority Date Filing Date Title
RU2017140045A RU2747655C2 (ru) 2017-11-17 2017-11-17 Горелка промежуточного подогрева для газовой турбины и газовая турбина, содержащая такую горелку промежуточного подогрева
EP18206809.8A EP3486569B1 (en) 2017-11-17 2018-11-16 Gas turbine for power plant
CN201811366161.7A CN110030582B (zh) 2017-11-17 2018-11-16 用于燃气涡轮的再热喷燃器和包括再热喷燃器的燃气涡轮

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2017140045A RU2747655C2 (ru) 2017-11-17 2017-11-17 Горелка промежуточного подогрева для газовой турбины и газовая турбина, содержащая такую горелку промежуточного подогрева

Publications (3)

Publication Number Publication Date
RU2017140045A RU2017140045A (ru) 2019-05-17
RU2017140045A3 RU2017140045A3 (zh) 2021-03-15
RU2747655C2 true RU2747655C2 (ru) 2021-05-11

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RU2017140045A RU2747655C2 (ru) 2017-11-17 2017-11-17 Горелка промежуточного подогрева для газовой турбины и газовая турбина, содержащая такую горелку промежуточного подогрева

Country Status (3)

Country Link
EP (1) EP3486569B1 (zh)
CN (1) CN110030582B (zh)
RU (1) RU2747655C2 (zh)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2818793C1 (ru) * 2023-10-18 2024-05-06 Николай Борисович Болотин Кольцевая камера сгорания газотурбинного двигателя и способ регулировки режима работы кольцевой камеры сгорания газотурбинного двигателя

Families Citing this family (4)

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US11859539B2 (en) 2021-02-01 2024-01-02 General Electric Company Aircraft propulsion system with inter-turbine burner
EP4206535A1 (en) * 2021-12-30 2023-07-05 Ansaldo Energia Switzerland AG Burner assembly with in-line injectors
US11898755B2 (en) 2022-06-08 2024-02-13 General Electric Company Combustor with a variable volume primary zone combustion chamber
US11835236B1 (en) 2022-07-05 2023-12-05 General Electric Company Combustor with reverse dilution air introduction

Citations (3)

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US5680766A (en) * 1996-01-02 1997-10-28 General Electric Company Dual fuel mixer for gas turbine combustor
EP2522912A1 (en) * 2011-05-11 2012-11-14 Alstom Technology Ltd Flow straightener and mixer
US20170191665A1 (en) * 2012-10-23 2017-07-06 General Electric Technology Gmbh Burner for a can combustor

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RU2531110C2 (ru) * 2010-06-29 2014-10-20 Дженерал Электрик Компани Газотурбинная установка и установка, содержащая лопатки-форсунки (варианты)
EP2725302A1 (en) * 2012-10-25 2014-04-30 Alstom Technology Ltd Reheat burner arrangement
EP2857658A1 (en) * 2013-10-01 2015-04-08 Alstom Technology Ltd Gas turbine with sequential combustion arrangement
EP3023696B1 (en) * 2014-11-20 2019-08-28 Ansaldo Energia Switzerland AG Lobe lance for a gas turbine combustor
EP3056819B1 (en) * 2015-02-11 2020-04-01 Ansaldo Energia Switzerland AG Fuel injection device for a gas turbine
GB201505502D0 (en) * 2015-03-31 2015-05-13 Rolls Royce Plc Combustion equipment
US10815789B2 (en) * 2016-02-13 2020-10-27 General Electric Company Impingement holes for a turbine engine component

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5680766A (en) * 1996-01-02 1997-10-28 General Electric Company Dual fuel mixer for gas turbine combustor
EP2522912A1 (en) * 2011-05-11 2012-11-14 Alstom Technology Ltd Flow straightener and mixer
US20170191665A1 (en) * 2012-10-23 2017-07-06 General Electric Technology Gmbh Burner for a can combustor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2818793C1 (ru) * 2023-10-18 2024-05-06 Николай Борисович Болотин Кольцевая камера сгорания газотурбинного двигателя и способ регулировки режима работы кольцевой камеры сгорания газотурбинного двигателя

Also Published As

Publication number Publication date
EP3486569A1 (en) 2019-05-22
RU2017140045A (ru) 2019-05-17
RU2017140045A3 (zh) 2021-03-15
CN110030582A (zh) 2019-07-19
CN110030582B (zh) 2022-05-13
EP3486569B1 (en) 2022-01-05

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