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MX2020012111A - Sistema y metodo para mejorar la estabilidad de combustion en una turbina de gas. - Google Patents

Sistema y metodo para mejorar la estabilidad de combustion en una turbina de gas.

Info

Publication number
MX2020012111A
MX2020012111A MX2020012111A MX2020012111A MX2020012111A MX 2020012111 A MX2020012111 A MX 2020012111A MX 2020012111 A MX2020012111 A MX 2020012111A MX 2020012111 A MX2020012111 A MX 2020012111A MX 2020012111 A MX2020012111 A MX 2020012111A
Authority
MX
Mexico
Prior art keywords
combustor
fuel
gas turbine
combustion stability
air
Prior art date
Application number
MX2020012111A
Other languages
English (en)
Inventor
Anup Vasant Sane
Mark Daniel D´Agostini
Original Assignee
Air Prod & Chem
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
Application filed by Air Prod & Chem filed Critical Air Prod & Chem
Publication of MX2020012111A publication Critical patent/MX2020012111A/es

Links

Classifications

    • 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
    • F23R3/343—Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion
    • 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
    • F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial 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
    • 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
    • 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
    • F23D14/20—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone
    • F23D14/22—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other
    • F23D14/24—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other at least one of the fluids being submitted to a swirling motion
    • 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
    • F23D14/32—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid using a mixture of gaseous fuel and pure oxygen or oxygen-enriched air
    • 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
    • F05D2240/00—Components
    • F05D2240/35—Combustors or associated equipment
    • 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
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00—Combustion technologies with mitigation potential
    • Y02E20/34—Indirect CO2mitigation, i.e. by acting on non CO2directly related matters of the process, e.g. pre-heating or heat recovery

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)

Abstract

Un combustor para un motor de turbina de gas que tiene un compresor corriente arriba del combustor y una turbina corriente abajo del combustor. El combustor también incluye una cámara de combustor, un quemador piloto de oxi-combustible (104) centralmente posicionado en un extremo de la cámara de combustor, y un quemador de pre-mezcla de aire-combustible configurado para por lo menos parcialmente pre-mezclar el aire y el combustible. El quemador de pre-mezcla de aire-combustible circunda el quemador piloto de oxi-combustible (104) en una configuración anular.
MX2020012111A 2018-05-15 2019-05-15 Sistema y metodo para mejorar la estabilidad de combustion en una turbina de gas. MX2020012111A (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201862671861P 2018-05-15 2018-05-15
PCT/US2019/032395 WO2019222334A1 (en) 2018-05-15 2019-05-15 System and method of improving combustion stability in a gas turbine

Publications (1)

Publication Number Publication Date
MX2020012111A true MX2020012111A (es) 2021-01-29

Family

ID=67002354

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2020012111A MX2020012111A (es) 2018-05-15 2019-05-15 Sistema y metodo para mejorar la estabilidad de combustion en una turbina de gas.

Country Status (12)

Country Link
US (1) US11592178B2 (es)
EP (1) EP3794283B1 (es)
JP (1) JP7165211B2 (es)
KR (1) KR102429643B1 (es)
CN (1) CN112088277B (es)
CA (1) CA3099915C (es)
ES (1) ES2975239T3 (es)
MX (1) MX2020012111A (es)
PL (1) PL3794283T3 (es)
PT (1) PT3794283T (es)
SA (1) SA520420501B1 (es)
WO (1) WO2019222334A1 (es)

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US11808457B2 (en) 2021-02-25 2023-11-07 Air Products And Chemicals, Inc. Hydrogen injection for enhanced combustion stability in gas turbine systems
PL4298382T3 (pl) 2021-02-25 2025-10-20 Air Products And Chemicals, Inc. Sposób wtryskiwania wodoru do komory spalania zespołu komory spalania układu turbiny gazowej
CN116293805A (zh) * 2023-04-03 2023-06-23 西北工业大学 一种掺氢燃料燃气轮机的多旋流器进气头部结构
GB202307700D0 (en) 2023-05-23 2023-07-05 Rolls Royce Plc An improved combustor apparatus
GB202307702D0 (en) * 2023-05-23 2023-07-05 Rolls Royce Plc An improved combustor apparatus
GB202307701D0 (en) 2023-05-23 2023-07-05 Rolls Royce Plc An improved combustor apparatus
WO2025019010A1 (en) 2023-07-19 2025-01-23 Air Products And Chemicals, Inc. Apparatus and process for reduced formation of nitrogen oxides during combustion
CN121420157A (zh) 2023-07-19 2026-01-27 气体产品与化学公司 用于氧化剂形成的设备和方法
US12492815B2 (en) 2023-07-19 2025-12-09 Air Products And Chemicals, Inc. Apparatus and process for oxidant formation
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US12085020B1 (en) 2023-08-28 2024-09-10 Air Products And Chemicals, Inc. Apparatus and process for gas turbine air filtration and fuel vaporization
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CN120212537B (zh) * 2025-05-30 2025-07-29 中国航发湖南动力机械研究所 一种集成式贫油预混低污染燃烧室

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Also Published As

Publication number Publication date
CN112088277A (zh) 2020-12-15
SA520420501B1 (ar) 2023-01-16
JP2021524011A (ja) 2021-09-09
EP3794283B1 (en) 2024-03-13
ES2975239T3 (es) 2024-07-04
CA3099915C (en) 2023-08-01
WO2019222334A1 (en) 2019-11-21
BR112020022559A2 (pt) 2021-02-02
EP3794283A1 (en) 2021-03-24
PT3794283T (pt) 2024-04-11
KR20200142077A (ko) 2020-12-21
US11592178B2 (en) 2023-02-28
JP7165211B2 (ja) 2022-11-02
CN112088277B (zh) 2022-06-14
KR102429643B1 (ko) 2022-08-04
CA3099915A1 (en) 2019-11-21
US20210222881A1 (en) 2021-07-22
PL3794283T3 (pl) 2024-06-10

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