AR090511A1 - Conjunto de combustor de turbomaquina - Google Patents

Conjunto de combustor de turbomaquina

Info

Publication number
AR090511A1
AR090511A1 ARP130100990A ARP130100990A AR090511A1 AR 090511 A1 AR090511 A1 AR 090511A1 AR P130100990 A ARP130100990 A AR P130100990A AR P130100990 A ARP130100990 A AR P130100990A AR 090511 A1 AR090511 A1 AR 090511A1
Authority
AR
Argentina
Prior art keywords
combustor
combustion chamber
turbomachine
supply nozzle
fluid supply
Prior art date
Application number
ARP130100990A
Other languages
English (en)
Original Assignee
Gen Electric
Exxonmobil Upstream Res Co
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 Gen Electric, Exxonmobil Upstream Res Co filed Critical Gen Electric
Publication of AR090511A1 publication Critical patent/AR090511A1/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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • 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
    • 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
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • 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 
    • F23C7/00—Combustion apparatus characterised by arrangements for air supply
    • F23C7/02—Disposition of air supply not passing through burner
    • 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 
    • F23C9/00—Combustion apparatus characterised by arrangements for returning combustion products or flue gases to the combustion chamber
    • F23C9/08—Combustion apparatus characterised by arrangements for returning combustion products or flue gases to the combustion chamber for reducing temperature in combustion chamber, e.g. for protecting walls of combustion chamber
    • 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
    • F23R3/002—Wall structures
    • 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
    • F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
    • 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
    • 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
    • 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
    • F23C2900/06041—Staged supply of oxidant
    • 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
    • F23R2900/03041—Effusion cooled combustion chamber walls or domes

Landscapes

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

Abstract

Un conjunto de combustor de turbomáquina incluye un cuerpo de combustor, y un revestimiento de combustor dispuesto dentro del cuerpo de combustor. El revestimiento de combustor define una cámara de combustión que tiene un extremo de cabecera y un extremo de descarga. Se disponen una pluralidad de boquillas de combustor en una serie anular en el extremo de cabecera de la cámara de combustión, y se dispone una boquilla de suministro de fluido en forma sustancialmente central dentro de la serie anular en el extremo de cabecera de la cámara de combustión. La boquilla de suministro de fluido incluye una primera porción de extremo que se extiende hacia una segunda porción de extremo a través de una porción de pared. La porción de pared incluye por lo menos una salida de la cámara de combustión. La boquilla de suministro de fluido está configurada para el suministro de un fluido no combustible hacia el interior de por lo menos una de la pluralidad de boquillas de combustor y la cámara de combustión.
ARP130100990A 2012-03-29 2013-03-26 Conjunto de combustor de turbomaquina AR090511A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/RU2012/000232 WO2013147633A1 (en) 2012-03-29 2012-03-29 Turbomachine combustor assembly

Publications (1)

Publication Number Publication Date
AR090511A1 true AR090511A1 (es) 2014-11-19

Family

ID=47116252

Family Applications (1)

Application Number Title Priority Date Filing Date
ARP130100990A AR090511A1 (es) 2012-03-29 2013-03-26 Conjunto de combustor de turbomaquina

Country Status (10)

Country Link
US (2) US20150075171A1 (es)
EP (1) EP2831505B8 (es)
JP (1) JP6002313B2 (es)
CN (1) CN104246371B (es)
AR (1) AR090511A1 (es)
AU (1) AU2012375461B2 (es)
CA (1) CA2868732C (es)
DE (1) DE112012006144T5 (es)
TW (1) TWI607188B (es)
WO (1) WO2013147633A1 (es)

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RU2637609C2 (ru) 2013-02-28 2017-12-05 Эксонмобил Апстрим Рисерч Компани Система и способ для камеры сгорания турбины
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Also Published As

Publication number Publication date
CA2868732C (en) 2017-02-14
AU2012375461A1 (en) 2014-10-16
US20150153044A1 (en) 2015-06-04
US20150075171A1 (en) 2015-03-19
JP6002313B2 (ja) 2016-10-05
JP2015513063A (ja) 2015-04-30
CN104246371A (zh) 2014-12-24
CA2868732A1 (en) 2013-10-03
WO2013147633A1 (en) 2013-10-03
EP2831505B8 (en) 2017-07-19
DE112012006144T5 (de) 2015-01-29
EP2831505A1 (en) 2015-02-04
TWI607188B (zh) 2017-12-01
AU2012375461B2 (en) 2015-10-29
CN104246371B (zh) 2016-06-15
EP2831505B1 (en) 2017-04-12
WO2013147633A8 (en) 2014-10-16
TW201411055A (zh) 2014-03-16

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