UA102361C2 - Газотурбинный двигатель, который работает на бедном газовом топливе - Google Patents

Газотурбинный двигатель, который работает на бедном газовом топливе

Info

Publication number
UA102361C2
UA102361C2 UAA201212179A UAA201212179A UA102361C2 UA 102361 C2 UA102361 C2 UA 102361C2 UA A201212179 A UAA201212179 A UA A201212179A UA A201212179 A UAA201212179 A UA A201212179A UA 102361 C2 UA102361 C2 UA 102361C2
Authority
UA
Ukraine
Prior art keywords
gas
turbine
fuel
compressor
extracted
Prior art date
Application number
UAA201212179A
Other languages
English (en)
Ukrainian (uk)
Inventor
Йошихиро Ямасаки
Со КУРОСАКА
Хироюки Кашихара
Original Assignee
Кавасаки Юкогийо Кабушики Кайша
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 Кавасаки Юкогийо Кабушики Кайша filed Critical Кавасаки Юкогийо Кабушики Кайша
Publication of UA102361C2 publication Critical patent/UA102361C2/ru

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N3/00—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
    • F01N3/08—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous
    • 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
    • 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
    • F23R3/40—Continuous combustion chambers using liquid or gaseous fuel characterised by the use of catalytic 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00002—Gas turbine combustors adapted for fuels having low heating value [LHV]

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Exhaust Gas After Treatment (AREA)
  • Supercharger (AREA)

Abstract

Газотурбинный двигатель, который работает на бедном газовом топливе, которое не приводит к ухудшению рабочих характеристик двигателя или потере давления в выхлопной системе, содержит компрессор (1) для сжатия рабочего газа (G1) для получения сжатого газа (G2), причем рабочий газ (G1) имеет концентрацию горючего компонента, меньшую предела его возгорания, каталитическую камеру сгорания (2) для сжигания сжатого газа (G2) каталитической реакцией с помощью помещенного в нее катализатора для получения дымового газа (G3), турбину (3), выполненную для приведения в действие дымовым газом
UAA201212179A 2010-03-24 2011-03-07 Газотурбинный двигатель, который работает на бедном газовом топливе UA102361C2 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2010067271A JP4751950B1 (ja) 2010-03-24 2010-03-24 希薄燃料吸入ガスタービン
PCT/JP2011/055210 WO2011118372A1 (ja) 2010-03-24 2011-03-07 希薄燃料吸入ガスタービン

Publications (1)

Publication Number Publication Date
UA102361C2 true UA102361C2 (ru) 2013-06-25

Family

ID=44597094

Family Applications (1)

Application Number Title Priority Date Filing Date
UAA201212179A UA102361C2 (ru) 2010-03-24 2011-03-07 Газотурбинный двигатель, который работает на бедном газовом топливе

Country Status (7)

Country Link
US (1) US20130276433A1 (ru)
JP (1) JP4751950B1 (ru)
CN (1) CN102933819A (ru)
AU (1) AU2011230790B2 (ru)
RU (1) RU2521179C2 (ru)
UA (1) UA102361C2 (ru)
WO (1) WO2011118372A1 (ru)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2669539C1 (ru) * 2016-09-15 2018-10-11 Эбершпехер Клаймит Контрол Системз Гмбх Унд Ко. Кг Конструктивный узел камеры сгорания для приводимого в действие посредством горючего материала нагревательного прибора транспортного средства

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5314637B2 (ja) * 2010-05-31 2013-10-16 三菱重工業株式会社 ガスエンジン
JP5723455B2 (ja) * 2011-10-17 2015-05-27 川崎重工業株式会社 希薄燃料吸入ガスタービン
WO2013080839A1 (ja) * 2011-11-28 2013-06-06 川崎重工業株式会社 重量構造物の支持機構
JP5183795B1 (ja) * 2011-12-05 2013-04-17 川崎重工業株式会社 希薄燃料吸入ガスタービン
AU2012355051A1 (en) * 2011-12-21 2014-07-10 Kawasaki Jukogyo Kabushiki Kaisha Control method and control device for lean fuel intake gas turbine
CN103998723A (zh) * 2011-12-22 2014-08-20 川崎重工业株式会社 贫燃料吸入燃气涡轮发动机的运转方法及燃气涡轮发电设备
CN103998749A (zh) * 2011-12-22 2014-08-20 川崎重工业株式会社 燃气涡轮发动机及其启动方法
AU2012354936A1 (en) * 2011-12-22 2014-07-17 Kawasaki Jukogyo Kabushiki Kaisha Gas turbine engine provided with heat exchanger, and method for starting same
AU2013282048A1 (en) * 2012-06-25 2015-01-29 Kawasaki Jukogyo Kabushiki Kaisha Oxidation system for treatment of low-concentration methane gas provided with multiple oxidizers
CH708276A1 (de) * 2013-07-04 2015-01-15 Liebherr Machines Bulle Sa Gasmotor.
CA2937162C (en) * 2014-01-17 2022-05-31 Mitsubishi Hitachi Power Systems Americas, Inc. Method and apparatus for operating a gas turbine power plant at low load conditions with stack compliant emissions levels
CN112627989A (zh) * 2021-01-08 2021-04-09 大连欧谱纳透平动力科技有限公司 控制小型燃气轮机排气温度和氮氧化物浓度的系统及方法
GB202215721D0 (en) * 2022-10-24 2022-12-07 Rolls Royce Plc Gas turbine engine fuel system

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4472935A (en) * 1978-08-03 1984-09-25 Gulf Research & Development Company Method and apparatus for the recovery of power from LHV gas
US4858428A (en) * 1986-04-24 1989-08-22 Paul Marius A Advanced integrated propulsion system with total optimized cycle for gas turbines
US4754607A (en) * 1986-12-12 1988-07-05 Allied-Signal Inc. Power generating system
US6107693A (en) * 1997-09-19 2000-08-22 Solo Energy Corporation Self-contained energy center for producing mechanical, electrical, and heat energy
US20020166324A1 (en) * 1998-04-02 2002-11-14 Capstone Turbine Corporation Integrated turbine power generation system having low pressure supplemental catalytic reactor
US6393821B1 (en) * 1998-08-21 2002-05-28 Edan Prabhu Method for collection and use of low-level methane emissions
US6269625B1 (en) * 1999-09-17 2001-08-07 Solo Energy Corporation Methods and apparatus for igniting a catalytic converter in a gas turbine system
RU2284434C2 (ru) * 2002-05-06 2006-09-27 Московский авиационный институт (государственный технический университет) Способ и устройство для сжигания топлив
AU2002951703A0 (en) * 2002-09-27 2002-10-17 Commonwealth Scientific And Industrial Research Organisation A method and system for a combustion of methane
US20040255588A1 (en) * 2002-12-11 2004-12-23 Kare Lundberg Catalytic preburner and associated methods of operation
RU38218U1 (ru) * 2003-12-23 2004-05-27 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И. Баранова" Устройство для подготовки и подачи топливовоздушной смеси в камеру сгорания
US7096667B2 (en) * 2004-01-09 2006-08-29 Siemens Power Generation, Inc. Control of gas turbine for catalyst activation
JP4538077B2 (ja) * 2008-06-13 2010-09-08 川崎重工業株式会社 希薄燃料吸入ガスタービン

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2669539C1 (ru) * 2016-09-15 2018-10-11 Эбершпехер Клаймит Контрол Системз Гмбх Унд Ко. Кг Конструктивный узел камеры сгорания для приводимого в действие посредством горючего материала нагревательного прибора транспортного средства

Also Published As

Publication number Publication date
RU2012145092A (ru) 2014-04-27
JP4751950B1 (ja) 2011-08-17
JP2011196355A (ja) 2011-10-06
AU2011230790A1 (en) 2012-11-08
RU2521179C2 (ru) 2014-06-27
US20130276433A1 (en) 2013-10-24
CN102933819A (zh) 2013-02-13
AU2011230790B2 (en) 2014-09-18
WO2011118372A1 (ja) 2011-09-29

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