FR3110197B1 - Systeme de purge d’un combustible au gaz reactif - Google Patents

Systeme de purge d’un combustible au gaz reactif Download PDF

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Publication number
FR3110197B1
FR3110197B1 FR2004746A FR2004746A FR3110197B1 FR 3110197 B1 FR3110197 B1 FR 3110197B1 FR 2004746 A FR2004746 A FR 2004746A FR 2004746 A FR2004746 A FR 2004746A FR 3110197 B1 FR3110197 B1 FR 3110197B1
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FR
France
Prior art keywords
reactive gas
gas fuel
purge system
fuel purge
combustion chamber
Prior art date
Legal status (The legal status 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 status listed.)
Active
Application number
FR2004746A
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English (en)
Other versions
FR3110197A1 (fr
Inventor
Montagne Pierre
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Technology GmbH
Original Assignee
GE Energy Products France SNC
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 GE Energy Products France SNC filed Critical GE Energy Products France SNC
Priority to FR2004746A priority Critical patent/FR3110197B1/fr
Priority to PCT/EP2021/062428 priority patent/WO2021228820A1/fr
Priority to JP2022567813A priority patent/JP2023524844A/ja
Priority to EP21725481.2A priority patent/EP4150198A1/fr
Priority to US17/924,324 priority patent/US20230184170A1/en
Priority to CN202180035164.6A priority patent/CN115605675A/zh
Publication of FR3110197A1 publication Critical patent/FR3110197A1/fr
Application granted granted Critical
Publication of FR3110197B1 publication Critical patent/FR3110197B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F02C3/30—Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner 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
    • F02C7/22—Fuel supply systems
    • F02C7/222—Fuel flow conduits, e.g. manifolds
    • 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
    • F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F02C3/22—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being gaseous at standard temperature and pressure
    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/48—Control of fuel supply conjointly with another control of the plant
    • F02C9/50—Control of fuel supply conjointly with another control of the plant with control of working fluid flow
    • F02C9/52—Control of fuel supply conjointly with another control of the plant with control of working fluid flow by bleeding or by-passing the working fluid
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)

Abstract

Ce système de purge d’un combustible contenant de l’hydrogène comporte une turbine à gaz. La turbine à gaz comporte au moins une chambre de combustion (20) munie d’au moins un injecteur (52) du combustible, une section d’échappement et un circuit de gaz chauds allant de la chambre de combustion (20) à la section d’échappement. Le système comporte au moins un point d’injection (A, A’) d’air et/ou de gaz inerte disposé sur le circuit de gaz chauds. Figure pour l’abrégé : Fig. 5
FR2004746A 2020-05-14 2020-05-14 Systeme de purge d’un combustible au gaz reactif Active FR3110197B1 (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
FR2004746A FR3110197B1 (fr) 2020-05-14 2020-05-14 Systeme de purge d’un combustible au gaz reactif
PCT/EP2021/062428 WO2021228820A1 (fr) 2020-05-14 2021-05-11 Système pour purger un carburant ayant un gaz réactif
JP2022567813A JP2023524844A (ja) 2020-05-14 2021-05-11 反応性ガスを有する燃料をパージする為のシステム
EP21725481.2A EP4150198A1 (fr) 2020-05-14 2021-05-11 Système pour purger un carburant ayant un gaz réactif
US17/924,324 US20230184170A1 (en) 2020-05-14 2021-05-11 System for purging a fuel having reactive gas
CN202180035164.6A CN115605675A (zh) 2020-05-14 2021-05-11 用于吹扫具有反应性气体的燃料的系统

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2004746 2020-05-14
FR2004746A FR3110197B1 (fr) 2020-05-14 2020-05-14 Systeme de purge d’un combustible au gaz reactif

Publications (2)

Publication Number Publication Date
FR3110197A1 FR3110197A1 (fr) 2021-11-19
FR3110197B1 true FR3110197B1 (fr) 2022-12-23

Family

ID=71894978

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2004746A Active FR3110197B1 (fr) 2020-05-14 2020-05-14 Systeme de purge d’un combustible au gaz reactif

Country Status (6)

Country Link
US (1) US20230184170A1 (fr)
EP (1) EP4150198A1 (fr)
JP (1) JP2023524844A (fr)
CN (1) CN115605675A (fr)
FR (1) FR3110197B1 (fr)
WO (1) WO2021228820A1 (fr)

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3998047A (en) * 1975-04-18 1976-12-21 The United States Of America As Represented By The United States Energy Research And Development Administration Method and apparatus for preventing overspeed in a gas turbine
US5491970A (en) 1994-06-10 1996-02-20 General Electric Co. Method for staging fuel in a turbine between diffusion and premixed operations
EP2119891B1 (fr) * 2008-05-15 2023-09-13 Mitsubishi Heavy Industries, Ltd. Control du débit du fluide moteur d'une turbine à gaz à deux arbres
US20140083078A1 (en) * 2012-09-27 2014-03-27 General Electric Company Method and system for controlling co2 emissions
US9003762B2 (en) * 2012-10-02 2015-04-14 General Electric Company Turbine exhaust plume mitigation system
US10215412B2 (en) * 2012-11-02 2019-02-26 General Electric Company System and method for load control with diffusion combustion in a stoichiometric exhaust gas recirculation gas turbine system
US9611756B2 (en) * 2012-11-02 2017-04-04 General Electric Company System and method for protecting components in a gas turbine engine with exhaust gas recirculation
CN203441604U (zh) * 2013-02-15 2014-02-19 通用电气公司 用于降低燃气涡轮系统中的背压的系统
US20150096306A1 (en) 2013-10-08 2015-04-09 General Electric Company Gas turbine airfoil with cooling enhancement
DE102014209544A1 (de) * 2014-05-20 2015-11-26 Siemens Aktiengesellschaft Turbinenanordnung
US9249723B2 (en) * 2014-06-13 2016-02-02 Bechtel Power Corporation Turbo-compound reheat combined cycle power generation
US9840953B2 (en) * 2015-06-29 2017-12-12 General Electric Company Power generation system exhaust cooling
US10267185B2 (en) * 2015-07-30 2019-04-23 General Electric Company System and method for controlling coolant supply to an exhaust gas
US20170058770A1 (en) * 2015-08-27 2017-03-02 General Electric Company System and method for decoupling steam production dependency from gas turbine load level
US10228141B2 (en) * 2016-03-04 2019-03-12 General Electric Company Fuel supply conduit assemblies
US10865992B2 (en) 2016-12-30 2020-12-15 General Electric Company Fuel injectors and methods of use in gas turbine combustor

Also Published As

Publication number Publication date
EP4150198A1 (fr) 2023-03-22
WO2021228820A1 (fr) 2021-11-18
CN115605675A (zh) 2023-01-13
US20230184170A1 (en) 2023-06-15
FR3110197A1 (fr) 2021-11-19
JP2023524844A (ja) 2023-06-13

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