FR3049044B1 - COMBUSTION CHAMBER OF A TURBINE, IN PARTICULAR OF A THERMODYNAMIC CYCLE TURBINE WITH RECUPERATOR, FOR THE PRODUCTION OF ENERGY, PARTICULARLY ELECTRICAL ENERGY. - Google Patents

COMBUSTION CHAMBER OF A TURBINE, IN PARTICULAR OF A THERMODYNAMIC CYCLE TURBINE WITH RECUPERATOR, FOR THE PRODUCTION OF ENERGY, PARTICULARLY ELECTRICAL ENERGY. Download PDF

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Publication number
FR3049044B1
FR3049044B1 FR1652294A FR1652294A FR3049044B1 FR 3049044 B1 FR3049044 B1 FR 3049044B1 FR 1652294 A FR1652294 A FR 1652294A FR 1652294 A FR1652294 A FR 1652294A FR 3049044 B1 FR3049044 B1 FR 3049044B1
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FR
France
Prior art keywords
turbine
energy
recuperator
production
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
FR1652294A
Other languages
French (fr)
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FR3049044A1 (en
Inventor
Hubert BAYA TODA
Jean-Baptiste Michel
Julien THIRIOT
Thomas VALIN
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.)
IFP Energies Nouvelles IFPEN
Original Assignee
IFP Energies Nouvelles IFPEN
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 IFP Energies Nouvelles IFPEN filed Critical IFP Energies Nouvelles IFPEN
Priority to FR1652294A priority Critical patent/FR3049044B1/en
Priority to CN201780016328.4A priority patent/CN108779918B/en
Priority to EP17705924.3A priority patent/EP3430316B1/en
Priority to PCT/EP2017/054167 priority patent/WO2017157631A1/en
Publication of FR3049044A1 publication Critical patent/FR3049044A1/en
Application granted granted Critical
Publication of FR3049044B1 publication Critical patent/FR3049044B1/en
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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
    • F23R3/10—Air inlet arrangements for primary air
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Spray-Type Burners (AREA)

Abstract

La présente invention concerne un chambre de combustion (18) d'une turbine, notamment d'une turbine à cycle thermodynamique avec récupérateur, pour la production d'énergie, en particulier d'énergie électrique, comportant un boîtier (50) logeant un tube à flamme (58) avec une cloison de diffusion (60) portant un stabilisateur de flamme (72) comprenant un diffuseur d'air perforé (78) et un tube mélangeur (88), ladite chambre comportant en outre un moyen d'injection (64) d'au moins un combustible. Selon l'invention, le diffuseur perforé (78) comprend au moins deux rangées circonférentielles (C1, C2) de trous (84; 84a, 84b).The present invention relates to a combustion chamber (18) of a turbine, in particular of a thermodynamic cycle turbine with recuperator, for the production of energy, in particular electrical energy, comprising a housing (50) housing a tube. flame (58) with a diffusion partition (60) carrying a flame stabilizer (72) comprising a perforated air diffuser (78) and a mixing tube (88), said chamber further comprising injection means ( 64) of at least one fuel. According to the invention, the perforated diffuser (78) comprises at least two circumferential rows (C1, C2) of holes (84; 84a, 84b).

FR1652294A 2016-03-18 2016-03-18 COMBUSTION CHAMBER OF A TURBINE, IN PARTICULAR OF A THERMODYNAMIC CYCLE TURBINE WITH RECUPERATOR, FOR THE PRODUCTION OF ENERGY, PARTICULARLY ELECTRICAL ENERGY. Active FR3049044B1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR1652294A FR3049044B1 (en) 2016-03-18 2016-03-18 COMBUSTION CHAMBER OF A TURBINE, IN PARTICULAR OF A THERMODYNAMIC CYCLE TURBINE WITH RECUPERATOR, FOR THE PRODUCTION OF ENERGY, PARTICULARLY ELECTRICAL ENERGY.
CN201780016328.4A CN108779918B (en) 2016-03-18 2017-02-23 Turbine for generating energy and combustion chamber thereof
EP17705924.3A EP3430316B1 (en) 2016-03-18 2017-02-23 Combustion chamber of a turbine, particularly a turbine with a thermodynamic cycle comprising a recuperator, for producing energy, particularly electrical energy
PCT/EP2017/054167 WO2017157631A1 (en) 2016-03-18 2017-02-23 Combustion chamber of a turbine, particularly a turbine with a thermodynamic cycle comprising a recuperator, for producing energy, particularly electrical energy

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1652294A FR3049044B1 (en) 2016-03-18 2016-03-18 COMBUSTION CHAMBER OF A TURBINE, IN PARTICULAR OF A THERMODYNAMIC CYCLE TURBINE WITH RECUPERATOR, FOR THE PRODUCTION OF ENERGY, PARTICULARLY ELECTRICAL ENERGY.
FR1652294 2016-03-18

Publications (2)

Publication Number Publication Date
FR3049044A1 FR3049044A1 (en) 2017-09-22
FR3049044B1 true FR3049044B1 (en) 2019-12-20

Family

ID=55953278

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1652294A Active FR3049044B1 (en) 2016-03-18 2016-03-18 COMBUSTION CHAMBER OF A TURBINE, IN PARTICULAR OF A THERMODYNAMIC CYCLE TURBINE WITH RECUPERATOR, FOR THE PRODUCTION OF ENERGY, PARTICULARLY ELECTRICAL ENERGY.

Country Status (4)

Country Link
EP (1) EP3430316B1 (en)
CN (1) CN108779918B (en)
FR (1) FR3049044B1 (en)
WO (1) WO2017157631A1 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3084447B1 (en) 2018-07-30 2020-07-31 Ifp Energies Now COMBUSTION CHAMBER FOR A GAS TURBINE INTENDED FOR ENERGY PRODUCTION, ESPECIALLY ELECTRICAL ENERGY, INCLUDING ASYMMETRICAL DILUTION HOLES IN A FLAME TUBE.
FR3084450B1 (en) 2018-07-30 2020-07-31 Ifp Energies Now COMBUSTION CHAMBER INCLUDING A PASSAGE SECTION OF A MODIFIED FLAME TUBE IN PARTICULAR FOR A TURBINE INTENDED FOR ENERGY PRODUCTION, ESPECIALLY ELECTRICAL ENERGY
FR3088969B1 (en) 2018-11-27 2021-02-19 Ifp Energies Now Fuel injector with cooling means
FR3119868B1 (en) 2021-02-15 2023-01-13 Ifp Energies Now Combustion system with a tubular combustion chamber and an annular heat exchanger

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2517015A (en) * 1945-05-16 1950-08-01 Bendix Aviat Corp Combustion chamber with shielded fuel nozzle
GB624779A (en) * 1946-01-09 1949-06-16 Bendix Aviat Corp An improved burner for gaseous, liquid or powdered solid fuel
US2621477A (en) * 1948-06-03 1952-12-16 Power Jets Res & Dev Ltd Combustion apparatus having valve controlled passages for preheating the fuel-air mixture
DE1627878A1 (en) 1967-03-14 1970-08-06 Schloemann Ag Device to compensate for the spring deflection on machines, in particular on forging presses or the like.
DE2020416A1 (en) * 1970-04-27 1971-11-11 Motoren Turbinen Union Combustion chamber for gas turbine engines
GB1335134A (en) * 1970-12-05 1973-10-24 Nissan Motor Combustion apparatus of a gas turbine engine
DE10064259B4 (en) * 2000-12-22 2012-02-02 Alstom Technology Ltd. Burner with high flame stability
US6968693B2 (en) * 2003-09-22 2005-11-29 General Electric Company Method and apparatus for reducing gas turbine engine emissions
JP4959620B2 (en) * 2007-04-26 2012-06-27 株式会社日立製作所 Combustor and fuel supply method for combustor
NL2005381C2 (en) * 2010-09-21 2012-03-28 Micro Turbine Technology B V Combustor with a single limited fuel-air mixing burner and recuperated micro gas turbine.

Also Published As

Publication number Publication date
EP3430316B1 (en) 2020-10-21
EP3430316A1 (en) 2019-01-23
FR3049044A1 (en) 2017-09-22
WO2017157631A1 (en) 2017-09-21
CN108779918A (en) 2018-11-09
CN108779918B (en) 2020-10-30

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