IT1400384B1 - Gruppo bruciatore per una camera di combustione di un impianto a turbina a gas, camera di combustione comprendente detto gruppo bruciatore e metodo per operare detto gruppo bruciatore. - Google Patents

Gruppo bruciatore per una camera di combustione di un impianto a turbina a gas, camera di combustione comprendente detto gruppo bruciatore e metodo per operare detto gruppo bruciatore.

Info

Publication number
IT1400384B1
IT1400384B1 ITMI2010A000942A ITMI20100942A IT1400384B1 IT 1400384 B1 IT1400384 B1 IT 1400384B1 IT MI2010A000942 A ITMI2010A000942 A IT MI2010A000942A IT MI20100942 A ITMI20100942 A IT MI20100942A IT 1400384 B1 IT1400384 B1 IT 1400384B1
Authority
IT
Italy
Prior art keywords
combustion chamber
burner
burner group
group
operate
Prior art date
Application number
ITMI2010A000942A
Other languages
English (en)
Inventor
Pierpaolo Pastorino
Rocco Galella
Pasquale Luigi Di
Original Assignee
Ansaldo Energia Spa
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 Ansaldo Energia Spa filed Critical Ansaldo Energia Spa
Priority to ITMI2010A000942A priority Critical patent/IT1400384B1/it
Publication of ITMI20100942A1 publication Critical patent/ITMI20100942A1/it
Application granted granted Critical
Publication of IT1400384B1 publication Critical patent/IT1400384B1/it

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D11/00Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/10Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour
    • F23D11/101Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting before the burner outlet
    • F23D11/102Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting before the burner outlet in an internal mixing chamber
    • F23D11/103Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting before the burner outlet in an internal mixing chamber with means creating a swirl inside the mixing chamber
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D11/00Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/36Details, e.g. burner cooling means, noise reduction means
    • F23D11/38Nozzles; Cleaning devices therefor
    • F23D11/383Nozzles; Cleaning devices therefor with swirl means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D17/00Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel
    • F23D17/002Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel gaseous or liquid fuel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/286Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34Feeding into different combustion zones
    • F23R3/343Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/36Supply of different fuels

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
ITMI2010A000942A 2010-05-26 2010-05-26 Gruppo bruciatore per una camera di combustione di un impianto a turbina a gas, camera di combustione comprendente detto gruppo bruciatore e metodo per operare detto gruppo bruciatore. IT1400384B1 (it)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ITMI2010A000942A IT1400384B1 (it) 2010-05-26 2010-05-26 Gruppo bruciatore per una camera di combustione di un impianto a turbina a gas, camera di combustione comprendente detto gruppo bruciatore e metodo per operare detto gruppo bruciatore.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ITMI2010A000942A IT1400384B1 (it) 2010-05-26 2010-05-26 Gruppo bruciatore per una camera di combustione di un impianto a turbina a gas, camera di combustione comprendente detto gruppo bruciatore e metodo per operare detto gruppo bruciatore.

Publications (2)

Publication Number Publication Date
ITMI20100942A1 ITMI20100942A1 (it) 2011-11-27
IT1400384B1 true IT1400384B1 (it) 2013-05-31

Family

ID=43598261

Family Applications (1)

Application Number Title Priority Date Filing Date
ITMI2010A000942A IT1400384B1 (it) 2010-05-26 2010-05-26 Gruppo bruciatore per una camera di combustione di un impianto a turbina a gas, camera di combustione comprendente detto gruppo bruciatore e metodo per operare detto gruppo bruciatore.

Country Status (1)

Country Link
IT (1) IT1400384B1 (it)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB632506A (en) * 1946-11-19 1949-11-28 Denis Richard Carlisle Improvements in or relating to fuel-injection nozzles and gas-turbine fuel-systems
FR1535474A (fr) * 1967-03-17 1968-08-09 Procédé de régulation d'un fluide par adjonction d'un débit de fluide auxiliaire et ses applications industrielles, en particulier aux injecteurs
KR100234569B1 (ko) * 1991-04-25 1999-12-15 피터 토마스 석탄가스 및 다른연료의 저공해 연소를 위한 버너장치
DE19653059A1 (de) * 1996-12-19 1998-06-25 Asea Brown Boveri Verfahren zum Betrieb eines Brenners

Also Published As

Publication number Publication date
ITMI20100942A1 (it) 2011-11-27

Similar Documents

Publication Publication Date Title
IT1399989B1 (it) Gruppo di iniezione per un combustore di una turbina a gas
EP2696139A4 (en) BURNERS, SOLID-DRIVEN BURNERS, SOLID-DRIVEN BOILERS, BOILERS AND OPERATING PROCESSES FOR THE BOILER
BRPI1013228A2 (pt) método de geração de vapor direto usando un combustor de oxicombustível
GB2498006B (en) Gas turbine engine systems
SG11201403015WA (en) Geared turbofan gas turbine engine architecture
SG11201402667QA (en) Geared turbofan gas turbine engine architecture
SG11201403012PA (en) Geared turbofan gas turbine engine architecture
SG11201402823TA (en) Geared turbofan gas turbine engine architecture
EP2900977A4 (en) GAS TURBINE ENGINE COMBUSTION CHAMBER
GB2470282B (en) Flameless combustion systems for gas turbine engines
EP2730845A4 (en) COMBUSTION CHAMBER FOR GAS TURBINE
SG11201402824RA (en) Geared turbofan gas turbine engine architecture
SG11201403011RA (en) Geared turbofan gas turbine engine architecture
EP2754963A4 (en) GAS TURBINE COMBUSTION CHAMBER
EP2716396A4 (en) HOLLOWED CROPPED PLATE, MANUFACTURING PROCESS AND BURNER FOR A GAS TURBINE
EP2799770A4 (en) BIOMASS COMBUSTION BURNER ONLY, BIOMASS MIXED COMBUSTION BOILER, AND BIOMASS FUEL COMBUSTION METHOD
EP2716976A4 (en) GAS TURBINE COMBUSTION CHAMBER
EP2713013A4 (en) GAS TURBINE ENGINE
PL2718627T3 (pl) Pierścieniowa komora spalania maszyny wirowej
EP2781838A4 (en) COMBUSTION CHAMBER FOR GAS TURBINE
BR112012002447A2 (pt) câmara de combustão de turbomáquina ,e, turbomáquina.
PL2748532T3 (pl) Pierścieniowa ścianka komory spalania maszyny wirowej
PL2783159T3 (pl) Komora spalania w turbinie gazowej
RS56483B1 (sr) Postupak optimizacije naknadnog sagorevanja gasova postrojenja za sagorevanje
IT1397226B1 (it) Metodo di manutenzione di una camera di combustione di un impianto a turbina a gas.