RU2302586C2 - Усовершенствованная огневая труба или "внутренняя облицовка" для камеры сгорания газовой турбины с малым уровнем выброса загрязняющих окружающую среду веществ - Google Patents

Усовершенствованная огневая труба или "внутренняя облицовка" для камеры сгорания газовой турбины с малым уровнем выброса загрязняющих окружающую среду веществ Download PDF

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Publication number
RU2302586C2
RU2302586C2 RU2002134607/06A RU2002134607A RU2302586C2 RU 2302586 C2 RU2302586 C2 RU 2302586C2 RU 2002134607/06 A RU2002134607/06 A RU 2002134607/06A RU 2002134607 A RU2002134607 A RU 2002134607A RU 2302586 C2 RU2302586 C2 RU 2302586C2
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RU
Russia
Prior art keywords
fire tube
holes
improved fire
cylindrical section
chamber
Prior art date
Application number
RU2002134607/06A
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English (en)
Russian (ru)
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RU2002134607A (ru
Inventor
Роберто МОДИ (IT)
Роберто МОДИ
Лучано БОНЧИАНИ (IT)
Лучано БОНЧИАНИ
Джанни ЧЕККЕРИНИ (IT)
Джанни ЧЕККЕРИНИ
Original Assignee
Нуово Пиньоне Холдинг С.П.А.
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.)
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Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=11448750&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=RU2302586(C2) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Нуово Пиньоне Холдинг С.П.А. filed Critical Нуово Пиньоне Холдинг С.П.А.
Publication of RU2002134607A publication Critical patent/RU2002134607A/ru
Application granted granted Critical
Publication of RU2302586C2 publication Critical patent/RU2302586C2/ru

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    • 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
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • 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
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/06Arrangement of apertures along the flame tube
    • 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
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00014Reducing thermo-acoustic vibrations by passive means, e.g. by Helmholtz resonators
    • 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
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03044Impingement cooled combustion chamber walls or subassemblies

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Gas Burners (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
RU2002134607/06A 2001-12-21 2002-12-20 Усовершенствованная огневая труба или "внутренняя облицовка" для камеры сгорания газовой турбины с малым уровнем выброса загрязняющих окружающую среду веществ RU2302586C2 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ITMI2001A002785 2001-12-21
IT2001MI002785A ITMI20012785A1 (it) 2001-12-21 2001-12-21 Tubo di fianna o "liner" migliorato per una camera di combustione di una turbina a gas a basse emissioni inquinanti

Publications (2)

Publication Number Publication Date
RU2002134607A RU2002134607A (ru) 2004-07-20
RU2302586C2 true RU2302586C2 (ru) 2007-07-10

Family

ID=11448750

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2002134607/06A RU2302586C2 (ru) 2001-12-21 2002-12-20 Усовершенствованная огневая труба или "внутренняя облицовка" для камеры сгорания газовой турбины с малым уровнем выброса загрязняющих окружающую среду веществ

Country Status (9)

Country Link
US (1) US6966187B2 (enExample)
EP (1) EP1321713B1 (enExample)
JP (1) JP4362283B2 (enExample)
KR (1) KR100760560B1 (enExample)
CA (1) CA2413655C (enExample)
DE (1) DE60225411T2 (enExample)
IT (1) ITMI20012785A1 (enExample)
RU (1) RU2302586C2 (enExample)
TW (1) TWI312851B (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2731141C2 (ru) * 2015-03-30 2020-08-31 Нуово Пиньоне Текнолоджи Срл Сменное поддерживающее устройство для жаровой трубы камер сгорания газовой турбины

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ITMI20012781A1 (it) * 2001-12-21 2003-06-21 Nuovo Pignone Spa Assieme migliorato di camera di pre miscelamento e di camera di combustione, a basse emissioni inquinanti per turbine a gas con combustibile
ITMI20032621A1 (it) * 2003-12-30 2005-06-30 Nuovo Pignone Spa Sistema di combustione a basse emissioni inquinanti
CA2457609A1 (en) * 2004-02-13 2005-08-13 Alberta Research Council Inc. Heating solid oxide fuel cell stack
US7350619B2 (en) * 2004-09-23 2008-04-01 Honeywell International, Inc. Auxiliary power unit exhaust duct with muffler incorporating an externally replaceable acoustic liner
EP1832812A3 (de) * 2006-03-10 2012-01-04 Rolls-Royce Deutschland Ltd & Co KG Gasturbinenbrennkammerwand mit Dämpfung von Brennkammerschwingungen
US8156743B2 (en) * 2006-05-04 2012-04-17 General Electric Company Method and arrangement for expanding a primary and secondary flame in a combustor
EP2245374B1 (de) * 2008-02-20 2017-11-15 General Electric Technology GmbH Thermische maschine
EP2187125A1 (de) * 2008-09-24 2010-05-19 Siemens Aktiengesellschaft Vorrichtung und Verfahren zur Dämpfung von Verbrennungsschwingungen
US8863525B2 (en) 2011-01-03 2014-10-21 General Electric Company Combustor with fuel staggering for flame holding mitigation
US20120208141A1 (en) * 2011-02-14 2012-08-16 General Electric Company Combustor
EP2644995A1 (en) 2012-03-27 2013-10-02 Siemens Aktiengesellschaft An improved hole arrangement of liners of a combustion chamber of a gas turbine engine with low combustion dynamics and emissions
US20140033726A1 (en) * 2012-08-06 2014-02-06 Wei Chen Liner cooling assembly for a gas turbine system
US10533750B2 (en) 2014-09-05 2020-01-14 Siemens Aktiengesellschaft Cross ignition flame duct
JP7262364B2 (ja) 2019-10-17 2023-04-21 三菱重工業株式会社 ガスタービン燃焼器

Citations (5)

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Publication number Priority date Publication date Assignee Title
GB1486684A (en) * 1974-09-06 1977-09-21 Mitsubishi Heavy Ind Ltd Fuel combustion apparatus
GB1570875A (en) * 1977-03-16 1980-07-09 Lucas Industries Ltd Combustion equipment
US4498288A (en) * 1978-10-13 1985-02-12 General Electric Company Fuel injection staged sectoral combustor for burning low-BTU fuel gas
RU2062406C1 (ru) * 1994-04-28 1996-06-20 Акционерное общество "Авиадвигатель" Камера сгорания газотурбинного двигателя
RU2162988C2 (ru) * 1999-02-22 2001-02-10 Открытое акционерное общество "Авиадвигатель" Камера сгорания газотурбинной установки

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US4201047A (en) * 1976-06-10 1980-05-06 Morgan J Randolph Low emission combustors
FR2381911A1 (fr) * 1977-02-25 1978-09-22 Guidas Chambre de combustion perfectionnee notamment pour une turbine a gaz
US4833881A (en) * 1984-12-17 1989-05-30 General Electric Company Gas turbine engine augmentor
US5287697A (en) * 1992-01-02 1994-02-22 General Electric Company Variable area bypass injector seal
GB2309296B (en) * 1995-10-11 2000-02-09 Europ Gas Turbines Ltd Gas turbine engine combuster
GB2328011A (en) * 1997-08-05 1999-02-10 Europ Gas Turbines Ltd Combustor for gas or liquid fuelled turbine
US6098397A (en) * 1998-06-08 2000-08-08 Caterpillar Inc. Combustor for a low-emissions gas turbine engine
GB9926257D0 (en) * 1999-11-06 2000-01-12 Rolls Royce Plc Wall elements for gas turbine engine combustors
US6446438B1 (en) * 2000-06-28 2002-09-10 Power Systems Mfg., Llc Combustion chamber/venturi cooling for a low NOx emission combustor
US6427446B1 (en) * 2000-09-19 2002-08-06 Power Systems Mfg., Llc Low NOx emission combustion liner with circumferentially angled film cooling holes
JP4610800B2 (ja) * 2001-06-29 2011-01-12 三菱重工業株式会社 ガスタービン燃焼器

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1486684A (en) * 1974-09-06 1977-09-21 Mitsubishi Heavy Ind Ltd Fuel combustion apparatus
GB1570875A (en) * 1977-03-16 1980-07-09 Lucas Industries Ltd Combustion equipment
US4498288A (en) * 1978-10-13 1985-02-12 General Electric Company Fuel injection staged sectoral combustor for burning low-BTU fuel gas
RU2062406C1 (ru) * 1994-04-28 1996-06-20 Акционерное общество "Авиадвигатель" Камера сгорания газотурбинного двигателя
RU2162988C2 (ru) * 1999-02-22 2001-02-10 Открытое акционерное общество "Авиадвигатель" Камера сгорания газотурбинной установки

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2731141C2 (ru) * 2015-03-30 2020-08-31 Нуово Пиньоне Текнолоджи Срл Сменное поддерживающее устройство для жаровой трубы камер сгорания газовой турбины

Also Published As

Publication number Publication date
CA2413655C (en) 2009-11-17
JP2003207133A (ja) 2003-07-25
US20030118963A1 (en) 2003-06-26
CA2413655A1 (en) 2003-06-21
KR100760560B1 (ko) 2007-09-20
EP1321713A2 (en) 2003-06-25
ITMI20012785A1 (it) 2003-06-21
TW200409886A (en) 2004-06-16
US6966187B2 (en) 2005-11-22
DE60225411D1 (de) 2008-04-17
EP1321713B1 (en) 2008-03-05
KR20030053436A (ko) 2003-06-28
JP4362283B2 (ja) 2009-11-11
EP1321713A3 (en) 2004-07-14
DE60225411T2 (de) 2009-03-19
TWI312851B (en) 2009-08-01

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