SE7513906L - Brennkammare med lag halt av kveveoxider i avgaserna samt forfarande for drift av brennkammaren med eg avgivning av kveveoxider - Google Patents

Brennkammare med lag halt av kveveoxider i avgaserna samt forfarande for drift av brennkammaren med eg avgivning av kveveoxider

Info

Publication number
SE7513906L
SE7513906L SE7513906A SE7513906A SE7513906L SE 7513906 L SE7513906 L SE 7513906L SE 7513906 A SE7513906 A SE 7513906A SE 7513906 A SE7513906 A SE 7513906A SE 7513906 L SE7513906 L SE 7513906L
Authority
SE
Sweden
Prior art keywords
nitrogen oxides
emission
procedure
layer
exhaust gases
Prior art date
Application number
SE7513906A
Other languages
English (en)
Swedish (sv)
Inventor
S J Markowski
R S Reilly
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of SE7513906L publication Critical patent/SE7513906L/xx

Links

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
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • 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
    • 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
    • F23R3/34—Feeding into different combustion zones

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Air Supply (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
SE7513906A 1974-12-18 1975-12-10 Brennkammare med lag halt av kveveoxider i avgaserna samt forfarande for drift av brennkammaren med eg avgivning av kveveoxider SE7513906L (sv)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/534,018 US3937008A (en) 1974-12-18 1974-12-18 Low emission combustion chamber

Publications (1)

Publication Number Publication Date
SE7513906L true SE7513906L (sv) 1976-06-21

Family

ID=24128368

Family Applications (1)

Application Number Title Priority Date Filing Date
SE7513906A SE7513906L (sv) 1974-12-18 1975-12-10 Brennkammare med lag halt av kveveoxider i avgaserna samt forfarande for drift av brennkammaren med eg avgivning av kveveoxider

Country Status (11)

Country Link
US (1) US3937008A (fr)
JP (1) JPS5189017A (fr)
BR (1) BR7508422A (fr)
CA (1) CA1072349A (fr)
CH (1) CH609425A5 (fr)
DE (1) DE2555085A1 (fr)
FR (1) FR2295236A1 (fr)
GB (1) GB1534186A (fr)
IT (1) IT1051100B (fr)
NO (1) NO754248L (fr)
SE (1) SE7513906L (fr)

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4173118A (en) * 1974-08-27 1979-11-06 Mitsubishi Jukogyo Kabushiki Kaisha Fuel combustion apparatus employing staged combustion
GB1600130A (en) * 1977-05-21 1981-10-14 Rolls Royce Combustion systems
US4262486A (en) * 1978-08-19 1981-04-21 Rolls-Royce Limited Combustion chambers
EP0019417B1 (fr) * 1979-05-18 1983-01-12 Rolls-Royce Plc Appareil de combustion pour turbines à gaz
US4445338A (en) * 1981-10-23 1984-05-01 The United States Of America As Represented By The Secretary Of The Navy Swirler assembly for a vorbix augmentor
US4545196A (en) * 1982-07-22 1985-10-08 The Garrett Corporation Variable geometry combustor apparatus
IE54394B1 (en) * 1982-08-19 1989-09-13 Westinghouse Electric Corp Turbine combustor having more uniform mixing of fuel and air for improved downstream combustion
US4720970A (en) * 1982-11-05 1988-01-26 The United States Of America As Represented By The Secretary Of The Air Force Sector airflow variable geometry combustor
US4891936A (en) * 1987-12-28 1990-01-09 Sundstrand Corporation Turbine combustor with tangential fuel injection and bender jets
JPH0684817B2 (ja) * 1988-08-08 1994-10-26 株式会社日立製作所 ガスタービン燃焼器及びその運転方法
US5076053A (en) * 1989-08-10 1991-12-31 United Technologies Corporation Mechanism for accelerating heat release of combusting flows
US5207064A (en) * 1990-11-21 1993-05-04 General Electric Company Staged, mixed combustor assembly having low emissions
US5235813A (en) * 1990-12-24 1993-08-17 United Technologies Corporation Mechanism for controlling the rate of mixing in combusting flows
US5406799A (en) * 1992-06-12 1995-04-18 United Technologies Corporation Combustion chamber
DE4341450A1 (de) * 1993-12-06 1995-06-08 Bmw Rolls Royce Gmbh Strömungsleitkörper für eine Gasturbinen-Brennkammer
US5918465A (en) * 1995-02-03 1999-07-06 Bmw Rolls-Royce Gmbh Flow guiding body for a gas turbine combustion chamber
CA2216115A1 (fr) * 1995-03-08 1996-09-12 Bmw Rolls-Royce Gmbh Chambre de combustion a anneau double et etagement axial pour une turbine a gaz
US5622054A (en) * 1995-12-22 1997-04-22 General Electric Company Low NOx lobed mixer fuel injector
JP4490912B2 (ja) 2002-10-10 2010-06-30 エル・ピィ・ピィ・コンバスチョン・リミテッド・ライアビリティ・カンパニー 燃焼のための液体燃料を気化するためのシステムおよび使用方法
GB2397643A (en) * 2002-12-04 2004-07-28 Alstom A combustion chamber burner including a corrugated burner outlet
CN100552301C (zh) * 2003-09-05 2009-10-21 德拉文公司 燃气轮机引擎的稳定燃烧用导引燃烧器室
WO2006063126A2 (fr) 2004-12-08 2006-06-15 Lpp Combustion, Llc Procede est dispositif de conditionnement de combustibles hydrocarbures liquides
US8529646B2 (en) * 2006-05-01 2013-09-10 Lpp Combustion Llc Integrated system and method for production and vaporization of liquid hydrocarbon fuels for combustion
US8117845B2 (en) * 2007-04-27 2012-02-21 General Electric Company Systems to facilitate reducing flashback/flame holding in combustion systems
US8453454B2 (en) * 2010-04-14 2013-06-04 General Electric Company Coannular oil injection nozzle
US20120067054A1 (en) * 2010-09-21 2012-03-22 Palmer Labs, Llc High efficiency power production methods, assemblies, and systems
EP2522912B1 (fr) * 2011-05-11 2019-03-27 Ansaldo Energia Switzerland AG Redresseur de flux et mélangeur
US8955329B2 (en) * 2011-10-21 2015-02-17 General Electric Company Diffusion nozzles for low-oxygen fuel nozzle assembly and method
US9194586B2 (en) 2011-12-07 2015-11-24 Pratt & Whitney Canada Corp. Two-stage combustor for gas turbine engine
US9243802B2 (en) 2011-12-07 2016-01-26 Pratt & Whitney Canada Corp. Two-stage combustor for gas turbine engine
US9416972B2 (en) 2011-12-07 2016-08-16 Pratt & Whitney Canada Corp. Two-stage combustor for gas turbine engine
US9677766B2 (en) * 2012-11-28 2017-06-13 General Electric Company Fuel nozzle for use in a turbine engine and method of assembly
EP2889542B1 (fr) * 2013-12-24 2019-11-13 Ansaldo Energia Switzerland AG Procédé pour le fonctionnement d'une chambre de combustion pour turbine à gaz et chambre de combustion
DE102014104104A1 (de) 2014-03-25 2015-10-01 Sec Ship's Equipment Centre Bremen Gmbh & Co. Kg Vorrichtung zum Verzurren von Containern
FR3029271B1 (fr) * 2014-11-28 2019-06-21 Safran Aircraft Engines Paroi annulaire de deflection pour systeme d'injection de chambre de combustion de turbomachine offrant une zone etendue d'atomisation de carburant

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3788065A (en) * 1970-10-26 1974-01-29 United Aircraft Corp Annular combustion chamber for dissimilar fluids in swirling flow relationship
JPS4724483Y1 (fr) * 1970-12-22 1972-08-02
DE2301865A1 (de) * 1973-01-15 1974-07-18 Robert Von Dipl Ing Linde Brennkraftmaschine mit aeusserer verbrennung
US3851467A (en) * 1973-07-02 1974-12-03 Gen Motors Corp Recirculating combustion apparatus jet pump
US3872664A (en) * 1973-10-15 1975-03-25 United Aircraft Corp Swirl combustor with vortex burning and mixing
US3930370A (en) * 1974-06-11 1976-01-06 United Technologies Corporation Turbofan engine with augmented combustion chamber using vorbix principle

Also Published As

Publication number Publication date
CH609425A5 (fr) 1979-02-28
GB1534186A (en) 1978-11-29
IT1051100B (it) 1981-04-21
FR2295236A1 (fr) 1976-07-16
DE2555085A1 (de) 1976-06-24
JPS5189017A (fr) 1976-08-04
US3937008A (en) 1976-02-10
BR7508422A (pt) 1976-09-08
CA1072349A (fr) 1980-02-26
NO754248L (fr) 1976-06-21

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