FR2206441A1 - - Google Patents

Info

Publication number
FR2206441A1
FR2206441A1 FR7340018A FR7340018A FR2206441A1 FR 2206441 A1 FR2206441 A1 FR 2206441A1 FR 7340018 A FR7340018 A FR 7340018A FR 7340018 A FR7340018 A FR 7340018A FR 2206441 A1 FR2206441 A1 FR 2206441A1
Authority
FR
France
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.)
Granted
Application number
FR7340018A
Other languages
French (fr)
Other versions
FR2206441B1 (en
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Publication of FR2206441A1 publication Critical patent/FR2206441A1/fr
Application granted granted Critical
Publication of FR2206441B1 publication Critical patent/FR2206441B1/fr
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F23R3/10Air inlet arrangements for primary air
    • F23R3/12Air inlet arrangements for primary air inducing a vortex
    • F23R3/14Air inlet arrangements for primary air inducing a vortex by using swirl vanes
FR7340018A 1972-11-09 1973-11-09 Expired FR2206441B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11161972A JPS5342897B2 (en) 1972-11-09 1972-11-09

Publications (2)

Publication Number Publication Date
FR2206441A1 true FR2206441A1 (en) 1974-06-07
FR2206441B1 FR2206441B1 (en) 1976-06-25

Family

ID=14565900

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7340018A Expired FR2206441B1 (en) 1972-11-09 1973-11-09

Country Status (8)

Country Link
US (1) US3886736A (en)
JP (1) JPS5342897B2 (en)
CA (1) CA985514A (en)
CH (1) CH560356A5 (en)
DE (1) DE2355127C2 (en)
FR (1) FR2206441B1 (en)
GB (1) GB1450190A (en)
IT (1) IT996392B (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2369418A1 (en) * 1976-10-27 1978-05-26 Gen Electric FUEL INJECTOR FOR GAS TURBINE
FR2495229A1 (en) * 1980-12-02 1982-06-04 United Technologies Corp DOUBLE OPEN FUEL INJECTION NOZZLE FOR GAS TURBINE ENGINE
EP0747636A2 (en) * 1995-06-05 1996-12-11 Allison Engine Company, Inc. Dry low emission combustor for gas turbine engines
WO1998033012A1 (en) * 1997-01-24 1998-07-30 Siemens Westinghouse Power Corporation Atomizing dual fuel nozzle for a combustion turbine

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5412607U (en) * 1977-06-29 1979-01-26
DE3026832A1 (en) * 1980-07-16 1982-02-11 Klöckner-Humboldt-Deutz AG, 5000 Köln SPRAYER NOZZLE FOR CONTINUOUS FUEL INJECTION
US4395874A (en) * 1980-12-02 1983-08-02 United Technologies Corporation Fuel nozzles with water injection for gas turbine engines
CA1259197A (en) * 1985-02-13 1989-09-12 Alan D. Bennett High reliability fuel oil nozzle for a gas turbine
US4996837A (en) * 1987-12-28 1991-03-05 Sundstrand Corporation Gas turbine with forced vortex fuel injection
US5040371A (en) * 1988-12-12 1991-08-20 Sundstrand Corporation Fuel injectors for use with combustors
US5224333A (en) * 1990-03-13 1993-07-06 Delavan Inc Simplex airblast fuel injection
US5115634A (en) * 1990-03-13 1992-05-26 Delavan Inc. Simplex airblade fuel injection method
US5309709A (en) * 1992-06-25 1994-05-10 Solar Turbines Incorporated Low emission combustion system for a gas turbine engine
US5288021A (en) * 1992-08-03 1994-02-22 Solar Turbines Incorporated Injection nozzle tip cooling
US5467926A (en) * 1994-02-10 1995-11-21 Solar Turbines Incorporated Injector having low tip temperature
US6082113A (en) * 1998-05-22 2000-07-04 Pratt & Whitney Canada Corp. Gas turbine fuel injector
US6289676B1 (en) 1998-06-26 2001-09-18 Pratt & Whitney Canada Corp. Simplex and duplex injector having primary and secondary annular lud channels and primary and secondary lud nozzles
US6533954B2 (en) 2000-02-28 2003-03-18 Parker-Hannifin Corporation Integrated fluid injection air mixing system
US6550696B2 (en) 2000-02-28 2003-04-22 Adel B. Mansour Integrated fuel injection and mixing system with impingement cooling face
US7117678B2 (en) * 2004-04-02 2006-10-10 Pratt & Whitney Canada Corp. Fuel injector head
US8146365B2 (en) * 2007-06-14 2012-04-03 Pratt & Whitney Canada Corp. Fuel nozzle providing shaped fuel spray
DE102008026459A1 (en) * 2008-06-03 2009-12-10 E.On Ruhrgas Ag Burner for combustion device in gas turbine system, has plate shaped element arranged in fuel injector, and including fuel passage openings that are arranged in rings and displaced to each other in radial direction
US8505304B2 (en) * 2008-12-01 2013-08-13 General Electric Company Fuel nozzle detachable burner tube with baffle plate assembly
US8893500B2 (en) 2011-05-18 2014-11-25 Solar Turbines Inc. Lean direct fuel injector
US8919132B2 (en) 2011-05-18 2014-12-30 Solar Turbines Inc. Method of operating a gas turbine engine
US9182124B2 (en) 2011-12-15 2015-11-10 Solar Turbines Incorporated Gas turbine and fuel injector for the same
KR101371291B1 (en) * 2012-05-04 2014-03-07 고등기술연구원연구조합 Non-slagging and partial-slagging gasifier
US10619855B2 (en) * 2012-09-06 2020-04-14 United Technologies Corporation Fuel delivery system with a cavity coupled fuel injector
US9284933B2 (en) * 2013-03-01 2016-03-15 Delavan Inc Fuel nozzle with discrete jet inner air swirler
US11421883B2 (en) 2020-09-11 2022-08-23 Raytheon Technologies Corporation Fuel injector assembly with a helical swirler passage for a turbine engine
US11754287B2 (en) 2020-09-11 2023-09-12 Raytheon Technologies Corporation Fuel injector assembly for a turbine engine
US11649964B2 (en) 2020-12-01 2023-05-16 Raytheon Technologies Corporation Fuel injector assembly for a turbine engine
US11808455B2 (en) 2021-11-24 2023-11-07 Rtx Corporation Gas turbine engine combustor with integral fuel conduit(s)
US11846249B1 (en) 2022-09-02 2023-12-19 Rtx Corporation Gas turbine engine with integral bypass duct

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2305265A (en) * 1942-05-01 1942-12-15 Letourneau Inc Sealing boot assembly
DE1625948A1 (en) * 1967-12-23 1970-12-03 Bizerba Werke Kraut Kg Wilh Damper for a control element pulsating in a housing
FR2039800A5 (en) * 1969-03-20 1971-01-15 List Hans
FR2149236A5 (en) * 1971-09-03 1973-03-23 List Hans

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2968925A (en) * 1959-11-25 1961-01-24 William E Blevans Fuel nozzle head for anti-coking
US3498055A (en) * 1968-10-16 1970-03-03 United Aircraft Corp Smoke reduction combustion chamber
US3684186A (en) * 1970-06-26 1972-08-15 Ex Cell O Corp Aerating fuel nozzle
JPS4931059Y1 (en) * 1970-11-30 1974-08-22
DE2160675C3 (en) * 1970-12-15 1978-04-20 Mitsubishi Jukogyo K.K., Tokio Burner device for a gas turbine combustion chamber
US3700173A (en) * 1970-12-30 1972-10-24 Combustion Eng Diffuser
US3777983A (en) * 1971-12-16 1973-12-11 Gen Electric Gas cooled dual fuel air atomized fuel nozzle
US3733169A (en) * 1972-02-22 1973-05-15 D Lefebvre Flame retention head assembly

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2305265A (en) * 1942-05-01 1942-12-15 Letourneau Inc Sealing boot assembly
DE1625948A1 (en) * 1967-12-23 1970-12-03 Bizerba Werke Kraut Kg Wilh Damper for a control element pulsating in a housing
FR2039800A5 (en) * 1969-03-20 1971-01-15 List Hans
FR2149236A5 (en) * 1971-09-03 1973-03-23 List Hans

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2369418A1 (en) * 1976-10-27 1978-05-26 Gen Electric FUEL INJECTOR FOR GAS TURBINE
FR2495229A1 (en) * 1980-12-02 1982-06-04 United Technologies Corp DOUBLE OPEN FUEL INJECTION NOZZLE FOR GAS TURBINE ENGINE
EP0747636A2 (en) * 1995-06-05 1996-12-11 Allison Engine Company, Inc. Dry low emission combustor for gas turbine engines
EP0747636A3 (en) * 1995-06-05 1998-09-02 Allison Engine Company, Inc. Dry low emission combustor for gas turbine engines
WO1998033012A1 (en) * 1997-01-24 1998-07-30 Siemens Westinghouse Power Corporation Atomizing dual fuel nozzle for a combustion turbine
US5873237A (en) * 1997-01-24 1999-02-23 Westinghouse Electric Corporation Atomizing dual fuel nozzle for a combustion turbine

Also Published As

Publication number Publication date
FR2206441B1 (en) 1976-06-25
CA985514A (en) 1976-03-16
US3886736A (en) 1975-06-03
CH560356A5 (en) 1975-03-27
DE2355127A1 (en) 1974-05-22
JPS5342897B2 (en) 1978-11-15
GB1450190A (en) 1976-09-22
IT996392B (en) 1975-12-10
JPS4968929A (en) 1974-07-04
DE2355127C2 (en) 1983-11-03

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Legal Events

Date Code Title Description
ST Notification of lapse