JPS5189018A - - Google Patents

Info

Publication number
JPS5189018A
JPS5189018A JP50151740A JP15174075A JPS5189018A JP S5189018 A JPS5189018 A JP S5189018A JP 50151740 A JP50151740 A JP 50151740A JP 15174075 A JP15174075 A JP 15174075A JP S5189018 A JPS5189018 A JP S5189018A
Authority
JP
Japan
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.)
Pending
Application number
JP50151740A
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 filed Critical
Publication of JPS5189018A publication Critical patent/JPS5189018A/ja
Pending legal-status Critical Current

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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00—Combustion technologies with mitigation potential
    • Y02E20/34—Indirect CO2mitigation, i.e. by acting on non CO2directly related matters of the process, e.g. pre-heating or heat recovery

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Air Supply (AREA)
JP50151740A 1974-12-18 1975-12-18 Pending JPS5189018A (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/533,921 US3973390A (en) 1974-12-18 1974-12-18 Combustor employing serially staged pilot combustion, fuel vaporization, and primary combustion zones

Publications (1)

Publication Number Publication Date
JPS5189018A true JPS5189018A (ja) 1976-08-04

Family

ID=24127990

Family Applications (1)

Application Number Title Priority Date Filing Date
JP50151740A Pending JPS5189018A (ja) 1974-12-18 1975-12-18

Country Status (9)

Country Link
US (1) US3973390A (ja)
JP (1) JPS5189018A (ja)
CA (1) CA1051674A (ja)
CH (1) CH618780A5 (ja)
DE (1) DE2555007A1 (ja)
FR (1) FR2295235A1 (ja)
GB (1) GB1530146A (ja)
IT (1) IT1054444B (ja)
SE (1) SE7513777L (ja)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS56135734A (en) * 1980-02-19 1981-10-23 Gen Electric Low profile fuel injector

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4201047A (en) * 1976-06-10 1980-05-06 Morgan J Randolph Low emission combustors
US4145879A (en) * 1977-12-15 1979-03-27 United Technologies Corp. Modified vorbix burner concept
US4145880A (en) * 1977-12-15 1979-03-27 United Technologies Corp. Vorbix augmenter configuration with diffuser and vorbix swirler
US4226083A (en) * 1978-01-19 1980-10-07 United Technologies Corporation Method and apparatus for reducing nitrous oxide emissions from combustors
US4215535A (en) * 1978-01-19 1980-08-05 United Technologies Corporation Method and apparatus for reducing nitrous oxide emissions from combustors
US4249373A (en) * 1978-01-28 1981-02-10 Rolls-Royce Ltd. Gas turbine engine
US4253301A (en) * 1978-10-13 1981-03-03 General Electric Company Fuel injection staged sectoral combustor for burning low-BTU fuel gas
GB2040031B (en) * 1979-01-12 1983-02-09 Gen Electric Dual stage-dual mode low emission gas turbine combustion system
GB2043868B (en) * 1979-03-08 1982-12-15 Rolls Royce Gas turbine
DE2937631A1 (de) * 1979-09-18 1981-04-02 Daimler-Benz Ag, 7000 Stuttgart Brennkammer fuer gasturbinen
JPS5741524A (en) * 1980-08-25 1982-03-08 Hitachi Ltd Combustion method of gas turbine and combustor for gas turbine
DE3331989A1 (de) * 1983-09-05 1985-04-04 L. & C. Steinmüller GmbH, 5270 Gummersbach Verfahren zur verminderung der no(pfeil abwaerts)x(pfeil abwaerts)-emission bei der verbrennung von stickstoffhaltigen brennstoffen
EP0210462B1 (de) * 1985-07-30 1989-03-15 BBC Brown Boveri AG Dualbrenner
US4967562A (en) * 1988-12-12 1990-11-06 Sundstrand Corporation Turbine engine with high efficiency fuel atomization
US5205117A (en) * 1989-12-21 1993-04-27 Sundstrand Corporation High altitude starting two-stage fuel injection
US5261224A (en) * 1989-12-21 1993-11-16 Sundstrand Corporation High altitude starting two-stage fuel injection apparatus
US5092128A (en) * 1989-12-22 1992-03-03 Sundstrand Corporation Stored energy combustor
US5216876A (en) * 1990-11-05 1993-06-08 Consolidated Natural Gas Service Company, Inc. Method for reducing nitrogen oxide emissions from gas turbines
US5207064A (en) * 1990-11-21 1993-05-04 General Electric Company Staged, mixed combustor assembly having low emissions
US5685156A (en) * 1996-05-20 1997-11-11 Capstone Turbine Corporation Catalytic combustion system
US5983642A (en) * 1997-10-13 1999-11-16 Siemens Westinghouse Power Corporation Combustor with two stage primary fuel tube with concentric members and flow regulating
US6286298B1 (en) * 1998-12-18 2001-09-11 General Electric Company Apparatus and method for rich-quench-lean (RQL) concept in a gas turbine engine combustor having trapped vortex cavity
US6295801B1 (en) * 1998-12-18 2001-10-02 General Electric Company Fuel injector bar for gas turbine engine combustor having trapped vortex cavity
US6453658B1 (en) 2000-02-24 2002-09-24 Capstone Turbine Corporation Multi-stage multi-plane combustion system for a gas turbine engine
EP1659339A1 (de) * 2004-11-18 2006-05-24 Siemens Aktiengesellschaft Verfahren zum Anfahren eines Brenners
US8511094B2 (en) * 2006-06-16 2013-08-20 Siemens Energy, Inc. Combustion apparatus using pilot fuel selected for reduced emissions
US8769955B2 (en) * 2010-06-02 2014-07-08 Siemens Energy, Inc. Self-regulating fuel staging port for turbine combustor
US9194586B2 (en) * 2011-12-07 2015-11-24 Pratt & Whitney Canada Corp. Two-stage combustor for gas turbine engine
US9062609B2 (en) 2012-01-09 2015-06-23 Hamilton Sundstrand Corporation Symmetric fuel injection for turbine combustor
US20130180248A1 (en) * 2012-01-18 2013-07-18 Nishant Govindbhai Parsania Combustor Nozzle/Premixer with Curved Sections
US9677766B2 (en) * 2012-11-28 2017-06-13 General Electric Company Fuel nozzle for use in a turbine engine and method of assembly
US9677513B2 (en) 2014-07-08 2017-06-13 David L. Wilson Mechanically induced vacuum driven delivery system providing pre-vaporized fuel to an internal combustion engine
CN113432150B (zh) * 2021-06-29 2022-04-22 中国人民解放军国防科技大学 可控火焰稳定器、发动机以及飞行器

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2955420A (en) * 1955-09-12 1960-10-11 Phillips Petroleum Co Jet engine operation
US3046731A (en) * 1955-10-07 1962-07-31 Edward Pohlmann Flame stabilization in jet engines
US2922279A (en) * 1956-02-02 1960-01-26 Power Jets Res & Dev Ltd Combustion apparatus and ignitor employing vaporized fuel
FR1166154A (fr) * 1957-02-01 1958-11-04 Snecma Brûleur à semi-vaporisation
US2974487A (en) * 1957-10-19 1961-03-14 Bristol Siddeley Engines Ltd Combustion system for a gas turbine engine
GB854135A (en) * 1958-03-05 1960-11-16 Rolls Royce Improvements in or relating to combustion equipment
FR1206830A (fr) * 1958-05-19 1960-02-11 Rolls Royce Perfectionnements aux appareillages de combustion des moteurs à turbine à gaz
US3074668A (en) * 1958-12-10 1963-01-22 Snecma Burner for hot fuel
US3531937A (en) * 1968-09-24 1970-10-06 Curtiss Wright Corp Fuel vaporizer for gas turbine engines
GB1357533A (en) * 1970-09-11 1974-06-26 Lucas Industries Ltd Combustion equipment for gas turbine engines
US3788065A (en) * 1970-10-26 1974-01-29 United Aircraft Corp Annular combustion chamber for dissimilar fluids in swirling flow relationship
JPS4724483Y1 (ja) * 1970-12-22 1972-08-02
DE2403657A1 (de) * 1973-02-28 1974-09-12 United Aircraft Corp Brennkammer mit vormischung fuer gasturbinentriebwerke
US3872664A (en) * 1973-10-15 1975-03-25 United Aircraft Corp Swirl combustor with vortex burning and mixing
GB1489339A (en) * 1973-11-30 1977-10-19 Rolls Royce Gas turbine engine combustion chambers
FR2289738A2 (fr) * 1974-10-30 1976-05-28 Engelhard Min & Chem Procede et appareillage d'obtention d'une combustion entretenue dans une turbine a gaz

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS56135734A (en) * 1980-02-19 1981-10-23 Gen Electric Low profile fuel injector
JPH0232463B2 (ja) * 1980-02-19 1990-07-20 Gen Electric

Also Published As

Publication number Publication date
US3973390A (en) 1976-08-10
FR2295235A1 (fr) 1976-07-16
GB1530146A (en) 1978-10-25
CA1051674A (en) 1979-04-03
DE2555007A1 (de) 1976-07-01
SE7513777L (sv) 1976-06-21
CH618780A5 (ja) 1980-08-15
IT1054444B (it) 1981-11-10

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