JPS4724483Y1 - - Google Patents

Info

Publication number
JPS4724483Y1
JPS4724483Y1 JP1970129344U JP12934470U JPS4724483Y1 JP S4724483 Y1 JPS4724483 Y1 JP S4724483Y1 JP 1970129344 U JP1970129344 U JP 1970129344U JP 12934470 U JP12934470 U JP 12934470U JP S4724483 Y1 JPS4724483 Y1 JP S4724483Y1
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.)
Expired
Application number
JP1970129344U
Other languages
Japanese (ja)
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
Priority to JP1970129344U priority Critical patent/JPS4724483Y1/ja
Priority to GB5560471A priority patent/GB1376147A/en
Priority to US00203546A priority patent/US3792581A/en
Publication of JPS4724483Y1 publication Critical patent/JPS4724483Y1/ja
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/34—Gas-turbine plants characterised by the use of combustion products as the working fluid with recycling of part of the working fluid, i.e. semi-closed cycles with combustion products in the closed part of the cycle
    • 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
    • F23R3/346—Feeding into different combustion zones for staged combustion

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Supercharger (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
JP1970129344U 1970-12-22 1970-12-22 Expired JPS4724483Y1 (sv)

Priority Applications (3)

Application Number Priority Date Filing Date Title
JP1970129344U JPS4724483Y1 (sv) 1970-12-22 1970-12-22
GB5560471A GB1376147A (en) 1970-12-22 1971-11-30 System and method for minimizing nitrogen oxide emission by a gas turbine engine
US00203546A US3792581A (en) 1970-12-22 1971-12-01 System and method used in a gas turbine engine for minimizing nitrogen oxide emission

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1970129344U JPS4724483Y1 (sv) 1970-12-22 1970-12-22

Publications (1)

Publication Number Publication Date
JPS4724483Y1 true JPS4724483Y1 (sv) 1972-08-02

Family

ID=15007274

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1970129344U Expired JPS4724483Y1 (sv) 1970-12-22 1970-12-22

Country Status (3)

Country Link
US (1) US3792581A (sv)
JP (1) JPS4724483Y1 (sv)
GB (1) GB1376147A (sv)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3846979A (en) * 1971-12-17 1974-11-12 Engelhard Min & Chem Two stage combustion process
GB1454280A (en) * 1972-11-28 1976-11-03 Nissan Motor Combustible mixture supply system
US3872664A (en) * 1973-10-15 1975-03-25 United Aircraft Corp Swirl combustor with vortex burning and mixing
US3901026A (en) * 1973-11-05 1975-08-26 Gen Motors Corp Gas turbine with auxiliary gasifier engine
GB1498034A (en) * 1974-05-14 1978-01-18 Secr Defence Dinghies
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
US3937008A (en) * 1974-12-18 1976-02-10 United Technologies Corporation Low emission combustion chamber
US3973390A (en) * 1974-12-18 1976-08-10 United Technologies Corporation Combustor employing serially staged pilot combustion, fuel vaporization, and primary combustion zones
US4058977A (en) * 1974-12-18 1977-11-22 United Technologies Corporation Low emission combustion chamber
US3973395A (en) * 1974-12-18 1976-08-10 United Technologies Corporation Low emission combustion chamber
US4045956A (en) * 1974-12-18 1977-09-06 United Technologies Corporation Low emission combustion chamber
US4012904A (en) * 1975-07-17 1977-03-22 Chrysler Corporation Gas turbine burner
US4083181A (en) * 1976-06-14 1978-04-11 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Gas turbine engine with recirculating bleed
JPS5741524A (en) * 1980-08-25 1982-03-08 Hitachi Ltd Combustion method of gas turbine and combustor for gas turbine
SE423742B (sv) * 1980-09-29 1982-05-24 United Motor & Transmissions A Gasturbinanleggning for automotiv drift
JPH076630B2 (ja) * 1988-01-08 1995-01-30 株式会社日立製作所 ガスタービン燃焼器
US5216876A (en) * 1990-11-05 1993-06-08 Consolidated Natural Gas Service Company, Inc. Method for reducing nitrogen oxide emissions from gas turbines
US5199255A (en) * 1991-04-03 1993-04-06 Nalco Fuel Tech Selective gas-phase nox reduction in gas turbines
DE4429757A1 (de) * 1994-08-22 1996-02-29 Abb Management Ag Brennkammer
US6192689B1 (en) 1998-03-18 2001-02-27 General Electric Company Reduced emissions gas turbine combustor
US8631657B2 (en) * 2003-01-22 2014-01-21 Vast Power Portfolio, Llc Thermodynamic cycles with thermal diluent
CA2537926C (en) * 2003-09-05 2011-01-11 Delavan Inc. Pilot combustor for stabilizing combustion in gas turbine engines
US8397482B2 (en) * 2008-05-15 2013-03-19 General Electric Company Dry 3-way catalytic reduction of gas turbine NOx
US20100180565A1 (en) * 2009-01-16 2010-07-22 General Electric Company Methods for increasing carbon dioxide content in gas turbine exhaust and systems for achieving the same
NL2005381C2 (en) * 2010-09-21 2012-03-28 Micro Turbine Technology B V Combustor with a single limited fuel-air mixing burner and recuperated micro gas turbine.
US8720179B2 (en) 2011-10-07 2014-05-13 General Electric Company Power plant including an exhaust gas recirculation system for injecting recirculated exhaust gases in the fuel and compressed air of a gas turbine engine

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2721444A (en) * 1948-09-21 1955-10-25 Johnson Horace James Series-type multiple ram jet propulsion system
US2773350A (en) * 1950-01-31 1956-12-11 Hillard E Barrett Combustion chamber assembly for ram jet fuel burner
NL98183C (sv) * 1954-11-24
US2913874A (en) * 1955-03-30 1959-11-24 Gen Electric Tailpipe thrust augmentor
DE1074920B (de) * 1955-07-07 1960-02-04 Ing habil Fritz A F Schmidt Murnau Dr (Obb) Verfahren und \ orrichtung zur Regelung von Gas turbmenbrennkammern mit unterteilter Verbrennung und mehreren Druckstufen
GB1225759A (sv) * 1967-10-05 1971-03-24
US3656298A (en) * 1970-11-27 1972-04-18 Gen Motors Corp Combustion apparatus
US3705492A (en) * 1971-01-11 1972-12-12 Gen Motors Corp Regenerative gas turbine system

Also Published As

Publication number Publication date
US3792581A (en) 1974-02-19
GB1376147A (en) 1974-12-04

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