US3684186A
(en)
*
|
1970-06-26 |
1972-08-15 |
Ex Cell O Corp |
Aerating fuel nozzle
|
FR2122820A5
(en)
*
|
1971-01-22 |
1972-09-01 |
Pillard Freres Cie |
|
GB1377184A
(en)
*
|
1971-02-02 |
1974-12-11 |
Secr Defence |
Gas turbine engine combustion apparatus
|
US3763650A
(en)
*
|
1971-07-26 |
1973-10-09 |
Westinghouse Electric Corp |
Gas turbine temperature profiling structure
|
US3741483A
(en)
*
|
1971-12-10 |
1973-06-26 |
Mitsubishi Heavy Ind Ltd |
Combustion air supply arrangement for gas turbines
|
US3826079A
(en)
*
|
1971-12-15 |
1974-07-30 |
Phillips Petroleum Co |
Combustion method with selective cooling and controlled fuel mixing
|
US3777983A
(en)
*
|
1971-12-16 |
1973-12-11 |
Gen Electric |
Gas cooled dual fuel air atomized fuel nozzle
|
US3866413A
(en)
*
|
1973-01-22 |
1975-02-18 |
Parker Hannifin Corp |
Air blast fuel atomizer
|
US3831854A
(en)
*
|
1973-02-23 |
1974-08-27 |
Hitachi Ltd |
Pressure spray type fuel injection nozzle having air discharge openings
|
FR2253389A5
(en)
*
|
1973-12-04 |
1975-06-27 |
France Etat |
|
US4253301A
(en)
*
|
1978-10-13 |
1981-03-03 |
General Electric Company |
Fuel injection staged sectoral combustor for burning low-BTU fuel gas
|
US4327547A
(en)
*
|
1978-11-23 |
1982-05-04 |
Rolls-Royce Limited |
Fuel injectors
|
US4265615A
(en)
*
|
1978-12-11 |
1981-05-05 |
United Technologies Corporation |
Fuel injection system for low emission burners
|
GB2055186B
(en)
*
|
1979-08-01 |
1983-05-25 |
Rolls Royce |
Gas turbine engine dual fuel injector
|
JPS56124834A
(en)
|
1980-03-05 |
1981-09-30 |
Hitachi Ltd |
Gas-turbine combustor
|
US4470262A
(en)
*
|
1980-03-07 |
1984-09-11 |
Solar Turbines, Incorporated |
Combustors
|
US4373325A
(en)
*
|
1980-03-07 |
1983-02-15 |
International Harvester Company |
Combustors
|
DE3361535D1
(en)
*
|
1982-05-28 |
1986-01-30 |
Bbc Brown Boveri & Cie |
Gas turbine combustion chamber and method of operating it
|
DE3520781A1
(en)
*
|
1985-06-10 |
1986-12-11 |
Stubinen Utveckling AB, Stockholm |
METHOD AND DEVICE FOR BURNING LIQUID AND / OR SOLID FUELS IN POWDERED FORM
|
CH672541A5
(en)
*
|
1986-12-11 |
1989-11-30 |
Bbc Brown Boveri & Cie |
|
US4854127A
(en)
*
|
1988-01-14 |
1989-08-08 |
General Electric Company |
Bimodal swirler injector for a gas turbine combustor
|
US4936090A
(en)
*
|
1988-07-15 |
1990-06-26 |
Sundstrand Corporation |
Assuring reliable starting of turbine engines
|
JP2839777B2
(en)
*
|
1991-12-24 |
1998-12-16 |
株式会社東芝 |
Fuel injection nozzle for gas turbine combustor
|
EP0617779B1
(en)
*
|
1991-12-26 |
1997-09-03 |
Solar Turbines Incorporated |
Low emission combustion nozzle for use with a gas turbine engine
|
US5288021A
(en)
*
|
1992-08-03 |
1994-02-22 |
Solar Turbines Incorporated |
Injection nozzle tip cooling
|
US5423132A
(en)
*
|
1992-09-30 |
1995-06-13 |
Graber; David A. |
Dryer apparatus using hot gases in free standing vortex
|
US5467926A
(en)
*
|
1994-02-10 |
1995-11-21 |
Solar Turbines Incorporated |
Injector having low tip temperature
|
DE19961947A1
(en)
*
|
1999-12-22 |
2001-06-28 |
Bosch Gmbh Robert |
Apparatus, for producing reductant-air mixture, has devices for subjecting air to pressure such that it flows through air feed channel at speed of sound
|
US6405536B1
(en)
*
|
2000-03-27 |
2002-06-18 |
Wu-Chi Ho |
Gas turbine combustor burning LBTU fuel gas
|
US6474071B1
(en)
|
2000-09-29 |
2002-11-05 |
General Electric Company |
Multiple injector combustor
|
US6363726B1
(en)
|
2000-09-29 |
2002-04-02 |
General Electric Company |
Mixer having multiple swirlers
|
US6381964B1
(en)
|
2000-09-29 |
2002-05-07 |
General Electric Company |
Multiple annular combustion chamber swirler having atomizing pilot
|
US6367262B1
(en)
|
2000-09-29 |
2002-04-09 |
General Electric Company |
Multiple annular swirler
|
US6484489B1
(en)
|
2001-05-31 |
2002-11-26 |
General Electric Company |
Method and apparatus for mixing fuel to decrease combustor emissions
|
US6418726B1
(en)
|
2001-05-31 |
2002-07-16 |
General Electric Company |
Method and apparatus for controlling combustor emissions
|
US6487861B1
(en)
*
|
2001-06-05 |
2002-12-03 |
General Electric Company |
Combustor for gas turbine engines with low air flow swirlers
|
US6983645B2
(en)
*
|
2002-08-06 |
2006-01-10 |
Southwest Research Institute |
Method for accelerated aging of catalytic converters incorporating engine cold start simulation
|
US20040007056A1
(en)
*
|
2001-08-06 |
2004-01-15 |
Webb Cynthia C. |
Method for testing catalytic converter durability
|
US7741127B2
(en)
*
|
2001-08-06 |
2010-06-22 |
Southwest Research Institute |
Method for producing diesel exhaust with particulate material for testing diesel engine aftertreatment devices
|
JP4426841B2
(en)
|
2001-08-06 |
2010-03-03 |
サウスウェスト リサーチ インスティテュート |
Method and apparatus for testing the durability of a catalytic converter
|
US7175422B2
(en)
*
|
2001-08-06 |
2007-02-13 |
Southwest Research Institute |
Method for accelerated aging of catalytic converters incorporating injection of volatilized lubricant
|
US7212926B2
(en)
*
|
2002-08-06 |
2007-05-01 |
Southwest Research Institute |
Testing using a non-engine based test system and exhaust product comprising alternative fuel exhaust
|
US7299137B2
(en)
|
2002-08-06 |
2007-11-20 |
Southwest Research Institute |
Method for drive cycle simulation using non-engine based test system
|
US7412335B2
(en)
*
|
2002-08-06 |
2008-08-12 |
Southwest Research Institute |
Component evaluations using non-engine based test system
|
US7007864B2
(en)
*
|
2002-11-08 |
2006-03-07 |
United Technologies Corporation |
Fuel nozzle design
|
JP4653985B2
(en)
*
|
2004-09-02 |
2011-03-16 |
株式会社日立製作所 |
Combustor and gas turbine combustor, and method for supplying air to the combustor
|
US8425224B2
(en)
|
2005-03-17 |
2013-04-23 |
Southwest Research Institute |
Mass air flow compensation for burner-based exhaust gas generation system
|
WO2006101987A2
(en)
*
|
2005-03-17 |
2006-09-28 |
Southwest Research Institute |
Use of recirculated exhaust gas in a burner-based exhaust generation system for reduced fuel consumption and for cooling
|
WO2007019329A2
(en)
*
|
2005-08-05 |
2007-02-15 |
Southwest Research Institute |
Secondary air injector for use with exhaust gas simulation system
|
US7617684B2
(en)
*
|
2007-11-13 |
2009-11-17 |
Opra Technologies B.V. |
Impingement cooled can combustor
|
US20090165435A1
(en)
*
|
2008-01-02 |
2009-07-02 |
Michal Koranek |
Dual fuel can combustor with automatic liquid fuel purge
|
US20110072823A1
(en)
*
|
2009-09-30 |
2011-03-31 |
Daih-Yeou Chen |
Gas turbine engine fuel injector
|
US8365534B2
(en)
|
2011-03-15 |
2013-02-05 |
General Electric Company |
Gas turbine combustor having a fuel nozzle for flame anchoring
|
RU2011115528A
(en)
|
2011-04-21 |
2012-10-27 |
Дженерал Электрик Компани (US) |
FUEL INJECTOR, COMBUSTION CHAMBER AND METHOD OF OPERATION OF THE COMBUSTION CHAMBER
|
JP5486619B2
(en)
*
|
2012-02-28 |
2014-05-07 |
株式会社日立製作所 |
Gas turbine combustor and operation method thereof
|
JP5889754B2
(en)
*
|
2012-09-05 |
2016-03-22 |
三菱日立パワーシステムズ株式会社 |
Gas turbine combustor
|
US9347378B2
(en)
|
2013-05-13 |
2016-05-24 |
Solar Turbines Incorporated |
Outer premix barrel vent air sweep
|
JP7287811B2
(en)
*
|
2019-03-25 |
2023-06-06 |
三菱重工業株式会社 |
Combustor and gas turbine
|