|
US2922279A
(en)
|
1956-02-02 |
1960-01-26 |
Power Jets Res & Dev Ltd |
Combustion apparatus and ignitor employing vaporized fuel
|
|
US3811274A
(en)
*
|
1972-08-30 |
1974-05-21 |
United Aircraft Corp |
Crossover tube construction
|
|
FR2221621B1
(enExample)
|
1973-03-13 |
1976-09-10 |
Snecma |
|
|
US4045956A
(en)
|
1974-12-18 |
1977-09-06 |
United Technologies Corporation |
Low emission combustion chamber
|
|
US4040252A
(en)
|
1976-01-30 |
1977-08-09 |
United Technologies Corporation |
Catalytic premixing combustor
|
|
US4112676A
(en)
|
1977-04-05 |
1978-09-12 |
Westinghouse Electric Corp. |
Hybrid combustor with staged injection of pre-mixed fuel
|
|
US4253301A
(en)
|
1978-10-13 |
1981-03-03 |
General Electric Company |
Fuel injection staged sectoral combustor for burning low-BTU fuel gas
|
|
US4288980A
(en)
|
1979-06-20 |
1981-09-15 |
Brown Boveri Turbomachinery, Inc. |
Combustor for use with gas turbines
|
|
US4928481A
(en)
|
1988-07-13 |
1990-05-29 |
Prutech Ii |
Staged low NOx premix gas turbine combustor
|
|
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
|
|
US5749219A
(en)
|
1989-11-30 |
1998-05-12 |
United Technologies Corporation |
Combustor with first and second zones
|
|
US5099644A
(en)
|
1990-04-04 |
1992-03-31 |
General Electric Company |
Lean staged combustion assembly
|
|
EP0540167A1
(en)
|
1991-09-27 |
1993-05-05 |
General Electric Company |
A fuel staged premixed dry low NOx combustor
|
|
FR2689567B1
(fr)
|
1992-04-01 |
1994-05-27 |
Snecma |
Injecteur de carburant pour chambre de post-combustion d'une turbomachine.
|
|
JP3335713B2
(ja)
|
1993-06-28 |
2002-10-21 |
株式会社東芝 |
ガスタービン燃焼器
|
|
AU681271B2
(en)
|
1994-06-07 |
1997-08-21 |
Westinghouse Electric Corporation |
Method and apparatus for sequentially staged combustion using a catalyst
|
|
JPH0868301A
(ja)
*
|
1994-08-30 |
1996-03-12 |
Toshiba Corp |
石炭ガス化発電プラント
|
|
RU2098719C1
(ru)
*
|
1995-06-13 |
1997-12-10 |
Акционерное общество "Авиадвигатель" |
Камера сгорания газовой турбины энергетической установки
|
|
RU2111416C1
(ru)
*
|
1995-09-12 |
1998-05-20 |
Акционерное общество "Авиадвигатель" |
Камера сгорания газовой турбины энергетической установки
|
|
US5974781A
(en)
|
1995-12-26 |
1999-11-02 |
General Electric Company |
Hybrid can-annular combustor for axial staging in low NOx combustors
|
|
GB2311596B
(en)
|
1996-03-29 |
2000-07-12 |
Europ Gas Turbines Ltd |
Combustor for gas - or liquid - fuelled turbine
|
|
US6047550A
(en)
|
1996-05-02 |
2000-04-11 |
General Electric Co. |
Premixing dry low NOx emissions combustor with lean direct injection of gas fuel
|
|
US6070406A
(en)
|
1996-11-26 |
2000-06-06 |
Alliedsignal, Inc. |
Combustor dilution bypass system
|
|
US6925809B2
(en)
|
1999-02-26 |
2005-08-09 |
R. Jan Mowill |
Gas turbine engine fuel/air premixers with variable geometry exit and method for controlling exit velocities
|
|
US6253538B1
(en)
|
1999-09-27 |
2001-07-03 |
Pratt & Whitney Canada Corp. |
Variable premix-lean burn combustor
|
|
AU2001272682A1
(en)
*
|
2000-06-15 |
2001-12-24 |
Alstom Power N.V. |
Method for operating a burner and burner with stepped premix gas injection
|
|
US6526756B2
(en)
|
2001-02-14 |
2003-03-04 |
General Electric Company |
Method and apparatus for enhancing heat transfer in a combustor liner for a gas turbine
|
|
GB0219461D0
(en)
|
2002-08-21 |
2002-09-25 |
Rolls Royce Plc |
Fuel injection arrangement
|
|
AU2003284210A1
(en)
|
2002-10-15 |
2004-05-04 |
Vast Power Systems, Inc. |
Method and apparatus for mixing fluids
|
|
US6868676B1
(en)
|
2002-12-20 |
2005-03-22 |
General Electric Company |
Turbine containing system and an injector therefor
|
|
US6935116B2
(en)
|
2003-04-28 |
2005-08-30 |
Power Systems Mfg., Llc |
Flamesheet combustor
|
|
US7028483B2
(en)
*
|
2003-07-14 |
2006-04-18 |
Parker-Hannifin Corporation |
Macrolaminate radial injector
|
|
GB0319329D0
(en)
|
2003-08-16 |
2003-09-17 |
Rolls Royce Plc |
Variable geometry combustor
|
|
US6968693B2
(en)
*
|
2003-09-22 |
2005-11-29 |
General Electric Company |
Method and apparatus for reducing gas turbine engine emissions
|
|
GB0323255D0
(en)
|
2003-10-04 |
2003-11-05 |
Rolls Royce Plc |
Method and system for controlling fuel supply in a combustion turbine engine
|
|
US7425127B2
(en)
|
2004-06-10 |
2008-09-16 |
Georgia Tech Research Corporation |
Stagnation point reverse flow combustor
|
|
WO2005124231A2
(en)
|
2004-06-11 |
2005-12-29 |
Vast Power Systems, Inc. |
Low emissions combustion apparatus and method
|
|
JP2006138566A
(ja)
|
2004-11-15 |
2006-06-01 |
Hitachi Ltd |
ガスタービン燃焼器及びその液体燃料噴射ノズル
|
|
US7237384B2
(en)
|
2005-01-26 |
2007-07-03 |
Peter Stuttaford |
Counter swirl shear mixer
|
|
US7137256B1
(en)
|
2005-02-28 |
2006-11-21 |
Peter Stuttaford |
Method of operating a combustion system for increased turndown capability
|
|
US7966822B2
(en)
|
2005-06-30 |
2011-06-28 |
General Electric Company |
Reverse-flow gas turbine combustion system
|
|
US7878000B2
(en)
|
2005-12-20 |
2011-02-01 |
General Electric Company |
Pilot fuel injector for mixer assembly of a high pressure gas turbine engine
|
|
US7665309B2
(en)
|
2007-09-14 |
2010-02-23 |
Siemens Energy, Inc. |
Secondary fuel delivery system
|
|
US8387398B2
(en)
|
2007-09-14 |
2013-03-05 |
Siemens Energy, Inc. |
Apparatus and method for controlling the secondary injection of fuel
|
|
CN101981381A
(zh)
|
2008-03-31 |
2011-02-23 |
川崎重工业株式会社 |
燃气涡轮燃烧器的冷却结构
|
|
US8516820B2
(en)
|
2008-07-28 |
2013-08-27 |
Siemens Energy, Inc. |
Integral flow sleeve and fuel injector assembly
|
|
US8528340B2
(en)
|
2008-07-28 |
2013-09-10 |
Siemens Energy, Inc. |
Turbine engine flow sleeve
|
|
US8375726B2
(en)
*
|
2008-09-24 |
2013-02-19 |
Siemens Energy, Inc. |
Combustor assembly in a gas turbine engine
|
|
EP2206964A3
(en)
|
2009-01-07 |
2012-05-02 |
General Electric Company |
Late lean injection fuel injector configurations
|
|
US8707707B2
(en)
*
|
2009-01-07 |
2014-04-29 |
General Electric Company |
Late lean injection fuel staging configurations
|
|
US8112216B2
(en)
|
2009-01-07 |
2012-02-07 |
General Electric Company |
Late lean injection with adjustable air splits
|
|
US8689559B2
(en)
*
|
2009-03-30 |
2014-04-08 |
General Electric Company |
Secondary combustion system for reducing the level of emissions generated by a turbomachine
|
|
US8763399B2
(en)
*
|
2009-04-03 |
2014-07-01 |
Hitachi, Ltd. |
Combustor having modified spacing of air blowholes in an air blowhole plate
|
|
US8281594B2
(en)
|
2009-09-08 |
2012-10-09 |
Siemens Energy, Inc. |
Fuel injector for use in a gas turbine engine
|
|
US8991192B2
(en)
|
2009-09-24 |
2015-03-31 |
Siemens Energy, Inc. |
Fuel nozzle assembly for use as structural support for a duct structure in a combustor of a gas turbine engine
|
|
US20110131998A1
(en)
|
2009-12-08 |
2011-06-09 |
Vaibhav Nadkarni |
Fuel injection in secondary fuel nozzle
|
|
US8381532B2
(en)
|
2010-01-27 |
2013-02-26 |
General Electric Company |
Bled diffuser fed secondary combustion system for gas turbines
|
|
RU2529987C2
(ru)
*
|
2010-03-25 |
2014-10-10 |
Дженерал Электрик Компани |
Камера сгорания и способ эксплуатации камеры сгорания
|
|
US8752386B2
(en)
*
|
2010-05-25 |
2014-06-17 |
Siemens Energy, Inc. |
Air/fuel supply system for use in a gas turbine engine
|
|
US8769955B2
(en)
|
2010-06-02 |
2014-07-08 |
Siemens Energy, Inc. |
Self-regulating fuel staging port for turbine combustor
|
|
US8919125B2
(en)
|
2011-07-06 |
2014-12-30 |
General Electric Company |
Apparatus and systems relating to fuel injectors and fuel passages in gas turbine engines
|
|
US9170024B2
(en)
|
2012-01-06 |
2015-10-27 |
General Electric Company |
System and method for supplying a working fluid to a combustor
|