US4012904A
(en)
*
|
1975-07-17 |
1977-03-22 |
Chrysler Corporation |
Gas turbine burner
|
GB1578474A
(en)
*
|
1976-06-21 |
1980-11-05 |
Gen Electric |
Combustor mounting arrangement
|
US4180974A
(en)
*
|
1977-10-31 |
1980-01-01 |
General Electric Company |
Combustor dome sleeve
|
IT1111808B
(it)
*
|
1978-03-28 |
1986-01-13 |
Rolls Royce |
Perfezionamenti apportati ai dispositivi di combustione di motori a turbina a gas
|
GB2044431B
(en)
*
|
1979-03-20 |
1983-03-16 |
Rolls Royce |
Gas turbine
|
GB2055187B
(en)
*
|
1979-08-01 |
1983-12-14 |
Rolls Royce |
Gaseous fuel injector for a gas turbine engine
|
FR2465080A1
(fr)
*
|
1979-09-17 |
1981-03-20 |
Snecma |
Dispositif de suspension aval de chambre de combustion pour turbomachines
|
GB2109532B
(en)
*
|
1981-11-07 |
1985-01-03 |
Rolls Royce |
Gas fuel injector
|
US4606190A
(en)
*
|
1982-07-22 |
1986-08-19 |
United Technologies Corporation |
Variable area inlet guide vanes
|
US4532762A
(en)
*
|
1982-07-22 |
1985-08-06 |
The Garrett Corporation |
Gas turbine engine variable geometry combustor apparatus
|
US4497170A
(en)
*
|
1982-07-22 |
1985-02-05 |
The Garrett Corporation |
Actuation system for a variable geometry combustor
|
DE3241162A1
(de)
*
|
1982-11-08 |
1984-05-10 |
Kraftwerk Union AG, 4330 Mülheim |
Vormischbrenner mit integriertem diffusionsbrenner
|
US4984429A
(en)
*
|
1986-11-25 |
1991-01-15 |
General Electric Company |
Impingement cooled liner for dry low NOx venturi combustor
|
US5117636A
(en)
*
|
1990-02-05 |
1992-06-02 |
General Electric Company |
Low nox emission in gas turbine system
|
US5207064A
(en)
*
|
1990-11-21 |
1993-05-04 |
General Electric Company |
Staged, mixed combustor assembly having low emissions
|
US5257499A
(en)
*
|
1991-09-23 |
1993-11-02 |
General Electric Company |
Air staged premixed dry low NOx combustor with venturi modulated flow split
|
US5572862A
(en)
*
|
1993-07-07 |
1996-11-12 |
Mowill Rolf Jan |
Convectively cooled, single stage, fully premixed fuel/air combustor for gas turbine engine modules
|
US5628182A
(en)
*
|
1993-07-07 |
1997-05-13 |
Mowill; R. Jan |
Star combustor with dilution ports in can portions
|
US5377483A
(en)
*
|
1993-07-07 |
1995-01-03 |
Mowill; R. Jan |
Process for single stage premixed constant fuel/air ratio combustion
|
US5638674A
(en)
*
|
1993-07-07 |
1997-06-17 |
Mowill; R. Jan |
Convectively cooled, single stage, fully premixed controllable fuel/air combustor with tangential admission
|
US5613357A
(en)
*
|
1993-07-07 |
1997-03-25 |
Mowill; R. Jan |
Star-shaped single stage low emission combustor system
|
US6220034B1
(en)
|
1993-07-07 |
2001-04-24 |
R. Jan Mowill |
Convectively cooled, single stage, fully premixed controllable fuel/air combustor
|
DE4408136A1
(de)
*
|
1994-03-10 |
1995-09-14 |
Bmw Rolls Royce Gmbh |
Verfahren und Vorrichtung zur Kraftstoff-Aufbereitung für eine Gasturbinen-Brennkammer
|
EP0678708B1
(en)
*
|
1994-04-20 |
1998-12-02 |
ROLLS-ROYCE plc |
Gas turbine engine fuel injector
|
DE19507088B4
(de)
*
|
1995-03-01 |
2005-01-27 |
Alstom |
Vormischbrenner
|
DE19512645A1
(de)
*
|
1995-04-05 |
1996-10-10 |
Bmw Rolls Royce Gmbh |
Vorrichtung zur Kraftstoffaufbereitung für eine Brennkammer
|
DE19516798A1
(de)
*
|
1995-05-08 |
1996-11-14 |
Abb Management Ag |
Vormischbrenner mit axialer oder radialer Luftzuströmung
|
DE19527453B4
(de)
*
|
1995-07-27 |
2009-05-07 |
Alstom |
Vormischbrenner
|
GB2307980B
(en)
*
|
1995-12-06 |
2000-07-05 |
Europ Gas Turbines Ltd |
A fuel injector arrangement; a method of operating a fuel injector arrangement
|
DE19547913A1
(de)
*
|
1995-12-21 |
1997-06-26 |
Abb Research Ltd |
Brenner für einen Wärmeerzeuger
|
DE19547912A1
(de)
*
|
1995-12-21 |
1997-06-26 |
Abb Research Ltd |
Brenner für einen Wärmeerzeuger
|
US5924276A
(en)
*
|
1996-07-17 |
1999-07-20 |
Mowill; R. Jan |
Premixer with dilution air bypass valve assembly
|
JP3706443B2
(ja)
*
|
1996-09-24 |
2005-10-12 |
三菱重工業株式会社 |
アニュラ型ガスタービン燃焼器
|
DE19649486A1
(de)
*
|
1996-11-29 |
1998-06-04 |
Abb Research Ltd |
Brennkammer
|
GB2332509B
(en)
|
1997-12-19 |
2002-06-19 |
Europ Gas Turbines Ltd |
Fuel/air mixing arrangement for combustion apparatus
|
US6272842B1
(en)
*
|
1999-02-16 |
2001-08-14 |
General Electric Company |
Combustor tuning
|
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
|
US6286300B1
(en)
|
2000-01-27 |
2001-09-11 |
Honeywell International Inc. |
Combustor with fuel preparation chambers
|
US6508061B2
(en)
*
|
2001-04-25 |
2003-01-21 |
Pratt & Whitney Canada Corp |
Diffuser combustor
|
US8590313B2
(en)
*
|
2008-07-30 |
2013-11-26 |
Rolls-Royce Corporation |
Precision counter-swirl combustor
|
US8281597B2
(en)
*
|
2008-12-31 |
2012-10-09 |
General Electric Company |
Cooled flameholder swirl cup
|
EP2781838B1
(en)
*
|
2011-11-16 |
2019-04-24 |
Mitsubishi Hitachi Power Systems, Ltd. |
Gas turbine combustor
|
US20160010866A1
(en)
*
|
2013-02-19 |
2016-01-14 |
United Technologies Corporation |
Aerating fuel injector system for a gas turbine engine
|
US9228747B2
(en)
*
|
2013-03-12 |
2016-01-05 |
Pratt & Whitney Canada Corp. |
Combustor for gas turbine engine
|
EP2789915A1
(en)
*
|
2013-04-10 |
2014-10-15 |
Alstom Technology Ltd |
Method for operating a combustion chamber and combustion chamber
|
EP3011231B1
(en)
*
|
2013-06-18 |
2019-10-30 |
Woodward, Inc. |
Gas turbine combustor assembly
|
US9482433B2
(en)
|
2013-11-11 |
2016-11-01 |
Woodward, Inc. |
Multi-swirler fuel/air mixer with centralized fuel injection
|
US9587833B2
(en)
|
2014-01-29 |
2017-03-07 |
Woodward, Inc. |
Combustor with staged, axially offset combustion
|
US20150338101A1
(en)
*
|
2014-05-21 |
2015-11-26 |
General Electric Company |
Turbomachine combustor including a combustor sleeve baffle
|
DE102017120370B4
(de)
*
|
2017-09-05 |
2019-06-06 |
Deutsches Zentrum für Luft- und Raumfahrt e.V. |
Brennerkopf, Brennersystem und Verfahren zum Betreiben des Brennersystems
|
GB202019222D0
(en)
|
2020-12-07 |
2021-01-20 |
Rolls Royce Plc |
Lean burn combustor
|
GB202019219D0
(en)
*
|
2020-12-07 |
2021-01-20 |
Rolls Royce Plc |
Lean burn combustor
|