US4174608A
(en)
*
|
1972-08-15 |
1979-11-20 |
Stal-Laval Turbin Ab |
Combustion chamber for a gas turbine
|
US3981142A
(en)
*
|
1974-04-01 |
1976-09-21 |
General Motors Corporation |
Ceramic combustion liner
|
US4073137A
(en)
*
|
1976-06-02 |
1978-02-14 |
United Technologies Corporation |
Convectively cooled flameholder for premixed burner
|
US4118925A
(en)
*
|
1977-02-24 |
1978-10-10 |
Carmel Energy, Inc. |
Combustion chamber and thermal vapor stream producing apparatus and method
|
DE2845588A1
(de)
*
|
1978-10-19 |
1980-04-24 |
Motoren Turbinen Union |
Brennkammer fuer gasturbinentriebwerke
|
US4380896A
(en)
*
|
1980-09-22 |
1983-04-26 |
The United States Of America As Represented By The Secretary Of The Army |
Annular combustor having ceramic liner
|
EP0061494B1
(en)
*
|
1980-10-07 |
1988-01-20 |
Foster-Miller Associates, Inc. |
Thermal enhancement
|
US4459101A
(en)
*
|
1981-08-28 |
1984-07-10 |
Foster-Miller Associates, Inc. |
Burner systems
|
US4422300A
(en)
*
|
1981-12-14 |
1983-12-27 |
United Technologies Corporation |
Prestressed combustor liner for gas turbine engine
|
US4787208A
(en)
*
|
1982-03-08 |
1988-11-29 |
Westinghouse Electric Corp. |
Low-nox, rich-lean combustor
|
US4485630A
(en)
*
|
1982-12-08 |
1984-12-04 |
General Electric Company |
Combustor liner
|
DE3328485A1
(de)
*
|
1983-08-06 |
1985-02-14 |
Motan Gmbh, 7972 Isny |
Schwingbrenner
|
US4655044A
(en)
*
|
1983-12-21 |
1987-04-07 |
United Technologies Corporation |
Coated high temperature combustor liner
|
JPS60149828A
(ja)
*
|
1984-01-13 |
1985-08-07 |
Hitachi Ltd |
燃焼器
|
USH140H
(en)
|
1985-04-18 |
1986-10-07 |
The United States Of America As Represented By The Secretary Of The Air Force |
Carbon/carbon combustor external insulation
|
JPS63243630A
(ja)
*
|
1987-03-30 |
1988-10-11 |
Tokyo Electric Power Co Inc:The |
ガスタ−ビン燃焼器
|
US4838030A
(en)
*
|
1987-08-06 |
1989-06-13 |
Avco Corporation |
Combustion chamber liner having failure activated cooling and dectection system
|
US4838031A
(en)
*
|
1987-08-06 |
1989-06-13 |
Avco Corporation |
Internally cooled combustion chamber liner
|
US5639531A
(en)
*
|
1987-12-21 |
1997-06-17 |
United Technologies Corporation |
Process for making a hybrid ceramic article
|
US5553455A
(en)
*
|
1987-12-21 |
1996-09-10 |
United Technologies Corporation |
Hybrid ceramic article
|
AT394768B
(de)
*
|
1990-11-02 |
1992-06-25 |
Chamottewaren U Thonoefenfabri |
Brennerflammenfuehrungsteil
|
US5184455A
(en)
*
|
1991-07-09 |
1993-02-09 |
The United States Of America As Represented By The Secretary Of The Air Force |
Ceramic blanket augmentor liner
|
US5687572A
(en)
*
|
1992-11-02 |
1997-11-18 |
Alliedsignal Inc. |
Thin wall combustor with backside impingement cooling
|
US5291733A
(en)
*
|
1993-02-08 |
1994-03-08 |
General Electric Company |
Liner mounting assembly
|
DE4343319A1
(de)
*
|
1993-12-18 |
1995-06-22 |
Abb Patent Gmbh |
Brennkammer mit keramischer Auskleidung
|
US5636508A
(en)
*
|
1994-10-07 |
1997-06-10 |
Solar Turbines Incorporated |
Wedge edge ceramic combustor tile
|
GB2298267B
(en)
*
|
1995-02-23 |
1999-01-13 |
Rolls Royce Plc |
An arrangement of heat resistant tiles for a gas turbine engine combustor
|
US5749229A
(en)
*
|
1995-10-13 |
1998-05-12 |
General Electric Company |
Thermal spreading combustor liner
|
DE19623300A1
(de)
*
|
1996-06-11 |
1997-12-18 |
Siemens Ag |
Hitzeschildanordnung, insbesondere für Strukturteile von Gasturbinenanlagen, mit geschichtetem Aufbau
|
US6014855A
(en)
*
|
1997-04-30 |
2000-01-18 |
Stewart & Stevenson Services, Inc. |
Light hydrocarbon fuel cooling system for gas turbine
|
US6101814A
(en)
*
|
1999-04-15 |
2000-08-15 |
United Technologies Corporation |
Low emissions can combustor with dilution hole arrangement for a turbine engine
|
US6495207B1
(en)
|
2001-12-21 |
2002-12-17 |
Pratt & Whitney Canada Corp. |
Method of manufacturing a composite wall
|
EP1441180A1
(de)
*
|
2003-01-27 |
2004-07-28 |
Siemens Aktiengesellschaft |
Hitzeschildelement, Brennkammer sowie Gasturbine
|
US6920836B2
(en)
*
|
2003-10-02 |
2005-07-26 |
The Boeing Company |
Regeneratively cooled synthesis gas generator
|
EP1528343A1
(de)
*
|
2003-10-27 |
2005-05-04 |
Siemens Aktiengesellschaft |
Keramischer Hitzeschildstein mit eingebetteten Verstärkungselementen zur Auskleidung einer Gasturbinenbrennkammerwand
|
CZ15297U1
(cs)
*
|
2005-02-24 |
2005-04-04 |
Dis-R S. R. O. |
Ústí spalovacího hořáku
|
US7740671B2
(en)
*
|
2006-12-18 |
2010-06-22 |
Pratt & Whitney Rocketdyne, Inc. |
Dump cooled gasifier
|
US7731783B2
(en)
*
|
2007-01-24 |
2010-06-08 |
Pratt & Whitney Rocketdyne, Inc. |
Continuous pressure letdown system
|
US8771604B2
(en)
*
|
2007-02-06 |
2014-07-08 |
Aerojet Rocketdyne Of De, Inc. |
Gasifier liner
|
US7972572B2
(en)
*
|
2008-03-04 |
2011-07-05 |
Pratt & Whitney Rocketdyne, Inc. |
Reactor vessel and liner
|
US8673234B2
(en)
*
|
2008-03-04 |
2014-03-18 |
Aerojet Rocketdyne Of De, Inc. |
Reactor vessel and liner
|
GB0913580D0
(en)
*
|
2009-08-05 |
2009-09-16 |
Rolls Royce Plc |
Combustor tile
|
US9341118B2
(en)
*
|
2009-12-29 |
2016-05-17 |
Rolls-Royce Corporation |
Various layered gas turbine engine component constructions
|
DE102012015449A1
(de)
*
|
2012-08-03 |
2014-02-20 |
Rolls-Royce Deutschland Ltd & Co Kg |
Gasturbinenbrennkammer mit Mischluftöffnungen und Luftleitelementen in modularer Bauweise
|
EP2769969B1
(en)
|
2013-02-25 |
2018-10-17 |
Ansaldo Energia IP UK Limited |
Method for manufacturing a metal-ceramic composite structure and metal-ceramic composite structure
|
US9651258B2
(en)
|
2013-03-15 |
2017-05-16 |
Rolls-Royce Corporation |
Shell and tiled liner arrangement for a combustor
|
GB2540769A
(en)
*
|
2015-07-27 |
2017-02-01 |
Rolls Royce Plc |
Combustor for a gas turbine engine
|