GB1490145A
(en)
*
|
1974-09-11 |
1977-10-26 |
Mtu Muenchen Gmbh |
Gas turbine engine
|
FR2340453A1
(fr)
*
|
1976-02-06 |
1977-09-02 |
Snecma |
Corps de chambre de combustion, notamment pour turboreacteurs
|
JPS53104019A
(en)
*
|
1977-02-23 |
1978-09-09 |
Hitachi Ltd |
Gas turbine combustor
|
US4192138A
(en)
*
|
1977-08-29 |
1980-03-11 |
Westinghouse Electric Corp. |
Gas turbine combustor air inlet
|
US4132066A
(en)
*
|
1977-09-23 |
1979-01-02 |
United Technologies Corporation |
Combustor liner for gas turbine engine
|
GB2017827B
(en)
*
|
1978-04-04 |
1983-02-02 |
Gen Electric |
Combustor liner cooling
|
JPS5827264Y2
(ja)
*
|
1978-07-07 |
1983-06-13 |
日産自動車株式会社 |
ガスタ−ビンの燃焼器ライナ
|
JPS5932862U
(ja)
*
|
1982-08-27 |
1984-02-29 |
三菱重工業株式会社 |
ガスタ−ビン燃焼器
|
GB8703101D0
(en)
*
|
1987-02-11 |
1987-03-18 |
Secr Defence |
Gas turbine engine combustion chambers
|
US4875339A
(en)
*
|
1987-11-27 |
1989-10-24 |
General Electric Company |
Combustion chamber liner insert
|
US4887432A
(en)
*
|
1988-10-07 |
1989-12-19 |
Westinghouse Electric Corp. |
Gas turbine combustion chamber with air scoops
|
US6101814A
(en)
*
|
1999-04-15 |
2000-08-15 |
United Technologies Corporation |
Low emissions can combustor with dilution hole arrangement for a turbine engine
|
US6494044B1
(en)
|
1999-11-19 |
2002-12-17 |
General Electric Company |
Aerodynamic devices for enhancing sidepanel cooling on an impingement cooled transition duct and related method
|
GB2379499B
(en)
*
|
2001-09-11 |
2004-01-28 |
Rolls Royce Plc |
Gas turbine engine combustor
|
EP1312865A1
(de)
*
|
2001-11-15 |
2003-05-21 |
Siemens Aktiengesellschaft |
Ringbrennkammer für eine Gasturbine
|
US6681577B2
(en)
*
|
2002-01-16 |
2004-01-27 |
General Electric Company |
Method and apparatus for relieving stress in a combustion case in a gas turbine engine
|
US6722134B2
(en)
|
2002-09-18 |
2004-04-20 |
General Electric Company |
Linear surface concavity enhancement
|
US6761031B2
(en)
|
2002-09-18 |
2004-07-13 |
General Electric Company |
Double wall combustor liner segment with enhanced cooling
|
US7104067B2
(en)
*
|
2002-10-24 |
2006-09-12 |
General Electric Company |
Combustor liner with inverted turbulators
|
US6681578B1
(en)
*
|
2002-11-22 |
2004-01-27 |
General Electric Company |
Combustor liner with ring turbulators and related method
|
GB2399408B
(en)
|
2003-03-14 |
2006-02-22 |
Rolls Royce Plc |
Gas turbine engine combustor
|
US6984102B2
(en)
*
|
2003-11-19 |
2006-01-10 |
General Electric Company |
Hot gas path component with mesh and turbulated cooling
|
US7186084B2
(en)
*
|
2003-11-19 |
2007-03-06 |
General Electric Company |
Hot gas path component with mesh and dimpled cooling
|
GB0601413D0
(en)
*
|
2006-01-25 |
2006-03-08 |
Rolls Royce Plc |
Wall elements for gas turbine engine combustors
|
US8281600B2
(en)
*
|
2007-01-09 |
2012-10-09 |
General Electric Company |
Thimble, sleeve, and method for cooling a combustor assembly
|
US8151570B2
(en)
*
|
2007-12-06 |
2012-04-10 |
Alstom Technology Ltd |
Transition duct cooling feed tubes
|
US8627669B2
(en)
|
2008-07-18 |
2014-01-14 |
Siemens Energy, Inc. |
Elimination of plate fins in combustion baskets by CMC insulation installed by shrink fit
|
US20100050649A1
(en)
*
|
2008-09-04 |
2010-03-04 |
Allen David B |
Combustor device and transition duct assembly
|
US8490400B2
(en)
*
|
2008-09-15 |
2013-07-23 |
Siemens Energy, Inc. |
Combustor assembly comprising a combustor device, a transition duct and a flow conditioner
|
US8161752B2
(en)
*
|
2008-11-20 |
2012-04-24 |
Honeywell International Inc. |
Combustors with inserts between dual wall liners
|
US20100223930A1
(en)
*
|
2009-03-06 |
2010-09-09 |
General Electric Company |
Injection device for a turbomachine
|
US20100269513A1
(en)
*
|
2009-04-23 |
2010-10-28 |
General Electric Company |
Thimble Fan for a Combustion System
|
US8397511B2
(en)
*
|
2009-05-19 |
2013-03-19 |
General Electric Company |
System and method for cooling a wall of a gas turbine combustor
|
US20120036859A1
(en)
*
|
2010-08-12 |
2012-02-16 |
General Electric Company |
Combustor transition piece with dilution sleeves and related method
|
US8650852B2
(en)
*
|
2011-07-05 |
2014-02-18 |
General Electric Company |
Support assembly for transition duct in turbine system
|
DE102012015452A1
(de)
*
|
2012-08-03 |
2014-04-24 |
Rolls-Royce Deutschland Ltd & Co Kg |
Gasturbinenbrennkammerwand mit Mischluftöffnungen und Luftleitelementen
|
DE102012015449A1
(de)
*
|
2012-08-03 |
2014-02-20 |
Rolls-Royce Deutschland Ltd & Co Kg |
Gasturbinenbrennkammer mit Mischluftöffnungen und Luftleitelementen in modularer Bauweise
|
US9255835B2
(en)
|
2012-08-22 |
2016-02-09 |
Siemens Energy, Inc. |
System for remote vibration detection on combustor basket and transition in gas turbines
|
US9255526B2
(en)
|
2012-08-23 |
2016-02-09 |
Siemens Energy, Inc. |
System and method for on line monitoring within a gas turbine combustor section
|
US10690006B2
(en)
*
|
2013-09-13 |
2020-06-23 |
Raytheon Technologies Corporation |
Shielding pockets for case holes
|
EP3186558B1
(en)
|
2014-08-26 |
2020-06-24 |
Siemens Energy, Inc. |
Film cooling hole arrangement for acoustic resonators in gas turbine engines
|
EP2993404B1
(en)
*
|
2014-09-08 |
2019-03-13 |
Ansaldo Energia Switzerland AG |
Dilution gas or air mixer for a combustor of a gas turbine
|
US11255543B2
(en)
*
|
2018-08-07 |
2022-02-22 |
General Electric Company |
Dilution structure for gas turbine engine combustor
|
US11085639B2
(en)
*
|
2018-12-27 |
2021-08-10 |
Rolls-Royce North American Technologies Inc. |
Gas turbine combustor liner with integral chute made by additive manufacturing process
|
GB201902693D0
(en)
*
|
2019-02-28 |
2019-04-17 |
Rolls Royce Plc |
Combustion liner and gas turbine engine comprising a combustion liner
|