|
US3174530A
(en)
*
|
1961-09-19 |
1965-03-23 |
Cyril F Meenan |
Furnace combustion chamber
|
|
US3359724A
(en)
*
|
1965-08-03 |
1967-12-26 |
Bristol Siddeley Engines Ltd |
Cooling means in combustors for gas turbine engines
|
|
GB1059199A
(en)
*
|
1965-10-20 |
1967-02-15 |
Rolls Royce |
Flame tube
|
|
FR1500110A
(en)
*
|
1966-07-08 |
1967-11-03 |
Snecma |
Improvements to turbo-reactors
|
|
US3463601A
(en)
*
|
1967-10-20 |
1969-08-26 |
Gen Dynamics Corp |
Torch assembly
|
|
US3481543A
(en)
*
|
1967-12-18 |
1969-12-02 |
Thiokol Chemical Corp |
Rocket thrust nozzle
|
|
GB1283827A
(en)
*
|
1970-09-26 |
1972-08-02 |
Rolls Royce |
Improvements in or relating to combustion apparatus
|
|
US3652181A
(en)
*
|
1970-11-23 |
1972-03-28 |
Carl F Wilhelm Jr |
Cooling sleeve for gas turbine combustor transition member
|
|
US3938323A
(en)
*
|
1971-12-15 |
1976-02-17 |
Phillips Petroleum Company |
Gas turbine combustor with controlled fuel mixing
|
|
US3955361A
(en)
*
|
1971-12-15 |
1976-05-11 |
Phillips Petroleum Company |
Gas turbine combustor with controlled fuel mixing
|
|
US3844116A
(en)
*
|
1972-09-06 |
1974-10-29 |
Avco Corp |
Duct wall and reverse flow combustor incorporating same
|
|
CA980584A
(en)
*
|
1972-11-10 |
1975-12-30 |
Edward E. Ekstedt |
Double walled impingement cooled combustor
|
|
US3845620A
(en)
*
|
1973-02-12 |
1974-11-05 |
Gen Electric |
Cooling film promoter for combustion chambers
|
|
US3939653A
(en)
*
|
1974-03-29 |
1976-02-24 |
Phillips Petroleum Company |
Gas turbine combustors and method of operation
|
|
US4012902A
(en)
*
|
1974-03-29 |
1977-03-22 |
Phillips Petroleum Company |
Method of operating a gas turbine combustor having an independent airstream to remove heat from the primary combustion zone
|
|
US4109459A
(en)
*
|
1974-07-19 |
1978-08-29 |
General Electric Company |
Double walled impingement cooled combustor
|
|
US3990835A
(en)
*
|
1974-07-26 |
1976-11-09 |
Occidental Petroleum Corporation |
Burner for igniting oil shale retort
|
|
FR2340453A1
(en)
*
|
1976-02-06 |
1977-09-02 |
Snecma |
COMBUSTION CHAMBER BODY, ESPECIALLY FOR TURBOREACTORS
|
|
CH633347A5
(en)
*
|
1978-08-03 |
1982-11-30 |
Bbc Brown Boveri & Cie |
GAS TURBINE.
|
|
US4292810A
(en)
*
|
1979-02-01 |
1981-10-06 |
Westinghouse Electric Corp. |
Gas turbine combustion chamber
|
|
GB2078363B
(en)
*
|
1980-06-17 |
1984-03-07 |
Bs & B Eng Co |
Fuel reactor
|
|
JPS5929766B2
(en)
*
|
1981-05-15 |
1984-07-23 |
明雄 田中 |
Combustion method and equipment
|
|
US4504211A
(en)
*
|
1982-08-02 |
1985-03-12 |
Phillips Petroleum Company |
Combination of fuels
|
|
US4606721A
(en)
*
|
1984-11-07 |
1986-08-19 |
Tifa Limited |
Combustion chamber noise suppressor
|
|
US4696431A
(en)
*
|
1985-11-29 |
1987-09-29 |
United Technologies Corporation |
Augmentor liner support band having finger positioners
|
|
US5394688A
(en)
*
|
1993-10-27 |
1995-03-07 |
Westinghouse Electric Corporation |
Gas turbine combustor swirl vane arrangement
|
|
US6018950A
(en)
*
|
1997-06-13 |
2000-02-01 |
Siemens Westinghouse Power Corporation |
Combustion turbine modular cooling panel
|
|
US6568187B1
(en)
*
|
2001-12-10 |
2003-05-27 |
Power Systems Mfg, Llc |
Effusion cooled transition duct
|
|
US7373772B2
(en)
*
|
2004-03-17 |
2008-05-20 |
General Electric Company |
Turbine combustor transition piece having dilution holes
|
|
DE102006011727B3
(en)
*
|
2006-03-14 |
2007-11-22 |
Webasto Ag |
Combined heating / hot water system for mobile applications
|
|
US20100018211A1
(en)
*
|
2008-07-23 |
2010-01-28 |
General Electric Company |
Gas turbine transition piece having dilution holes
|
|
US20080264035A1
(en)
*
|
2007-04-25 |
2008-10-30 |
Ricciardo Mark J |
Coolant flow swirler for a rocket engine
|
|
AU2009216835B2
(en)
*
|
2008-02-20 |
2013-12-05 |
General Electric Technology Gmbh |
Thermal machine
|
|
US8549861B2
(en)
*
|
2009-01-07 |
2013-10-08 |
General Electric Company |
Method and apparatus to enhance transition duct cooling in a gas turbine engine
|
|
US8931280B2
(en)
*
|
2011-04-26 |
2015-01-13 |
General Electric Company |
Fully impingement cooled venturi with inbuilt resonator for reduced dynamics and better heat transfer capabilities
|
|
US8925326B2
(en)
|
2011-05-24 |
2015-01-06 |
General Electric Company |
System and method for turbine combustor mounting assembly
|
|
US8397514B2
(en)
*
|
2011-05-24 |
2013-03-19 |
General Electric Company |
System and method for flow control in gas turbine engine
|
|
US8919127B2
(en)
|
2011-05-24 |
2014-12-30 |
General Electric Company |
System and method for flow control in gas turbine engine
|
|
US8966910B2
(en)
*
|
2011-06-21 |
2015-03-03 |
General Electric Company |
Methods and systems for cooling a transition nozzle
|
|
US9228747B2
(en)
*
|
2013-03-12 |
2016-01-05 |
Pratt & Whitney Canada Corp. |
Combustor for gas turbine engine
|
|
US20170167729A1
(en)
*
|
2014-07-30 |
2017-06-15 |
Siemens Aktiengesellschaft |
Multiple feed platefins within a hot gas path cooling system in a combustor basket in a combustion turbine engine
|
|
EP3048370A1
(en)
*
|
2015-01-23 |
2016-07-27 |
Siemens Aktiengesellschaft |
Combustion chamber for a gas turbine engine
|