157481 ⎘
Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration; Air inlet arrangements; Arrangement of apertures along the flame tube between annular flame tube sections, e.g. flame tubes with telescopic sections
COMBUSTOR FOR A GAS TURBINE ENGINE
#2Combustor with a variable primary zone combustion chamber
#3Combustion liner
#4Combustion liner
#5Combustor assembly with moveable interface dilution opening
#6Combustor for a gas turbine engine
#7Combustor for a gas turbine engine
#8Combustor and gas turbine
#9Multi-walled structure for a gas turbine engine
#10Combustor heat shield and method of cooling same
#11Combustor and gas turbine including the same
#12Heatshield for a gas turbine engine
#13Annular free-vortex combustor
#14Dual fuel lance with cooling microchannels
#15Igniter seal arrangement for a combustion chamber
#16Liner of a gas turbine engine combustor including dilution holes with airflow features
#17Apparatus and method for mitigating particulate accumulation on a component of a gas turbine
#18Apparatus and method for mitigating particulate accumulation on a component of a gas turbine
#19Heat shield panels with overlap joints for a turbine engine combustor
#20Gas turbine combustor
#21Combustor device for a gas turbine engine and gas turbine engine incorporating said combustor device
#22Cross fire tube with guide ring and angled cooling holes
#23Combustion chamber
#24Combustor and gas turbine
#25Bundled tube fuel nozzle with internal cooling
#26Combustor shape cooling system
#27Combustion duct assembly for gas turbine
#28Combustor wall with tapered cooling cavity
#29Heat shield panels with overlap joints for a turbine engine combustor
#30Sealing device for a gas turbine combustor
#31Gas turbine engines with plug resistant effusion cooling holes
#32Gas turbine system with a transition duct having axially extending cooling channels
#33LOW POROSITY AUXETIC SHEET
#34Combustor liners with U-shaped cooling channels
#35Wake reducing structure for a turbine system
#36Annular combustor with scoop ring for gas turbine engine
#37HEAT-SHIELD ELEMENT FOR A COMPRESSOR-AIR BYPASS AROUND THE COMBUSTION CHAMBER
#38ANNULAR-COMBUSTION-CHAMBER BYPASS
#39Air regulation for film cooling and emission control of combustion gas structure
#40Combustor liner cooling assembly
#41Combustor and method for supplying flow to a combustor
#42Temperature mixing enhancement with locally co-swirling quench jet pattern for gas turbine engine combustor
#43Coated gas turbine components
#44Flow sleeve impingement cooling baffles
#45Fuel gas cooling system for combustion basket spring clip seal support
#46Fuel nozzle assembly for use as structural support for a duct structure in a combustor of a gas turbine engine
#47Combustion chamber arrangement for operating a gas turbine
#48Combustor liner cooling flow disseminator and related method
#49Flow sleeve impingement cooling baffles
#50Combustor wall apparatus with parts joined by mechanical fasteners
#51Methods and systems to facilitate reducing combustor pressure drops
#52Method and apparatus for assembling gas turbine engine combustors
#53Pulsed combustion engine
#54Arrangement for the cooling of thermally highly loaded components
#55Thick coated combustor liner
#56Method for repairing an air cooled combustor liner segment edge portion and repaired segment
#57Method of operating a combustor with a variable combustion chamber
#58Cross-fire tube for gas turbine with axially spaced purge air hole pairs