139205 ⎘
Features, components parts, details or accessories, not provided for in, or of interest apart form groups - ; Air intakes for jet-propulsion plants; Fuel supply systems; Fuel delivery systems comprising two or more pumps comprising an air supply system for the atomisation of fuel
OXYFUEL TURBINE SYSTEM AND METHOD FOR OXIDANT CONTROL
#2HIGH SHEAR FUEL DISTRIBUTOR
#3Thermal resistant air cap
#4Thermal resistant air caps
#5GAS TURBINE ENGINE COMBUSTOR WITH TAILORED TEMPERATURE PROFILE
#6Fuel nozzle, fuel supply assembly thereof, and method of assembling a fuel nozzle
#7Airblast injector for a gas turbine engine
#8Compressor geometry control
#9Multi-cycle stratified internal combustion system
#10Electric motor assisted airblast injector
#11Additive manufactured fuel nozzle core for a gas turbine engine
#12Swirler for a turbine engine combustor
#13Swirler mount interface for gas turbine engine combustor
#14Gas turbine engine systems and methods involving enhanced fuel dispersion
#15Combustion casing manifold for high pressure air delivery to a fuel nozzle pilot system
#16Dual flow air injection intraturbine engine and method of operating same
#17Gas turbine engine combustor with tailored temperature profile
#18Multi-cycle stratified internal combustion system
#19System having multi-tube fuel nozzle with floating arrangement of mixing tubes
#20Atomizing air heat exchange for heating attemperation feed water in a combined cycle turbine
#21Radial vane inner air swirlers
#22SYSTEM FOR CONDITIONING AIR FLOW INTO A MULTI-NOZZLE ASSEMBLY
#23Systems and method for cooling a staged airblast fuel injector
#24Purge system, system including a purge system, and purge method
#25COMBINED CYCLE POWER AUGMENTATION BY EFFICIENT UTILIZATION OF ATOMIZING AIR ENERGY
#26Combined cycle power augmentation by efficient utilization of atomizing air energy
#27Fuel nozzle swirler assembly
#28Fuel injector arrangement having porous premixing chamber
#29Gas turbine engine systems and methods involving enhanced fuel dispersion
#30Managing leaks in a gas turbine system