157511 ⎘
Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers Cyclone or vortex type combustion chambers
COMBUSTOR HAVING A PLURALITY OF OPENINGS TO CONTROL A VORTEX DRIVER JET FOR A GAS TURBINE ENGINE
#2METHOD OF CONTROLLING DEFLAGRATION COMBUSTION PROCESS IN PISTONLESS COMBUSTOR
#3INJECTOR WITH INJECTOR ELEMENTS IN CIRCUMFERENTIAL ROWS THAT ALTERNATE BETWEEN COUNTER-CLOCKWISE AND CLOCKWISE SWIRL
#4VORTEX STATION
#5TRAPPED VORTEX COMBUSTOR AND METHOD FOR OPERATING THE SAME
#6BURNER WITH A BILAMINAR COUNTERDIRECTIONAL VORTEX FLOW
#7Vortex station
#8Adaptive trapped vortex combustor
#9Method of controlling deflagration combustion process in pistonless combustor
#10Trapped vortex combustor for a gas turbine engine with a driver airflow channel
#11Injector with injector elements in circumferential rows that alternate between counter-clockwise and clockwise swirl
#12Trapped vortex combustor and method for operating the same
#13Volute trapped vortex combustor assembly
#14Single cavity trapped vortex combustor with CMC inner and outer liners
#15TRAPPED VORTEX COMBUSTOR
#16Vortex station
#17Jet swirl air blast fuel injector for gas turbine engine
#18Production of activated carbon
#19Involute trapped vortex combustor assembly
#20Volute trapped vortex combustor assembly
#21Tangential bulk swirl air in a trapped vortex combustor for a gas turbine engine
#22Aerospace turbofan engines
#23Trapped vortex combustor and method for operating the same
#24Hybrid combustor assembly and method of operation
#25Single cavity trapped vortex combustor with CMC inner and outer liners
#26Trapped vortex combustor for a gas turbine engine with a driver airflow channel
#27Gas turbine engine combustor comprising air inlet tubes arranged around the combustor
#28Combustor for use in a turbine engine
#29TURBINE ENGINE ASSEMBLY INCLUDING A ROTATING DETONATION COMBUSTOR
#30Gas turbine combustor
#31SHOCK COMPRESSION BASED SUPERSONIC COMBUSTOR
#32Fuel injector
#33High G-field Combustion
#34Cooling apparatus for a fuel injector
#35Annular turbomachine combustion chamber
#36Apparatus and method for air extraction at a gas turbine engine combustor
#37Thrust increasing device
#38Trapped vortex cavity staging in a combustor
#39Cooling flow for leading panel in a gas turbine engine combustor
#40Swept combustor liner panels for gas turbine engine combustor
#41Liner retaining feature for a combustor
#42Combustor arrangement with fastening system for combustor parts
#43Apparatus and methods for treating and/or utilizing a gaseous medium
#44Combustor liners with U-shaped cooling channels
#45COMBUSTION SYSTEM FOR A GAS TURBINE ENGINE
#46System, method and apparatus for lean combustion with plasma from an electrical arc
#47Fuel air premix chamber for a gas turbine engine
#48Combustion chamber
#49Lean azimuthal flame combustor
#50System, method and apparatus for lean combustion with plasma from an electrical arc
#51Mid-section of a can-annular gas turbine engine with a cooling system for the transition
#52COMBUSTOR
#53Gas turbine combustion chamber arrangement of axial type of construction
#54System, method and apparatus for lean combustion with plasma from an electrical arc
#55Tangential Combustor
#56Triple helical flow vortex reactor improvements
#57Gas turbine combustor
#58System, method and apparatus for lean combustion with plasma from an electrical arc
#59Apparatus and method for a gas turbine entrainment system
#60Turbomachine combustion chamber with helical air flow
#61Triple helical flow vortex reactor
#62Low emission combustion and method of operation
#63Gas turbine engine combustor can with trapped vortex cavity
#64Turbine engine having a reverse flow annular vortex combustor
#65Swirler ferrule plate having pressure drop purge passages
#66Tangential annular combustor with premixed fuel and air for use on gas turbine engines
#67Tangential and flameless annular combustor for use on gas turbine engines