139160 ⎘
Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the combustion chambers having inlet or outlet valves, e.g. Holzwarth gas-turbine plants
ROTATING INTERNAL COMBUSTION ENGINE
#2Gas Turbine System
#3METHOD OF CONTROLLING DEFLAGRATION COMBUSTION PROCESS IN PISTONLESS COMBUSTOR
#4Turbine driven by confrontation of explosions of oxygen and hydrogen, or any hydrogenated hydrocarbon, under pressure and vacuum by aqueous precipitation of the resulting water vapor
#5Constant-volume combustion system with synchronized injection
#6Pulse detonation combustion system
#7Constant volume turbomachine combustion chamber
#8Method of controlling deflagration combustion process in pistonless combustor
#9COMBUSTION ENGINE INCLUDING TURBOMACHINE
#10Constant-volume combustion system comprising a rotating closure element with segmented apertures
#11ROTARY INTERNAL COMBUSTION ENGINE
#12System and method for generating power
#13ROTATING INTERNAL COMBUSTION ENGINE
#14CVC combustion module for aircraft turbomachine comprising sub-assemblies of independent chambers
#15Constant volume combustion chamber with counter rotating shutter valve
#16ENGINE
#17JET ENGINE WITH CONTINUOUS AND DISCONTINUOUS IMPULSE
#18Constant volume combustion system
#19SYSTEM AND METHOD FOR GENERATING ELECTRIC ENERGY
#20Constant-volume combustion (CVC) chamber for an aircraft turbine engine including an intake/exhaust valve having a spherical plug
#21Systems and methods for improving operation of pulse combustors
#22Active clearance control for gas turbine engine
#23METHODS OF OPERATING A ROTATING DETONATION COMBUSTOR AT APPROXIMATELY CONSTANT DETONATION CELL SIZE
#24Multiple chamber rotating detonation combustor
#25System and method for generating power
#26Rotating detonation engine upstream wave arrestor
#27Constant-volume combustion module for a turbine engine
#28Internal combustion engine control device
#29Compressor having elliptically-shaped combustion chambers with fuel injection and ignition occurring at the foci
#30SYSTEM AND METHOD FOR GENERATING ELECTRIC ENERGY
#31CONSTANT-VOLUME COMBUSTION SYSTEM FOR A TURBINE ENGINE OF AN AIRCRAFT ENGINE
#32Constant-volume combustion module for a turbine engine, comprising communication-based ignition
#33System and method for generating electric energy
#34Multi-cycle stratified internal combustion system
#35Systems and methods for generating power using a combustion source
#36Rotating pulse detonation engine, power generation system including the same, and methods of making and using the same
#37Systems and methods for improving operation of pulse combustors
#38System and method for generating electric energy
#39Internal detonation engine, hybrid engines including the same, and methods of making and using the same
#40Active clearance control for gas turbine engine
#41System and method for generating electric energy
#42Constant-volume combustion (CVC) chamber for an aircraft turbine engine including an intake/exhaust valve having a spherical plug
#43Method and thermal reactor for single-valve propulsion with multiple injections and combustions per rotation cycle
#44Continuous detonation combustion engine and system
#45SYSTEM AND METHOD FOR CONTROLLING FUEL DISTRIBUTIONS IN A COMBUSTOR IN A GAS TURBINE ENGINE
#46Internal detonation engine, hybrid engines including the same, and methods of making and using the same
#47Multi-cycle stratified internal combustion system
#48Helical cross flow (HCF) pulse detonation engine
#49M Thermodynamic resonant engine with a rotary variant
#50Pulsed detonation engine
#51SYSTEM AND METHOD FOR DAMPING PRESSURE OSCILLATIONS WITHIN A PULSE DETONATION ENGINE
#52Jet engine, in particular a jet engine for an aircraft
#53Combustion turbine in which combustion is intermittent
#54PULSE DETONATION SYSTEM WITH FUEL LEAN INLET REGION
#55PULSE DETONATION INLET MANAGEMENT SYSTEM
#56Helical cross flow (HCF) pulse detonation engine
#57System and method for power production using a hybrid helical detonation device
#58MULTI-TUBE, CAN-ANNULAR PULSE DETONATION COMBUSTOR BASED ENGINE WITH TANGENTIALLY AND LONGITUDINALLY ANGLED PULSE DETONATION COMBUSTORS
#59SYSTEM AND METHOD FOR POWER PRODUCTION USING A HYBRID HELICAL DETONATION DEVICE
#60Pulse combustion device
#61Pulse combustion device
#62Thermodynamic pressure generator
#63Methods and apparatus for generating gas turbine engine thrust using a pulse detonator
#64Transverse disc motor
#65Rotating pulse detonation system for a gas turbine engine
#66Pistonless, rotary internal combustion engine and associated support systems