139153 ⎘
Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
Sub-classes:AIRCRAFT PROPULSION SYSTEM
#2SERIAL ROTATING DETONATION COMBUSTOR SYSTEMS
#3ANTONI CYCLE INTERMITTENT COMBUSTION ENGINE
#4Turbulence generator mixer for rotating detonation engine
#5Forced-induction device
#6Forced-induction device
#7Turbocharger system for a two-stroke engine
#8System and method for ram air intake for pulse combustors
#9Aircraft power plant with supercritical COheat engine
#10Regenerative cooling and adjustable throat for rotating detonation engine
#11Turbulence generator mixer for rotating detonation engine
#12ADJUSTABLE EXHAUST NOZZLE FOR DETONATION ENGINES
#13Aircraft power plant with supercritical COheat engine
#14Turbocharger system for a two-stroke engine
#15Wastegate assembly and turbocharger including the same
#16Multi-mode combustion control for a rotating detonation combustion system
#17Auto-driven plasma actuator for transition from deflagration to detonation combustion regime and method
#18Pulse drive
#19Turbofan engine assembly with intercooler
#20Turbocharger system for a two-stroke engine
#21Effervescent atomizing structure and method of operation for rotating detonation propulsion system
#22Supercharger
#23Engine assembly with combined engine and cooling exhaust
#24Intermittent injection system for a gas turbine combustor
#25Turboprop engine assembly with combined engine and cooling exhaust
#26AUXILIARY POWER UNIT WITH COMBINED COOLING OF GENERATOR
#27Supercharged internal combustion engine
#28Effervescent atomizing structure and method of operation for rotating detonation propulsion system
#29Turbocharger, engine system, and control method for turbocharger
#30ROTATING DETONATION ENGINE WAVE INDUCED MIXER
#31ROTATING DETONATION ENGINE COMBUSTOR WAVE REFLECTOR
#32Turbofan engine assembly with intercooler
#33TURBINE ENGINE ASSEMBLY AND METHOD OF OPERATING
#34Combustor for rotating detonation engine and method of operating same
#35Turbine
#36Engine assembly with exhaust pipe nozzle
#37Modified energy-saving one-dimensional internal combustion engine
#38Engine assembly with combined engine and cooling exhaust
#39Positive displacement rotary motion device including a pulse detonation device
#40Auxiliary power unit with combined cooling of generator
#41Turboprop engine assembly with combined engine and cooling exhaust
#42Compound engine assembly with exhaust pipe nozzle
#43COMPOSITE MATERIAL INLET PLENUM AND GAS TURBINE ENGINE SYSTEM COMPRISING SAID PLENUM
#44Compound cycle engine
#45Shroud for rotary engine
#46Compound cycle engine
#47Spiral pulse detonation tube configuration
#48Pulse detonation engine having a scroll ejector attenuator
#49Indexed positive displacement rotary motion device
#50Compound cycle engine
#51Shockwave rotor detonation (omni-engine, ubiquitous X engine) multipurpose engine
#52External Combustion Engine with a General Wheel Power Rotation Motor
#53METHOD OF OPTIMIZING THE SPECIFIC FUEL CONSUMPTION OF A TWIN ENGINE HELICOPTER AND TWIN ENGINE ARCHITECTURE WITH CONTROL SYSTEM FOR IMPLEMENTING IT
#54Fan-less Thrust Generating Component for Air-bypass Engine
#55Variable initiation location system for pulse detonation combustor
#56Pulse Detonation Turbine Engine Using Turbine Shaft Speed for Monitoring Combustor Tube Operation
#57Catalytic Converter for a Pulse Detonation Turbine Engine
#58Optimal Feedback Heat Energy Internal Combustion Engine And Its Applications
#59Engine using hydrogen as a fuel
#60Shroud for rotary engine
#61THRUST MODULATION IN A MULTIPLE COMBUSTOR PULSE DETONATION ENGINE USING CROSS-COMBUSTOR DETONATION INITIATION
#62PULSE DETONATION COMBUSTOR
#63Gas turbine engine
#64Indexed positive displacement rotary motion device
#65Ground based pulse detonation combustor for power generation
#66Aircraft combination engines exhaust thrust recovery
#67System and method for passive valving for pulse detonation combustors
#68DETONATION COMBUSTOR TO TURBINE TRANSITION PIECE FOR HYBRID ENGINE
#69Multiple tube pulse detonation engine turbine apparatus and system
#70Pulse detonation combustor with folded flow path
#71Geometric configuration and confinement for deflagration to detonation transition enhancement
#72Swirling flows and swirler to enhance pulse detonation engine operation
#73Method for converting low-grade energy and a fuelless jet engine for its implementation
#74Pulse detonation assembly with cooling enhancements
#75Mixing-enhancement inserts for pulse detonation chambers
#76Pulse detonation assembly and hybrid engine
#77Gas turbine engine having improved core system
#78High thrust gas turbine engine with improved core system
#79Multiple detonation initiator for frequency multiplied pulsed detonation combustion
#80Off-axis pulse detonation configuration for gas turbine engine
#81Method and apparatus for improved flame stabilization
#82Method of operating a pulsejet
#83Hybrid fuel cell-pulse detonation power system
#84Pulsejet ejector thrust augmentor
#85Mixing elements for rotating detonation combustion systems
#86Rotating detonation augmentors with adjustable throats for gas turbine engines
#87Steam powered engine