140400 ⎘
Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
Sub-classes:Flowpath Assembly with Composite Tube Array
#2RAM AIR TURBINE FIXED WITHIN AIRCRAFT
#3ACOUSTIC SANDWICH PANEL WITH IMPROVED MOUNTING
#4SHAPEABLE INLET MANIFOLD FOR HYPERSONIC SCRAMJET
#5Single stage to orbit rocket engine
#6INLETS FOR HYPERSONIC AIR-BREATHING VEHICLES AND DESIGN METHODS AND SYSTEMS THEREFOR
#7Dual-mode ramjet engine with variable fuel injection
#8ENGINE FOR AN AIRCRAFT
#9RAMJET PROPULSION METHOD
#10ENGINE WITH ROTATING DETONATION COMBUSTION SYSTEM
#11CHECK VALVE FOR RAT RESTOW PUMP
#12High Speed Aircraft Propelled by Thorium or Uranium Fueled Molten Salt Reactor
#13Hypersonic large internal contraction ratio air inlet channel having stepless adjustable air release valve and control method
#14Electrically powered supersonic and hypersonic propulsor
#15AIRCRAFT WITH THERMAL ENERGY STORAGE SYSTEM
#16HYPERSONIC VEHICLE AND SCRAMJET ENGINE WITH VARIABLE FUEL INJECTION FOR OPERATION OVER A LARGE MACH NUMBER RANGE
#17Effector inlet cover, and method of separation
#18Inlets for hypersonic air-breathing vehicles and design methods and systems therefor
#19Actuator release mechanism
#20STOWABLE ELECTRIC-HYBRID PROPFAN
#21Mixed-compression inlet duct for turbine engines facilitating supersonic flight
#22100% AMBIENT AIR ENVIRONMENTAL CONTROL SYSTEM
#23Cooling system for aircraft components including ram chute body and relatively rotatable air conduit
#24AIRCRAFT WITH RAM AIR TURBINE DISK WITH GENERATOR HAVING BLADE TIP INTEGRATED MAGNETS
#25APPARATUS AND METHOD FOR FLUID MANIPULATION
#26Electricity generation system and methods of making and using the same
#27Effector having morphing airframe and method
#28Engine with rotating detonation combustion system
#29Engine with rotating detonation combustion system
#30Mixed-compression inlet duct for turbine engines facilitating supersonic flight
#31Engine with rotating detonation combustion system
#32VARIABLE CYCLE JET ENGINE
#33RAMJET PROPULSION METHOD
#34ENGINE FOR AN AIRCRAFT
#35Motor and fuel-powered hybrid system for a rocket thruster
#36APPARATUS AND METHOD FOR FLUID MANIPULATION
#37Engine with rotating detonation combustion system
#38PROPULSION CONCEPT COMBINING CONVENTIONAL ROCKET ENGINES AND AIR-BREATHING ENGINES (HEBER CONCEPT)
#39METHOD AND APPARATUS FOR FILTRATION
#40Aircraft engines with a fuel cell
#41Aircraft with thermal energy storage system for multiple heat loads
#42Airframe integrated scramjet with fixed geometry and shape transition for hypersonic operation over a large Mach number range
#43FILTRATION APPARATUS AND METHOD
#44Jet engine
#45Hydraulic control valves for ram air turbine stow actuators
#46Method of reducing low energy flow in an isolator of a flight vehicle air breathing engine
#47Fuel injector for hypersonic jet engine operation
#48Cooling system for an engine assembly
#49Regeneration cooler of ramjet engine, and manufacturing method of the same
#50Mixed-compression inlet duct for turbine engines facilitating supersonic flight
#51Rectification structure body and flying vehicle
#52Ramjet engine with rotating detonation combustion system and method for operation
#53Ramjet propulsion method
#54Rotating Detonation Combustion System
#55Engine for an aircraft
#56Shapeable inlet manifold for hypersonic scramjet
#57Engine with rotating detonation combustion system
#58Engine with rotating detonation combustion system
#59Engine With Rotating Detonation Combustion System
#60Engine with rotating detonation combustion system
#61Filtration apparatus and method
#62Fuel reformation for use in high speed propulsion systems
#63Use of infrared transparent airframe materials for passive cooling of internal components
#64Flight vehicle with air inlet isolator having wedge on inner mold line
#65Multi-can annular rotating detonation combustor
#66Jet engine, flying object, and operation method of jet engine
#67JET ENGINE AND FLYING OBJECT
#68Multiple chamber rotating detonation combustor
#69Hybrid combustor assembly and method of operation
#70Flight vehicle air breathing propulsion system with isolator having obstruction
#71Flight vehicle air breathing engine with isolator having bulged section
#72Unmanned aerial vehicle with deployable transmit/receive module apparatus with ramjet
#73Flight vehicle engine with finned inlet
#74MAGNETIC GAS ENGINE AND METHOD OF EXTRACTING WORK
#75Propulsion system using large scale vortex generators for flow redistribution and supersonic aircraft equipped with the propulsion system
#76Unmanned aerial vehicle with deployable transmit/receive module apparatus with ramjet
#77COOLING OF AEROSPACE FLIGHT SYSTEMS
#78Mobile multi-mode power generation system with mode based adjustable drag configuration
#79Combustor and jet engine having the same
#80Combustor, jet engine, flying body, and operation method of jet engine
#81Jet engine, flying object, and method of operating a jet engine
#82Inlet flow restrictor
#83Jet engine, flying object, and method of operating jet engine
#84Hyperjet superconducting turbine blisk propulsion and power generation
#85Isentropic compression inlet for supersonic aircraft
#86Actuator housing for ram air turbine deployment actuator
#87Air inlet arrangement and method of making the same
#88Magnetic Gas Engine and Method of Extracting Work
#89RAM AIR FAN OUTER HOUSING
#90Engine for propelling an aircraft and aircraft having at least one engine and at least one hydrogen tank
#91Process for operating a dual-mode combustor
#92Combined cycle integrated combustor and nozzle system
#93Combustion systems and combustion system components for rotary ramjet engines
#94Propulsion system using large scale vortex generators for flow redistribution and supersonic aircraft equipped with the propulsion system
#95Ramjet including a detonation chamber and aircraft comprising such a ramjet
#96Integrated thermal protection and leakage reduction in a supersonic air intake system
#97Ramjet superheater
#98Isentropic compression inlet for supersonic aircraft
#99Ram air fan outer housing
#100Supersonic aircraft jet engine installation
#101Air inlet arrangement and method of making the same
#102HIGHLY INTEGRATED INSIDE-OUT RAMJET
#103Compression ramp boundary layer removal
#104Isentropic compression inlet for supersonic aircraft
#105Turbine based combined cycle engine
#106Integrated aero-engine flowpath structure
#107Isentropic compression inlet for supersonic aircraft
#108Hydrogen gas generator for jet engines
#109Methods and apparatus for missile air inlet
#110Rayleigh-Taylor assisted combustion and combustors adapted to exploit Rayleigh-Taylor instability for increasing combustion rates therein
#111Self-starting turbineless jet engine
#112Combined cycle integrated combustor and nozzle system
#113Subsonic and Stationary Ramjet Engines
#114Fuel-cooled heat exchanger with thermoelectric device compression
#115Relating to air-breathing flight vehicles
#116Vortex combustor for low NOX emissions when burning lean premixed high hydrogen content fuel
#117Magnetic gas engine and method of extracting work
#118Hypersonic inlet systems and methods
#119Mechanical acoustic noise generator system for scramjet engine
#120Stationary mechanical engines and subsonic jet engines using supersonic gas turbines
#121Combined cycle missile engine system
#122Pumping Ejector
#123Ramjet superheater
#124Statically-operating ejector ramjet
#125Hypermixing Fluid Ejector
#126Seal for pulse detonation engine
#127Vortex combustor for low NOx emissions when burning lean premixed high hydrogen content fuel
#128Continously air breathing assisted jet engine linear aerospkie rocket
#129Combined cycle integrated combustor and nozzle system
#130Isentropic compression inlet for supersonic aircraft
#131Valve control unit for ramjet propulsion system as well as guided missile having such a valve control unit
#132Strut cavity pilot and fuel injector assembly
#133Annular isolator dual mode scramjet engine
#134Core burning for scramjet engines
#135Multi-height ramp injector scramjet combustor
#136Methods and apparatus for missile air inlet
#137Multipurpose gas generator ramjet/scramjet cold start system
#138Advanced hypersonic magnetic jet/electric turbine engine (AHMJET)
#139Hyperjet
#140Plasma torch for ignition, flameholding and enhancement of combustion in high speed flows
#141Ram air turbine centrifugal brake
#142Magnetic gas engine and method of extracting work
#143Self powdered missile turbojet
#144Cooling scheme for scramjet variable geometry hardware
#145Integrated air inlet system for multi-propulsion aircraft engines
#146Cooling scheme for scramjet variable geometry hardware
#147Jet aircraft electrical energy production system
#148Sensing of isolator shock systems
#149Passive bypass for mitigation of inlet buzz in supersonic or hypersonic air-breathing engines
#150Power plant cycle using renewable energy facilitated by a supersonic shock wave compressor apparatus
#151Airbreathing propulsion engines including rotating detonation and bluff body systems
#152Laser powered, air breathing, open-cycle heat engines
#153Tridyne ignition and pressurization system for hypersonic vehicles
#154Solid-fuel ramjet ammunition
#155Thermodynamic louvered jet engine
#156Supersonic elliptical ramp inlet