140403 ⎘
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 with external combustion, e.g. scram-jet engines
ADVANCED RAM SCOOP CONCEPTS FOR ROTATING DETONATION ENABLED HIGH-SPEED PROPULSION SYSTEMS
#2THERMAL MANAGEMENT FOR RAMJET-RDRE CONFIGURATION OF RBCC
#3SYSTEMS AND METHODS FOR PRODUCING TRAVELING WAVES ALONG SURFACES EXPOSED TO SUPERSONIC FLUID FLOWS
#4ENGINE FOR AN AIRCRAFT
#5LAUNCH SYSTEM AND METHOD
#6Electrically powered supersonic and hypersonic propulsor
#7Systems and methods for producing traveling waves along surfaces exposed to supersonic fluid flows
#8Combined cycle propulsion system for hypersonic flight
#9ENGINE FOR AN AIRCRAFT
#10Motor and fuel-powered hybrid system for a rocket thruster
#11ATTENUATORS FOR COMBUSTION NOISE IN DUAL MODE RAMJETS AND SCRAMJETS
#12HELICON YIELD PLASMA ELECTROMAGNETIC RAM-SCRAMJET DRIVE ROCKET ION VECTOR ENGINE
#13Fuel injector for hypersonic jet engine operation
#14Scramjet engine and flying object
#15Hybrid propulsion cooling system
#16Anti-unstart for combined cycle high mach vehicles
#17HIGH SPEED PROPULSION SYSTEM WITH INLET COOLING
#18Engine for an aircraft
#19Scramjet engine
#20HYPERSONIC VEHICLE USING SCRAMJET
#21Use of infrared transparent airframe materials for passive cooling of internal components
#22Scramjets and associated aircraft and methods
#23Catalytic N2O Pilot Ignition System for Upper Stage Scramjets
#24Engine for hypersonic aircrafts with supersonic combustor
#25Centripetal aerodynamic platform spacecraft
#26Jet engine, flying object, and method of operating a jet engine
#27CATALYTIC N2O PILOT IGNITION SYSTEM FOR UPPER STAGE SCRAMJETS
#28COMBINED CYCLE PROPULSION SYSTEM
#29Laser-charged high-speed propulsion system and method for production of high-powered laser
#30Energy-deposition systems, equipment and methods for modifying and controlling shock waves and supersonic flow
#31High speed propulsion system with inlet cooling
#32Process for operating a dual-mode combustor
#33Combined cycle integrated combustor and nozzle system
#34Fuel supply system, scramjet engine and method for operating the same
#35SELF-STARTING SUPERSONIC INLET
#36Turbine based combined cycle engine
#37Combined cycle integrated combustor and nozzle system
#38Energy-deposition systems, equipment and method for modifying and controlling shock waves and supersonic flow
#39TURBOJET ENGINE FOR AIRCRAFT
#40Fuel-cooled flexible heat exchanger with thermoelectric device compression
#41Continously air breathing assisted jet engine linear aerospkie rocket
#42Combined cycle integrated combustor and nozzle system
#43Single-stage hypersonic vehicle featuring advanced swirl combustion
#44Two-stage hypersonic vehicle featuring advanced swirl combustion
#45Annular isolator dual mode scramjet engine
#46Multipurpose gas generator ramjet/scramjet cold start system
#47SCRAMjet arrangement for hypersonic aircraft
#48Semi-axisymmetric scramjet flowpath with conformal nozzle
#49Integrated air inlet system for multi-propulsion aircraft engines
#50Sensing of isolator shock systems
#51Detachable strut structure in combustion chamber of scramjet-oblique detonation engine
#52Passive bypass for mitigation of inlet buzz in supersonic or hypersonic air-breathing engines
#53Airbreathing propulsion engines including rotating detonation and bluff body systems
#54Scramjet isolator
#55Scramjet isolator
#56Decahydronaphthalene as an endothermic fuel for hypersonic vehicles
#57Active control of scramjet isolator shock systems