140404 ⎘
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 Composite ram-jet/turbo-jet engines
PROPULSION SYSTEM USING RAMJET BLEED AIR FOR GAS TURBINE COMBUSTION
#2RAMJET PROPULSION METHOD
#3ENGINE WITH ROTATING DETONATION COMBUSTION SYSTEM
#4Duplex Turbine Guide Vane Assembly
#5Ammonia based hydrogen powered combined propulsion system
#6PROPULSION SYSTEM USING RAMJET BLEED AIR FOR GAS TURBINE COMBUSTION
#7Electrically powered supersonic and hypersonic propulsor
#8Duplex Turbine Guide Vane Assembly
#9TURBORAMJET ENGINE
#10Combined cycle propulsion system for hypersonic flight
#11Ram-air duct system
#12ENGINE COMPRISING A DEVICE FOR INDUCING NUCLEAR FUSION REACTIONS BY ACCELERATED IONS
#13Jet engine for aircraft
#14Engine with rotating detonation combustion system
#15Multi-mode combined cycle propulsion engine
#16ION JET ENGINE SYSTEM AND ASSOCIATED METHOD(S)
#17Air direction arrangement for an aircraft with integrated heat exchanger
#18HELICON YIELD PLASMA ELECTROMAGNETIC RAM-SCRAMJET DRIVE ROCKET ION VECTOR ENGINE
#19Supersonic turbofan engine
#20Turbine engine structure with oxidizer enhanced mode
#21High Speed Aircraft Flight Technologies
#22Turbo engine with cooler for cooling inlet air and turbine for expanding cryogenic fuel
#23HYPERSONIC SUPERCONDUCTING COMBUSTION RAM ACCELERATED MAGNETOHYDRODYNAMIC-DRIVE
#24Hybrid propulsion cooling system
#25Anti-unstart for combined cycle high mach vehicles
#26COMBINED CYCLE FLIGHT PROPULSION SYSTEMS
#27Ramjet propulsion method
#28Nozzle wall for an air-breathing engine of a vehicle and method therefor
#29Ram-jet and turbo-jet detonation engine
#30HYDROGEN-FUELED SUPERSONIC TURBORAMJET ENGINE
#31Engine with rotating detonation combustion system
#32MULTI-STAGE, LIQUID HYDROGEN-BASED AEROSPACE SYSTEM
#33High-mach vehicle cooling
#34Fuel reformation for use in high speed propulsion systems
#35Centripetal aerodynamic platform spacecraft
#36Mobile multi-mode power generation system with mode based adjustable drag configuration
#37HELICON YIELD PLASMA ELECTROMAGNETIC RAM-SCRAMJET DRIVE ROCKET ION VECTOR ENGINE
#38Air inlet arrangement and method of making the same
#39COMBINED CYCLE PROPULSION SYSTEM
#40Airflow modulation system and method
#41Ram air turbine driveshaft gear and bearing arrangement
#42Aircraft nozzle system
#43Rotational machine, such as a turbomachine, and engines and flying machines incorporating same
#44Combined cycle integrated combustor and nozzle system
#45Combined turbojet and ramjet engine
#46Aircraft airflow modulation system and method
#47Low shock strength propulsion system
#48Air inlet arrangement and method of making the same
#49Flade discharge in 2-D exhaust nozzle
#50Turbine based combined cycle engine
#51Combined cycle integrated combustor and nozzle system
#52Airflow modulation for dual mode combined cycle propulsion systems
#53Combining a series of more efficient engines into a unit, or modular units
#54Fuel-cooled flexible heat exchanger with thermoelectric device compression
#55Relating to air-breathing flight vehicles
#56Low shock strength propulsion system
#57Low shock strength inlet
#58Combined cycle integrated combustor and nozzle system
#59Centerline compression turbine engine
#60Single-stage hypersonic vehicle featuring advanced swirl combustion
#61Two-stage hypersonic vehicle featuring advanced swirl combustion
#62Turbofan gas turbine engine with variable fan outlet guide vanes
#63Hyperjet
#64Rotary ramjet turbo-generator
#65SCRAMjet arrangement for hypersonic aircraft
#66Integrated air inlet system for multi-propulsion aircraft engines
#67Methods and apparatus for assembling a gas turbine engine
#68Methods and apparatus for assembling a gas turbine engine
#69Turbo rocket with real carnot cycle
#70Combined cycle engines incorporating swirl augmented combustion for reduced volume and weight and improved performance
#71Jet aircraft electrical energy production system
#72Inlet bleed diversion through rotating detonation rocket engine
#73Jet-propelled engine using discharged exhaust gas
#74Dual flowpath exhaust for fuel cooling in a hypersonic propulsion system
#75Pressure equalization in a dual flow path exhaust of a hypersonic propulsion system