Patents
Patents for F02K 7 - 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 (1,599)
04/1998
04/09/1998WO1998014367A2 Method for the operation of a supersonic jet-engine combined power unit
04/09/1998DE19640191A1 Nach dem Verfahren der pulsierenden Verbrennung arbeitende Kraftmaschine In the process of pulsating combustion engine working
03/1998
03/25/1998EP0830500A1 Improved method and apparatus for power generation
03/17/1998US5727382 Aircraft ram jet engine for supersonic and/or hypersonic flight
03/03/1998US5722234 Aircraft ram jet engine for supersonic and/or hypersonic flight
01/1998
01/20/1998US5709076 Method and apparatus for power generation using rotating ramjet which compresses inlet air and expands exhaust gas against stationary peripheral wall
01/07/1998EP0816665A1 Fuel injector for a ramjet working at high Mach number
01/07/1998EP0816664A1 Fuel injector for a ramjet working at high Mach number
12/1997
12/24/1997CA2207837A1 Fuel injection bar for ramjet engine operating at high mach number
12/09/1997US5694768 Variable cycle turbofan-ramjet engine
10/1997
10/14/1997US5676522 Supersonic distributor for the inlet stage of a turbomachine
10/08/1997EP0799982A2 Internal compression supersonic engine inlet
10/07/1997US5673550 Laser initiated non-linear fuel droplet ignition
09/1997
09/30/1997US5672184 Repeated injection and ignition of gaseous fuel mixture to create a detonation wave which discharges a high pressure, high temperature exhaust pulse, at selected frequency, into the coal bed to improve movement and conversion
09/25/1997DE19611448A1 Rotary hydrogen-oxygen type rocket engine arrangement e.g. for automobile engineering
09/11/1997DE3890359C2 Piloting fuel injector assembly
09/09/1997US5665272 Multifuel combustion engine and use in generating obscurant smoke
09/03/1997EP0793011A1 Ramjet with variable geometry
09/03/1997EP0793010A1 Fuel injector for a ramjet
09/03/1997EP0680557B1 Turbojet engine with a fan or propfan
08/1997
08/26/1997US5660040 Scramjet fuel injection system having independent fuel supplies for supersonic and hypersonic operation
07/1997
07/17/1997WO1997025527A1 Method of accelerating a supersonic ramjet engine
07/17/1997DE19600824A1 Turbine shaft load drive mechanism for hypersonic region
07/08/1997US5645127 Coolant supply arrangement for jet engine turbine walls
06/1997
06/10/1997US5636509 Flywheel engine improvements
04/1997
04/03/1997DE19536181A1 Jet engine for hypersonic aircraft
04/02/1997EP0714477B1 Control of position of supersonic inlet shock
04/01/1997US5615548 Dual rotor pulse detonation apparatus
02/1997
02/04/1997US5598699 Laser initiated non-linear fuel droplet ignition apparatus
01/1997
01/15/1997EP0753655A1 Cooled fuel injection strut for ramjet
01/15/1997EP0753654A1 Ramjet for supersonic and/or hypersonic vehicle
01/15/1997EP0753653A1 Ramjet for supersonic and/or hypersonic vehicle
01/15/1997EP0662193A4 Method and apparatus for power generation.
12/1996
12/31/1996US5589632 Method and device for estimating the thrust of a ramjet
12/19/1996WO1996041073A1 Improved method and apparatus for power generation
12/18/1996EP0748432A1 Flameholder
12/03/1996US5579633 Annular pulse detonation apparatus and method
11/1996
11/21/1996WO1996036804A1 Thermodynamic drive
11/14/1996DE19618740A1 Rocket drive using liquid fuels
10/1996
10/29/1996US5568724 Turbofan engine with means to smooth intake air
10/09/1996EP0735991A1 Process for operating a reaction-type missile propulsion system and missile propulsion system
09/1996
09/24/1996US5557926 Pulse detonation apparatus with inner and outer Spherical valves
08/1996
08/27/1996US5548952 Hydrogen jet-phase engine
08/20/1996US5546745 Scramjet combustor having a two-part, aft-facing step with primary and secondary fuel injector discharge orifices
08/20/1996US5546744 Pulse detonation apparatus with spherical seals
08/13/1996US5544586 Solid fuel ramjet tubular projectile
08/06/1996US5542247 Apparatus powered using laser supplied energy
07/1996
07/23/1996US5537815 Power units of the ram-jet engine type
07/03/1996EP0719906A1 First stage supersonic stator vane for turbomachine
06/1996
06/28/1996CA2165863A1 A supersonic distributor for the inlet stage of a turbomachine
06/11/1996US5524429 Laser initiated non-linear fuel droplet ignition
06/05/1996EP0714477A1 Control of position of supersonic inlet shock
05/1996
05/30/1996DE4441730A1 Rotary combustion and steam power machine with back thrust and nozzle devices
05/07/1996US5513571 Airbreathing propulsion assisted gun-launched projectiles
05/07/1996US5513489 Rotary valve multiple combustor pulse detonation engine
05/02/1996WO1996012688A1 Process for operating a reaction-type missile propulsion system and missile propulsion system
04/1996
04/25/1996DE4437524A1 Verfahren zum Betreiben eines nach dem Rückstoßprinzip arbeitenden Antriebes eines Flugkörpers sowie Flugkörperantrieb Method for operating an operating according to the principle of repulsion drive a missile and missile propulsion
04/10/1996CN1120319A Pulse combusted acoustic agglomeration apparatus and process
03/1996
03/12/1996USRE35172 Pulsed piston-compressor jet engine
03/12/1996US5497612 Laser initiated non-linear fuel droplet ignition method
02/1996
02/27/1996US5494438 Sudden expansion combustion chamber with slotted inlet port
01/1996
01/24/1996EP0693668A2 Gas gun launched scramjet test projectile
01/23/1996US5485787 Gas gun launched scramjet test projectile
01/23/1996US5485720 Laser initiated non-linear fuel droplet ignition
01/17/1996EP0691881A1 Pulse combusted acoustic agglomeration process
01/17/1996CN1115004A Reaction type jet engine
12/1995
12/26/1995US5477672 High-temperature, high-pressure gas generation apparatus for turbine drive
12/20/1995EP0474633B1 Controlling the flow ratio in a multiflow jet engine
12/12/1995US5473885 Pulse detonation engine
11/1995
11/22/1995EP0683385A1 Procedure and device for estimating the thrust of a ramjet
11/22/1995EP0683376A1 Airbreathing propulsion assisted gun-launched projectiles
11/19/1995CA2149074A1 Process and device for the evaluation of a ramjet thrust
11/15/1995EP0681647A1 Laser initiated non-linear fuel droplet ignition
09/1995
09/08/1995WO1995023941A1 Flameholder
08/1995
08/10/1995EP0681647A4 Laser initiated non-linear fuel droplet ignition.
08/01/1995US5437151 Detecting and controlling supersonic airflow normal shock pattern position in an aircraft jet engine assembly
07/1995
07/19/1995EP0663524A1 Scram-stage missile
07/12/1995EP0662193A1 Method and apparatus for power generation
06/1995
06/13/1995US5423179 Solid fuel ramjet engine for a spin-stabilized projectile
05/1995
05/30/1995US5419118 Multi-stage rocket motors
05/30/1995US5419117 Turbo jet/RAM jet propulsion system
05/23/1995US5417057 Thermodynamic drive
04/1995
04/27/1995DE4339415C1 Method for the generation of thrust in jet engines
04/12/1995CN1101398A Jet rotor engine
04/11/1995US5404712 Laser initiated non-linear fuel droplet ignition
03/1995
03/07/1995US5394685 Method and apparatus to enhance combustion rates and extend extinction limits in high speed propulsion units
03/02/1995WO1995006198A1 Control of position of supersonic inlet shock
03/02/1995CA2169726A1 Control of position of supersonic inlet shock
02/1995
02/28/1995US5392614 Gas turbine engine cooling system
01/1995
01/17/1995US5381655 Apparatus for mixing bypass air and exhaust gas within a jet engine
12/1994
12/20/1994US5373698 Inert gas turbine engine
12/13/1994US5372005 Method and apparatus for power generation
11/1994
11/08/1994US5361581 Pulsed piston-compressor jet engine
10/1994
10/27/1994WO1994024427A1 Improved rotary valve multiple combustor pulse detonation engine
10/13/1994WO1994022559A1 Pulse combusted acoustic agglomeration apparatus and process
10/11/1994US5353721 Pulse combusted acoustic agglomeration apparatus and process
10/11/1994US5353588 Rotary valve multiple combustor pulse detonation engine
10/04/1994US5351480 Jet engine
09/1994
09/27/1994US5349815 Scramjet combustor having a two-part, aft-facing step
09/20/1994US5347807 Combined jet engine with RAM jet and turbojet
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