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)
07/2003
07/01/2003US6584765 Pulse detonation engine having an aerodynamic valve
07/01/2003US6584764 Propulsion module
07/01/2003US6584761 MAPP gas fuel for flight vehicles having pulse detonation engines and method of use
06/2003
06/25/2003EP1321014A1 Device for producing a plasma, ionisation method, use of said method and production processes using said device
06/11/2003EP1009927A4 Ejector ramjet engine
06/10/2003US6575404 Air intake and flying device, particularly a missile, equipped with such an air intake
05/2003
05/06/2003US6557339 Blanking-cap system for an orifice of a conduit, in particular for an orifice of an air-intake duct into the combustion chamber of a ramjet
05/01/2003US20030079713 Rotary ejector enhanced pulsed detonation system and method
04/2003
04/22/2003US6550235 Combined cycle pulse detonation turbine engine operating method
04/16/2003EP1003989B1 Quick-acting valve
04/15/2003US6547530 Fluid pump apparatus
04/10/2003US20030068828 Novel method for chromatographic finger printing and standardization of single medicines and formulations
03/2003
03/27/2003WO2003025379A1 Shesterenko method and device for jet acceleration of gas and producing energy from a vacuum
03/25/2003US6536350 Stagnation pressure activated fuel release mechanism for hypersonic projectiles
03/20/2003WO2003023203A2 Rotary ejector enhanced pulsed detonation system and method
03/20/2003US20030051536 Method and apparatus for testing engines
03/18/2003US6533539 Pressurized gas turbine engine
03/18/2003US6532728 Reducing skin friction drag
03/13/2003US20030049119 Pressurized gas turbine engine
03/13/2003US20030046920 Shaped charge engine
03/05/2003EP1288480A1 Ramjet for supersonic and hypersonic aircraft
02/2003
02/27/2003WO2003016849A2 Method and apparatus for testing engines
02/25/2003US6523339 Variable mode jet engine—compact
02/13/2003US20030029162 Propulsion module
02/13/2003US20030029161 Mapp gas fuel for flight vehicles having pulse detonation engines and method of use
02/13/2003US20030029160 Combined cycle pulse detonation turbine engine
02/11/2003US6516605 Pulse detonation aerospike engine
02/06/2003WO2003010433A1 Radial impulse turbine for rotary ramjet engine
02/06/2003WO2003010432A1 Rotary ramjet engine with flameholder extending to running clearance at engine casing interior wall
02/06/2003WO2003010431A1 Compact rotary ramjet engine generator set
01/2003
01/28/2003US6510683 Apparatus for power generation with low drag rotor and ramjet assembly
01/16/2003US20030010013 Rotary impeller driven turbine
01/14/2003US6505462 Rotary valve for pulse detonation engines
01/09/2003US20030006614 Jet assisted hybrid wind turbine system
12/2002
12/31/2002US6499286 Method for the operation of a supersonic jet-engine combined power unit
12/17/2002US6494034 Pulsed detonation engine with backpressure
12/11/2002EP1264100A1 Shaped charge engine
12/10/2002US6492743 Jet assisted hybrid wind turbine system
11/2002
11/26/2002US6484492 Magnetohydrodynamic flow control for pulse detonation engines
11/26/2002CA2107429C Gas turbine engine cooling systems
11/14/2002WO2002090725A1 Pressurized gas turbine engine
11/14/2002US20020166318 Pulse detonation bypass engine propulsion pod
11/12/2002US6477829 Combined cycle pulse combustion/gas turbine engine
11/06/2002EP1255032A1 Air intake and flying vehicle, in particular a missile, with such air intake
10/2002
10/31/2002US20020158165 Air intake and flying device, particularly a missile, equipped with such an air intake
10/30/2002CN2519029Y Multi-stage inlet jet engine
10/29/2002US6470672 Minimally intrusive and nonintrusive supersonic injectors for LANTR and RBCC/Scramjet propulsion systems
10/17/2002WO2002081893A1 Exhaust thrust booster for a thrust generator
10/10/2002DE10117605A1 Unlocking of air inlet doors in combustion chamber of ramjets takes place through heating up of thermally or pressure sensitive spring components directly produced by combustion of starting propellant or by gas generator
10/09/2002CN2515432Y Contrarotating gear jet engine
10/09/2002CN1092289C Ramjet engine for power generation
10/09/2002CN1092288C Method for operation of supersonic jet-engine combined power unit
10/03/2002US20020139108 Exhaust thrust booster for a thrust generator
10/03/2002US20020139106 Rotary valve for pulse detonation engines
10/01/2002US6457305 Turbo shaft engine with acoustical compression flow amplifying ramjet
09/2002
09/12/2002US20020124758 Stagnation pressure activated fuel release mechanism for hypersonic projectiles
09/12/2002DE10126632A1 Combination propulsion system pref. for aircraft has thrust vector control, also useable as lifting device, located behind multistage vacuum system or ram jet engines
09/10/2002US6446428 Pulsed detonation engine with divergent inflow transition section
09/10/2002US6446427 Solid fuel regression rate control method and device
09/10/2002US6446425 Ramjet engine for power generation
09/05/2002US20020121079 Turbo shaft engine with acoustical compression flow amplifying ramjet
09/03/2002US6442930 Combined cycle pulse detonation turbine engine
08/2002
08/27/2002US6439503 Pulse detonation cluster engine
08/20/2002US6434924 Ramjet engine for power generation
08/15/2002WO2002063150A1 Rotary pulse jet engine
08/13/2002US6430919 Shaped charged engine
08/08/2002US20020104315 Turbo shaft engine with acoustical compression flow amplifying ramjet
07/2002
07/30/2002CA2255904C Improved method and apparatus for power generation
07/24/2002EP1225326A1 Conduit obturation system, in particular for ramjet air conduits
07/11/2002US20020088219 Magnetohydrodynamic flow control for pulse detonation engines
06/2002
06/27/2002US20020078679 Pulsed Detonation Engine With Divergent Inflow Transition Section
06/18/2002US6405526 Solid fuel propulsion system for a ram jet rocket
06/13/2002WO2002046739A1 A novel method for chromatographic finger printing and standardization of single medicines and formulations
06/13/2002CA2424363A1 A novel method for chromatographic finger printing and standardization of single medicines and formulations
06/04/2002US6397581 Heat exchanger in composite material and method for making same
05/2002
05/28/2002CA2089278C Gas turbine engine cooling system
05/23/2002US20020059793 Pulsed Detonation Engine With Backpressure
05/02/2002US20020050719 Co-probe power generation system
04/2002
04/09/2002US6367243 Atomic-based combined cycle propulsion system and method
03/2002
03/28/2002WO2002026004A1 Device for producing a plasma, ionisation method, use of said method and production processes using said device
03/07/2002WO2001054981A3 Propulsion module
03/07/2002DE10033653A1 Drive system for e.g. aircraft, is formed multistage with drives units such that the drive system is combined with at least one negative pressure system
03/06/2002EP1184559A1 Closure device for the entry of a duct, in particular for an air inlet duct to a ramjet combustion chamber
02/2002
02/28/2002US20020023428 Blanking-cap system for an orifice of a conduit, in particular for an orifice of an air-intake duct into the combustion chamber of a ramjet
02/27/2002CN1337912A Payload carry and Launch system
02/26/2002US6349538 Annular liquid fueled pulse detonation engine
02/19/2002US6347509 Pulsed detonation engine with ejector bypass
02/19/2002US6347507 Method and apparatus for power generation using rotating ramjets
02/14/2002US20020017096 Variable mode jet engine - compact
01/2002
01/24/2002US20020009363 Fluid pump apparatus
01/01/2002US6334299 Ramjet engine for power generation
12/2001
12/19/2001EP1163152A2 Payload carry and launch system
12/18/2001US6331099 Flexible hoses communicating with a deployable hydraulic power assembly
12/18/2001CA2016346C Fringed thermal protection device and method of manufacturing it
11/2001
11/22/2001DE10118373A1 Rotating ram jet engine for operating as a drive unit in stationary and mobile applications incorporates an engine wound as a spiral around a supporting cylinder rotating on bearings around its longitudinal axis.
10/2001
10/31/2001CN1319718A Method for generating power
10/18/2001DE10018494A1 Regulator valve for solid fuel powered engine has oppositely disposed inlet openings at closed end of gas duct facing gas generator and principal axes of which are located approximately perpendicularly to principal axis of gas duct
10/09/2001US6298653 Ramjet engine for power generation
10/04/2001EP1138922A1 Combined cycle pulse detonation turbine engine
09/2001
09/25/2001US6293091 Axisymmetrical annular plug propulsion system for integrated rocket/ramjet or rocket/scramjet
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