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)
07/2004
07/07/2004EP1435449A1 Pulsed combustion device with distributed ignition
07/07/2004EP1435448A1 Pulsed combustion turbine engine
07/07/2004EP1435447A1 Pulsed combustion turbine engine
07/07/2004EP1435440A1 Pulsed combustion engine
07/06/2004US6758032 System of pulsed detonation injection for fluid flow control of inlets, nozzles, and lift fans
07/01/2004US20040123583 Combustion ignition
07/01/2004US20040123582 Pulsed combustion engine
06/2004
06/30/2004EP1433946A1 Combined cycle pulse detonation turbine engine
06/24/2004US20040118972 Pulsejet augmentor powered vtol aircraft
06/24/2004US20040118104 Methods and apparatus for generating gas turbine engine thrust
06/23/2004EP1431563A1 Methods and apparatus for generating gas turbine engine thrust
06/22/2004US6751943 Method of magnetohydrodynamic flow control for pulse detonation engines
06/17/2004US20040112060 Methods and apparatus for operating gas turbine engines
06/16/2004EP1429016A1 Methods and apparatus for operating gas turbine engines
06/09/2004CN2620100Y Combined fanjet
05/2004
05/20/2004US20040096375 Device for producing a plasma, ionisation method, use of said method and production processes using said device
05/20/2004US20040094341 Hybrid electric vehicle using micro-thrust engines
04/2004
04/28/2004CN1492137A Method for combustable gas to burn under water to produce power and ship engine
04/27/2004US6725664 Shut-off system for an orifice of a duct, particularly for an orifice of an air inlet passage that allows air into the combustion chamber of a ramjet
04/14/2004EP1407130A1 Jet engine using exhaust gas
04/08/2004WO2004029432A2 Gas turbine power plant with supersonic gas compressor
04/08/2004US20040065087 Variable geometry inlet design for scram jet engine
04/07/2004EP1045971B1 Heat exchanger in composite material and method for making same
04/06/2004US6715293 Scram jet engine design
04/01/2004WO2003074858A3 Ramjet engine combustion chamber and ramjet engine equipped with same
03/2004
03/18/2004US20040050062 Shut-off system for an orifice of a duct, particularly for an orifice of an air inlet passage that allows air into the combustion chamber of a ramjet
03/18/2004US20040050061 Compact swirl augmented afterburners for gas turbine engines
03/03/2004EP1163152A4 Payload carry and launch system
02/2004
02/26/2004WO2003081013A3 System and method of pulsed detonation injection for fluid flow control of inlets, nozzles, and lift fans
02/26/2004DE20315339U1 Circular piston aided magnetic centrifugal motor, e.g. for motor vehicle, has rigid camshaft with cam(s), rotors that move around camshaft and end as shaped centrifugal masses with explosion chambers
02/24/2004US6694743 Rotary ramjet engine with flameholder extending to running clearance at engine casing interior wall
02/19/2004DE10255356A1 Reliable ramjet drive ignition device regulation has valve chamber between gas generator, combustion chamber, valve control elements in drive chamber connected to cold end of gas generator chamber
02/19/2004DE10235645A1 Device for reliable ramjet ignition and control has regulating valve, variable valve opening, ignition/safety devices in valve chamber tested and controlled/regulated by elements in drive chamber
02/12/2004US20040026572 Dual-mode airbreathing propulsion system
02/05/2004US20040020211 Trapped vortex combustor
02/05/2004US20040020187 Blanking-plug system for blanking off an orifice of a pipe, particularly for blanking off an orifice of a duct for introducing air into the combustion chamber of a ramjet
02/05/2004US20040020185 Rotary ramjet engine
02/04/2004CN1472433A Jet supercharged thrust regulatable impulse detonation engine and method for increasing its thrust
01/2004
01/29/2004US20040016853 Method and apparatus for modulating flow separation
01/29/2004US20040016235 Rotary ramjet engine with flameholder extending to running clearance at engine casing interior wall
01/29/2004US20040016226 Radial impulse turbine for rotary ramjet engine
01/28/2004EP1384897A2 Method and apparatus for modulating flow separation
01/28/2004EP1384896A2 Method and apparatus for modulating airfoil lift
01/22/2004WO2004007928A1 Method for energy transformation in jet-engines
01/22/2004US20040011045 Ramjet for a supersonic and hypersonic aircraft
01/21/2004CN1470152A Device for producing a plasma, ionisation method, use of said method and production processes using said device
01/15/2004WO2004005684A1 Rotary impeller driven turbine
01/15/2004US20040006965 Turbo shaft engine with acoustical compression flow amplifying ramjet
01/08/2004US20040005214 Pressurized gas turbine engine with electrothermodynamic enhancement
01/07/2004CN2597682Y Boosting impacting fanjet
01/06/2004US6672068 Ramjet for a supersonic and hypersonic aircraft
01/06/2004US6672048 Rotary impeller driven turbine
01/02/2004EP1375865A2 Method and apparatus for generating torque
01/02/2004EP1375864A2 Method and apparatus for lifting and propelling rotorcraft
01/01/2004US20040000614 Method and apparatus for lifting and propelling rotorcraft
01/01/2004US20040000145 Method and apparatus for generating torque
01/01/2004US20040000134 Pulse detonation engine having an aerodynamic valve
12/2003
12/30/2003US6668542 Pulse detonation bypass engine propulsion pod
12/27/2003CA2432850A1 Method and apparatus for lifting and propelling rotorcraft
12/27/2003CA2432819A1 Method and apparatus for generating torque
12/23/2003US6666018 Combined cycle pulse detonation turbine engine
12/16/2003US6662550 Method and apparatus for improving the efficiency of pulsed detonation engines
12/10/2003CN1460791A Reaction rotor engine
12/10/2003CN1460790A Adaptive control method of pulse engine frequency and its device
12/09/2003US6658838 Shaped charge engine
12/03/2003EP1367251A1 Closure system for an orifice of an air-intake duct of a combustion chamber of a ramjet, as well as ramjet and missile comprising said system
11/2003
11/20/2003WO2003095890A1 Method for using the potential energy of compressed gas during vortex flow energy separation and device for carrying out said method
11/18/2003US6647709 Turbo shaft engine with acoustical compression flow amplifying ramjet
11/13/2003US20030209006 Pulsed jet augmentation
11/04/2003US6640549 Method and device for modulation of a flame
10/2003
10/30/2003WO2003089773A1 Stationary detonation combustor, and stationary detonation wave generating method
10/30/2003US20030200753 Method and apparatus for improving the efficiency of pulsed detonation engines
10/28/2003US6637187 Rotary inlet flow controller for pulse detonation combustion engines
10/16/2003CA2382382A1 Continuous rotary motor powered by shockwave induced combustion
10/14/2003US6631610 Consumable port cover for ducted integral rocket-ramjet engine
10/08/2003EP1350943A2 Shock wave reflector and detonation chamber
10/08/2003CN1123687C Ejector ramjet engine
10/07/2003US6629674 Method and apparatus for modulating airfoil lift
10/02/2003WO2003081013A2 System and method of pulsed detonation injection for fluid flow control of inlets, nozzles, and lift fans
10/02/2003US20030182928 Scram jet engine design
10/02/2003US20030182927 Shock wave reflector and detonation chamber
09/2003
09/25/2003US20030177756 Apparatus and method for positron fueled ramjet operation
09/12/2003WO2003074858A2 Ramjet engine combustion chamber and ramjet engine equipped with same
09/12/2003WO2003016849A3 Method and apparatus for testing engines
09/10/2003EP1342904A1 Combustion chamber for a ram-jet and ram-jet with such a combustion chamber
09/10/2003EP1264100A4 Shaped charge engine
09/04/2003WO2003072924A1 Jet propulsion system
09/03/2003EP1340071A1 A method for chromatographic finger printing and standardization of single medicines and formulations
09/03/2003CN1120113C Payload carry and launch system
08/2003
08/28/2003WO2003071117A1 Ejector based engines
08/21/2003WO2003023203A3 Rotary ejector enhanced pulsed detonation system and method
08/21/2003US20030154720 Ejector based engines
08/21/2003US20030154707 Rotary inlet flow controller for pulse detonation combustion engines
08/07/2003WO2003064841A1 Pulse detonation engine and method for initiating detonations
08/07/2003US20030145577 System and method of pulsed detonation injection for fluid flow control of inlets, nozzles, and lift fans
07/2003
07/24/2003US20030136108 Method of magnetohydrodynamic flow control for pulse detonation engines
07/17/2003US20030131584 Combined cycle pulse detonation turbine engine
07/10/2003US20030126853 Methods and apparatus for operating gas turbine engines
07/02/2003CN1113164C Heat exchanger in composite material and method for making same
07/01/2003US6584774 High frequency pulsed fuel injector
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