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)
12/2006
12/19/2006US7150143 Hybrid fuel cell-pulse detonation power system
12/14/2006WO2006131083A1 Ejector power plant
12/14/2006US20060282242 Methods and apparatus for modeling gas turbine engines
12/05/2006US7144740 Method for chromatographic finger printing and standardization of single medicines and formulations
11/2006
11/21/2006US7137255 Compact swirl augmented afterburners for gas turbine engines
11/21/2006US7137243 Constant volume combustor
11/21/2006CA2180501C Ramjet engine for supersonic and/or hypersonic aircraft
11/16/2006US20060257242 Gas-jet driven rotary device for generating a field and a process for treating items within the field for increased performance
11/16/2006US20060254254 Mixing-enhancement inserts for pulse detonation chambers
11/08/2006EP1718857A2 Integrated air inlet system for multi-propulsion aircraft engines
11/08/2006EP1718856A1 Propulsion of vehicles or transport of a medium by means of a conical body
11/07/2006US7131260 Multiple detonation initiator for frequency multiplied pulsed detonation combustion
10/2006
10/24/2006US7124573 Rotary pulse detonation system with aerodynamic detonation passages for use in a gas turbine engine
10/19/2006US20060230764 Compact swirl augmented afterburners for gas turbine engines
10/19/2006US20060230746 Turbineless jet engine
10/12/2006US20060225405 Cooling scheme for scramjet variable geometry hardware
10/11/2006EP1710426A2 Combi-supersonic-adjusting-nozzle
10/11/2006EP1710425A1 Pulse combustion device
10/11/2006EP1710417A2 Pulse combustion device
10/10/2006US7117680 Cooling scheme for scramjet variable geometry hardware
10/05/2006DE10302041B4 Injektor-Zentrifugen-Turbinen-Triebwerk und Injektor-Zentrifugen-Luftstrahl-Triebwerk Injector centrifugal turbine engine and injector centrifugal air jet thruster
10/05/2006DE102005015585B3 Combination-supersonic-adjustment-nozzle for e.g. injector-centrifugal-turbines-engine, has nozzle stream bundling unit with small supersonic auxiliary nozzles to load initial-intake-injector to increase the intake effect of engines
09/2006
09/21/2006US20060207261 Rotary pulse detonation system with aerodynamic detonation passages for use in a gas turbine engine
09/20/2006CN1834437A I.C.jetting rotor engine
09/19/2006US7107755 Engine arrangement
09/12/2006CA2180502C Ramjet engine for supersonic and/or hypersonic aircraft
09/05/2006US7101514 Control devices for evaporative chemical mixing/reaction
09/05/2006US7100360 Pulsed combustion engine
08/2006
08/17/2006DE102005005934A1 Ramjet engine operating method, involves utilizing hydrosilicon mixture in hot combustion chamber, where mixture disintegrates into atomic hydrogen and silicon and twenty one percent of oxygen portion in air is burned stoichiometrically
08/10/2006US20060174606 High static thrust valveless pulse-jet engine with forward-facing intake duct
07/2006
07/19/2006CN1804386A Minisize propeller with electrolyzing water function
06/2006
06/28/2006EP1673520A2 Generation of mechanical or electrical energy using any thermal potential
06/20/2006US7062901 Variable geometry nozzle with flexible side wall
06/07/2006CN1784574A Trapped vortex combustor
06/06/2006US7055308 Detonation damper for pulse detonation engines
06/01/2006WO2006057577A1 Intermittent detonation combustion engine
06/01/2006US20060112674 Semi-axisymmetric scramjet flowpath with conformal nozzle
05/2006
05/30/2006US7051659 Projectile structure
05/30/2006US7051510 Method of operating a pulsejet
05/24/2006CN1257656C Device for producing a plasma, ionisation method and use
05/23/2006US7047724 Combustion ignition
05/18/2006US20060102800 Method and apparatus for modulating flow separation
05/03/2006EP1653074A2 Rocket-ramjet propelled missile
04/2006
04/27/2006WO2005106234A3 Pulse jet engines
04/05/2006EP1643114A2 Multiflow jet engine, system and method of operating the same
04/05/2006EP1643113A2 Multiflow jet engine, system and method of operating the same
04/05/2006CN2769540Y Isobaric gas combustion injection engine
04/04/2006US7021889 Gas-jet driven rotary device for generating a field and a process for treating items within the field for increased performance
03/2006
03/09/2006US20060048499 Pulsed detonation engine
03/08/2006EP1632673A1 Pulse detonation system for a gas turbine engine having multiple spools
03/08/2006EP1632647A1 Rotary combustion engine system and its applications
03/07/2006US7007455 Methods and apparatus for operating gas turbine engines
02/2006
02/28/2006US7003961 Trapped vortex combustor
02/23/2006DE3934071B3 Staustrahltriebwerk mit Rohrstruktur und durch ein solches Staustrahltriebwerk antreibbare Flugkörper Ramjet with tubular structure and by such a ramjet driven missile
02/22/2006EP1627185A2 Trapped vortex combustor
02/21/2006US7000398 Ramjet engine combustion chamber and ramjet engine equipped with same
02/14/2006US6996971 Rotary heat engine
01/2006
01/26/2006US20060016170 Methods and apparatus for generating gas turbine engine thrust
01/24/2006US6988573 Cooling system for internal combustion engine
01/10/2006US6983586 Two-stage pulse detonation system
01/03/2006US6981366 Turbineless jet engine
01/03/2006US6981365 Supersonic revolving nozzle
01/03/2006US6981364 Combine engine for single-stage spacecraft
01/03/2006US6981361 Methods for operating gas turbine engines
01/03/2006CA1341492C Tubular structure ramjet, and missile propelled by such ramjet
12/2005
12/29/2005US20050284127 Detonation engine and flying object provided therewith
12/22/2005US20050279083 Folded detonation initiator for constant volume combustion device
12/22/2005US20050279078 Multiple detonation initiator for frequency multiplied pulsed detonation combustion
12/22/2005US20050279077 Off-axis pulse detonation configuration for gas turbine engine
12/20/2005US6976654 Vertical takeoff and landing aircraft
12/14/2005CA2470137A1 The gas jet engine generator
12/01/2005DE4226666B4 Wärmetauscher für die Kühlung eines heißen Gases Heat exchanger for cooling a hot gas
11/2005
11/29/2005US6968676 Propulsion from combustion of solid propellant pellet-projectiles
11/22/2005CA2207839C Fuel injection device for ramjet engine operating at high mach number
11/15/2005US6964154 Axisymmetric, throttleable non-gimballed rocket engine
11/10/2005WO2005106234A2 Pulse jet engines
11/10/2005CA2565140A1 Pulse jet engines
11/08/2005US6962323 Apparatus comprising a rotary-acting pilot valve
11/02/2005EP1590564A1 Jet ejector and method of altering fluid flow
10/2005
10/27/2005US20050235957 Engine systems and methods
10/27/2005US20050235630 High temperature dynamic seal for scramjet variable geometry
10/27/2005US20050235629 Cooling scheme for scramjet variable geometry hardware
09/2005
09/27/2005US6948306 Apparatus and method of using supersonic combustion heater for hypersonic materials and propulsion testing
09/21/2005EP1577531A2 Gas turbine engine comprising a rotary pulse detonation system
09/18/2005CA2500522A1 Rotary pulse detonation system with aerodynamic detonation passages for use in a gas turbine engine
08/2005
08/25/2005US20050183413 Pulse detonation engine and valve
08/23/2005US6931858 Rotating pulse detonation system for a gas turbine engine
08/23/2005US6931833 Pulse combustion device
08/18/2005US20050178856 High-efficiency jet ejector and propulsive jet
08/16/2005US6928804 Pulse detonation system for a gas turbine engine
08/09/2005US6926231 Vertical takeoff and landing aircraft
08/03/2005CN1647999A Aircraft, particularly small aircraft, having a propulsion system including a plurality of pulse detonation engines (PDES)
07/2005
07/28/2005US20050160737 Rotary combustor, and electrical generator comprising a combustor of this type
07/28/2005US20050160715 Rotary combustor, and electricity generator comprising such a combustor
07/27/2005EP1557356A1 Aircraft, particularly small aircraft, having a propulsion system including a plurality of pulse detonation engines (PDEs)
07/27/2005CN1644905A Electrojet self-adaptable impulsive jetting engine device and controlling method thereof
07/21/2005US20050155339 Rotary combustor, and electricity generator comprising such a combustor
07/14/2005US20050151004 Vertical takeoff and landing aircraft
07/13/2005CN1637347A A rotary combustor, and electrical generator comprising a combustor of this type
07/13/2005CN1637346A A rotary combustor, and electrical generator comprising a combustor of this type
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