F02K 99 - Subject matter not provided for in other groups of this subclass

Patents for F02K 99 - Subject matter not provided for in other groups of this subclass (464)
12/2005
12/29/2005	US20050284690 High admittance acoustic liner
12/29/2005	US20050284129 Hybrid propulsion system
12/15/2005	DE10050715B4 Solarwärme-Rakete Solar thermal rocket
12/13/2005	US6973774 Hybrid propulsion system
12/07/2005	EP1601865A1 Compact compound engine package
12/07/2005	EP1601864A1 Integral cooling system for rotary engine
12/06/2005	US6971228 Propulsion device, in particular for a rocket
11/2005
11/24/2005	DE102004056604A1 Inertial jet propulsion especially hydrojet systems for boats has curved ducts for additional thrust prior to expelling fluid through a rear nozzle
11/15/2005	US6964169 Hollow tapered body flattened in the transverse direction, wall being divided transversely into four adjacent parts, trapezoidal wall, made of refractory fibers embedded in another refractory matrics; vapor deposit refractory matrics; durability
11/10/2005	DE10118005B4 Mikrotriebwerk Micro-engine
10/2005
10/13/2005	DE102005005533A1 Antriebseinrichtung für ein Sekundärluft-Einblassystem Drive device for a secondary air injection
09/2005
09/29/2005	US20050210866 Drive device for a secondary air injection system
09/29/2005	US20050210862 Quantum jet turbine propulsion system
09/06/2005	US6938406 Propulsion device, in particular for a rocket
08/2005
08/18/2005	US20050178106 Enhanced performance torroidal coolant-collection manifold
08/17/2005	EP1564398A1 Toroidal coolant-collection manifold
08/04/2005	US20050166574 Propulsion device, in particular for a rocket
05/2005
05/10/2005	US6890660 Combustion chamber with internal jacket made of a ceramic composite material and process for manufacture
04/2005
04/27/2005	EP1526073A1 Equipment to nullify gravitational force
04/14/2005	WO2005033498A1 Aerospace laser jet engine
04/12/2005	US6877309 Nuclear-fueled power generating system
03/2005
03/24/2005	DE102004007632A1 Catalyzer laser drive for generating heat quickly has high-frequency resonance unit to use an oscillating laser for applying heat to the catalyzer so as to vaporize fuel fed via injection holes
03/17/2005	DE10350734B3 Solar-thermal drive unit for rocket propulsion system has hollow chamber body and heating channel system
01/2005
01/13/2005	US20050005608 Long life nozzle flap for aircraft turbojets
12/2004
12/09/2004	US20040244360 Rocket engine tubular chamber with single piece jacket
12/09/2004	US20040244356 Thermal transpiration pump for gaseous material driven by chemical reaction
12/08/2004	EP1484496A1 Rocket engine tubular combustion chamber with single piece jacket
12/01/2004	EP1482158A1 Movable exhaust nozzle flap of a turbomachine with extended durability
12/01/2004	CN1550655A Process for replacing an abradable on the fan case of a turbojet
11/2004
11/25/2004	US20040231155 Method of replacing an abradable portion on the casing on a turbojet fan
10/2004
10/27/2004	EP1471212A1 Method to replace an abradable layer on a gas turbine fan casing
10/26/2004	US6808145 Dual-mode airbreathing propulsion system
10/20/2004	CN1538051A Long service life jet deflection plate for turbine jet motor of aircraft
10/07/2004	US20040194445 Antimatter engine
09/2004
09/02/2004	WO2004074654A1 Integral cooling system for rotary engine
09/02/2004	WO2004074653A1 Compact compound engine package
07/2004
07/29/2004	DE10300621A1 Jet drive method for glider aircraft, water or air vehicle, model or toy, using fan system with one or more fan units for generating propulsion jets
07/22/2004	US20040139723 Microwave heat-exchange thruster and method of operating the same
07/08/2004	US20040133396 Appliance for reading identification connectors
07/08/2004	US20040128979 Combustion chamber with internal jacket made of a ceramic composite material and process for manufacture
06/2004
06/03/2004	US20040103639 Rocket engine member and a method for manufacturing a rocket engine member
06/01/2004	US6742325 Method of generating thrust and electrical power from an optical solar image
05/2004
05/12/2004	EP1418478A1 Apparatus for reading identification connectors
04/2004
04/21/2004	EP1411225A1 Acoustic liner for gas turbine engine
04/15/2004	DE10246201A1 Rocket propulsion unit for operation at high reaction temperatures, introduces dust particles into reaction plasma to reduce thermal conduction to walls
03/2004
03/10/2004	EP1396631A2 Liquid rocket engine and rocket comprising said engine
02/2004
02/12/2004	US20040026572 Dual-mode airbreathing propulsion system
12/2003
12/18/2003	US20030230071 Wall structure
11/2003
11/13/2003	US20030209005 Wick injection of liquids for colloidal propulsion
10/2003
10/23/2003	DE10226223C1 Bypass jet turbine motor, for model aircraft, has at least two micro turbo air jet motors arranged equidistantly around the main turbine shaft as the combustion chamber, surrounded by a radial bypass ring channel
10/15/2003	EP1352170A1 Rocket engine member and a method for manufacturing a rocket engine member
09/2003
09/25/2003	WO2003078818A1 Solar-heated rocket engine and the operating method thereof
09/25/2003	US20030177756 Apparatus and method for positron fueled ramjet operation
09/18/2003	US20030173469 Combined thrust and power generator for a satellite
08/2003
08/27/2003	CN1119629C Weighing charging element
07/2003
07/22/2003	US6594984 Combined thrust and power generator for a satellite
07/17/2003	US20030131583 Combined thrust and power generator for a satellite
06/2003
06/10/2003	US6574951 Solar thermal rocket
03/2003
03/11/2003	US6530212 Laser plasma thruster
02/2003
02/11/2003	US6517341 Injecting effective amount of elemental silicon and/or silicon-containing compound into combustion gas environment to prevent or reduce volatilization of silica film located on silicon-containing ceramic or ceramic composite
01/2003
01/30/2003	US20030021974 Combustion chamber with internal jacket made of a ceramic composite material and process for manufacture
12/2002
12/12/2002	US20020184873 Propulsion device, in particular for a rocket
12/12/2002	DE10126926A1 Brennkammer mit Innenmantel aus einem keramischen Komposit-Material und Verfahren zur Herstellung Combustion chamber with inner shell made from a ceramic composite material and method for producing
12/03/2002	US6488233 Laser propelled vehicle
10/2002
10/24/2002	DE10118005A1 Micro-rocket operating with periodic explosive combustion, includes distributor, combustion chamber, igniter and flame traps in supply lines
10/03/2002	US20020139107 Solar thermal rocket
08/2002
08/22/2002	WO2002064427A1 Steam rocket engine for ground effect vehicles, hovercrafts and seaplanes
07/2002
07/18/2002	WO2002055864A1 Rocket engine member and a method for manufacturing a rocket engine member
07/02/2002	US6412274 Solar thermal rocket
04/2002
04/30/2002	US6378290 High-frequency ion source
04/09/2002	US6367739 Compound exhaust system
01/2002
01/01/2002	US6334302 Variable specific impulse magnetoplasma rocket engine
12/2001
12/20/2001	DE10126797A1 Solare thermische Rakete Solar thermal rocket
09/2001
09/18/2001	US6290185 Solar thermal rocket
09/18/2001	US6290184 Flying craft with water and air propulsion source
06/2001
06/12/2001	US6246162 Ion optics
05/2001
05/31/2001	DE10050715A1 Solarwärme-Rakete Solar thermal rocket
05/03/2001	DE19948229C1 Hochfrequenz-Ionenquelle An rf ion source
03/2001
03/22/2001	DE19942834A1 Rocket propulsion drive method uses injection of water into gas plasma for providing water vapor discharged via rocket engine jets
10/2000
10/17/2000	US6131385 Integrated pulsed propulsion system for microsatellite
10/04/2000	CN1268624A Straight directional propulsion plant
09/2000
09/07/2000	DE19909846A1 Flat propulsion drive e.g. for aircraft, space vehicle or turbine drive, has large number of microjet propulsion units incorporated in multilayer surface
08/2000
08/30/2000	EP1031546A1 Method to prevent recession loss of silica and silicon-containing materials in combustion gas environments
08/10/2000	DE19906161A1 Rear charger jet propulsion system has rear charger that converts residual thermal energy of jet engine hot exhaust gases into additional thrust with two sub-systems mounted parallel to axis
05/2000
05/23/2000	US6065284 Refractory heat transfer module
03/2000
03/14/2000	US6036636 Endoscope with tip portion disposed on distal side of insertion portion
12/1999
12/23/1999	DE19827506A1 Solar turboprop aircraft for running on solar energy and normal fuel
09/1999
09/30/1999	WO1999049202A2 System for supplying a working medium in a nuclear rocket engine
05/1999
05/20/1999	DE19746588A1 Starting aid for vehicles starting in water
05/04/1999	US5899060 Wall structure for fuel-cooled rocket engine walls
03/1999
03/24/1999	EP0903487A2 Integrated pulsed propulsion system for microsatellite
05/1998
05/20/1998	DE19748795A1 Endoscope with elongated introduction region and tip region on distal side of this
01/1998
01/28/1998	CN1171545A Weighing charging element
11/1997
11/12/1997	CN2267331Y Quantitative volume combustion type jet propulsion plant
10/1997
10/01/1997	EP0798544A2 Load cell
07/1997
07/10/1997	DE19602731C1 Reduced thermal stress wall structure for a rocket drive mechanism
05/1997
05/07/1997	DE19541183A1 Hydrodynamic drive device
01/1997
01/21/1997	US5595358 Multipurpose airborne vehicle
05/1996
05/28/1996	US5520356 System for propelling and guiding a solid object with a beam of electromagnetic radiation
11/1995
11/23/1995	WO1995031691A1 Energy discharge device with pressure and/or thermal effect

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