| Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
|---|
| 05/11/2005 | EP1529163A1 Swivelling nozzle for a rocket engine |
| 05/11/2005 | CN1201076C 火箭发动机 Rocket Engine |
| 05/10/2005 | US6890660 Combustion chamber with internal jacket made of a ceramic composite material and process for manufacture |
| 05/10/2005 | US6890148 Transition duct cooling system |
| 05/10/2005 | US6889496 Combustion chamber structure and its manufacturing process |
| 05/10/2005 | CA2198252C Reduced pollution power generation system and gas generator therefore |
| 05/04/2005 | EP1298389A4 Coaxial spray nozzle injector |
| 05/04/2005 | DE19858197B4 Triebwerk Engine |
| 05/03/2005 | US6886327 Second ductile structural layer superalloy comprising nickel, cobalt, iron, and/or copper; toughness, physical properties, thermoconductivity |
| 04/28/2005 | US20050086928 Wall structure |
| 04/26/2005 | US6883220 Method for forming a tube-walled article |
| 04/21/2005 | WO2005035965A1 Combustion chamber comprising a cooling unit and method for producing said combustion chamber |
| 04/21/2005 | US20050081510 Rocket engine combustion chamber |
| 04/20/2005 | CN1607323A Operated hot flap of asymmetrical nozzle of turbojet |
| 04/20/2005 | CN1197685C Method for producing high heat-flux regenerative loop for rocket engine combustion chamber |
| 04/19/2005 | US6880326 High regression rate hybrid rocket propellants and method of selecting |
| 04/14/2005 | WO2005033498A1 Aerospace laser jet engine |
| 04/14/2005 | WO2004072465A3 Diversion of combustion gas within a rocket engine to preheat fuel |
| 04/14/2005 | US20050077341 Method of manufacturing an active cooling panel out of thermostructural composite material |
| 04/14/2005 | DE10353423B3 Rocket motor casing has cooling passages for fuel or liquid oxygen within concentric structure |
| 04/14/2005 | DE10343049B3 Brennkammer mit Kühleinrichtung und Verfahren zur Herstellung der Brennkammer Combustion chamber with cooling means and methods for making the combustion chamber |
| 04/13/2005 | EP1522711A2 Method of distributing propellant inside a solid-propellant casing, and tool for implementing such a method |
| 04/13/2005 | EP1248902B1 Rocket motor nozzle assembly comprising a refractory metal shell |
| 04/07/2005 | US20050072876 Variably angled propulsion/steering system |
| 04/06/2005 | CN1603599A Minisize chemical propeller with pressure sensor |
| 03/31/2005 | WO2005028844A1 Rocket engine having guide vanes in the nozzle of the engine |
| 03/31/2005 | WO2005028842A2 Controlled autoignition propellant systems |
| 03/31/2005 | WO2004085016A3 Hydrogen powered toy rocket with electrolysis of water |
| 03/29/2005 | US6873945 Rocket motor propellant temperature simulator |
| 03/24/2005 | DE19642407B4 Vorrichtung für die Lageregelung eines Raumflugkörpers mittels Betätigung eines Gasventils mit beweglicher Düse Device for attitude control of a spacecraft by operation of a gas valve with a movable nozzle |
| 03/23/2005 | EP1517032A1 Operated flap for an axisymmetrical exhaust nozzle of a jet engine |
| 03/23/2005 | EP1451544B1 Measuring shear stress at an interface with two walls and two crossed sensor elements |
| 03/23/2005 | CN1598280A Method for preparing composite rail control thrust chamber by pioneer impregnating cracking technology |
| 03/19/2005 | CA2480538A1 Operated hot flap of asymmetrical nozzle of turbojet |
| 03/15/2005 | US6865878 Hybrid rocket engine and method of propelling a rocket |
| 03/09/2005 | EP1511930A1 Wall structure |
| 03/03/2005 | US20050047907 Transition duct cooling system |
| 03/03/2005 | US20050045306 Transpiration cooling system |
| 03/03/2005 | US20050044709 Ablative composite assemblies and joining methods thereof |
| 03/02/2005 | CN1589383A Streamlined body and combustion apparatus having such a streamlined body |
| 03/01/2005 | US6860099 Liquid propellant tracing impingement injector |
| 02/17/2005 | US20050034448 Sliding-action magneto-mechanical injector throttling device |
| 02/17/2005 | US20050034447 Polyoxymethylene as structural support member and propellant |
| 02/10/2005 | US20050028514 Method of insulating a case of a solid propellant rocket motor |
| 02/10/2005 | CA2526591A1 Turbo rocket with real carnot cycle |
| 02/03/2005 | US20050026096 Streamlined body and combustion apparatus having such a streamlined body |
| 02/03/2005 | US20050022500 Rocket engine passivation system |
| 02/01/2005 | US6848163 Comprises high strength aluminum alloy joined with ceramic particulate reinforced metal matrix fitting, using solid-state friction welding; for high-pressure liquids such as propellants in rocket engines |
| 01/27/2005 | US20050017132 Asonic aerospike engine |
| 01/27/2005 | US20050016179 Extendible exhaust nozzle bell for a rocket engine |
| 01/27/2005 | US20050016159 Apparatus comprising a rotary- acting pilot valve |
| 01/27/2005 | US20050016158 Swivelling nozzle for a rocket engine |
| 01/26/2005 | EP1500880A2 A transpiration cooling system |
| 01/25/2005 | US6845605 Hypergolic ignitor |
| 01/20/2005 | DE102004004459A1 Verfahren zur Herstellung einer aktiven Kühltafel aus Thermostruktur-Kompositwerkstoff A method for producing an active cooling panel of thermostructural composite material |
| 01/20/2005 | DE102004004424A1 Aktive Kühltafel aus Thermostruktur-Kompositwerkstoff und Verfahren zur Herstellung selbiger Active cooling panel of thermostructural composite material and method for producing Selbiger |
| 01/12/2005 | EP1494981A1 Protection against oxidation of parts made of composite material |
| 01/12/2005 | EP1171705A4 Rocket engine |
| 01/11/2005 | US6840275 Variable-gravity anti-vortex and vapor-ingestion-suppression device |
| 01/06/2005 | US20050000218 Rocket motor nozzle assemblies having vacuum plasma-sprayed refractory metal shell throat inserts, methods of making, and rocket motors including same |
| 12/30/2004 | DE10325170A1 Rocket-propulsion force increasing method involves supplying auxiliary propellant through cooling route for cooling shell flow drive device which takes in auxiliary propellant to area of drive-device jacket |
| 12/29/2004 | WO2004085252A3 Unitized hybrid rocket system |
| 12/29/2004 | EP1179132B1 Apparatus for controlling the heat transfer to the nozzle wall of expander cycle rocket engines |
| 12/29/2004 | EP1179131B1 An apparatus for controlling the flow separation line of rocket nozzles |
| 12/28/2004 | US6834493 System for reducing pump cavitation |
| 12/23/2004 | US20040255460 Nanophase composite duct assembly |
| 12/22/2004 | EP1187979B1 Rocket thrust chamber |
| 12/21/2004 | US6832471 Expander cycle rocket engine with staged combustion and heat exchange |
| 12/16/2004 | WO2004109085A1 Micropump-based microthruster |
| 12/16/2004 | US20040250530 Rocket engine combustion chamber |
| 12/15/2004 | EP1486660A1 Rocket engine combustion chamber |
| 12/14/2004 | US6829884 Rocket engine combustion chamber having multiple conformal throat supports |
| 12/09/2004 | US20040245406 Micropump-based microthruster |
| 12/09/2004 | US20040245371 Three-axis attitude control propulsion device and flying object comprising the same |
| 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 |
| 12/08/2004 | CN1553050A Method of insulating a case of a solid propellant rocket motor |
| 12/02/2004 | US20040241408 For use with rocket motors and airframe structures which require protection from extreme heat |
| 12/02/2004 | US20040237533 Method for manufacturing outlet nozzles for rocket engines |
| 12/01/2004 | EP1482163A2 Silicone-fiber-cork ablative insulation material |
| 12/01/2004 | CN1178000C Apparatus for controlling heat transfer to nozzle wall of expander cycle rocket engines |
| 12/01/2004 | CN1177999C Apparatus for controlling flow separation line of rocket engine nozzles |
| 11/25/2004 | US20040231766 Propulsion device, flying object comprising the same and propulsion device igniting method |
| 11/25/2004 | US20040231318 Bi-propellant injector with flame-holding zone igniter |
| 11/25/2004 | US20040231316 Method for extending a nozzle and extended nozzle for rocket drives |
| 11/24/2004 | EP1478837A1 Pulse detonation engine and method for initiating detonations |
| 11/23/2004 | US6820840 Hydrogen powered toy rocket utilizing hydrogen from the electrolysis of water |
| 11/23/2004 | US6820412 Hybrid rocket motor having a precombustion chamber |
| 11/18/2004 | WO2004099600A2 Method & apparatus for thrust augmentation for rocket nozzles |
| 11/18/2004 | US20040226280 Monopropellant combustion system |
| 11/18/2004 | US20040226279 Wick injection of colloidal fluids for satellite propulsion |
| 11/17/2004 | EP1477663A2 Monopropellant reactor system and operating method for a reactor system |
| 11/16/2004 | US6817184 Nozzle extension |
| 11/11/2004 | US20040222571 Actively-cooled fiber-reinforced ceramic matrix composite rocket propulsion thrust chamber and method of producing the same |
| 11/10/2004 | EP1412631B1 Method for extending a nozzle and extended nozzle for rocket drives |
| 11/10/2004 | CN1175013C Method for insulating a case of a solid propellant rocket motor |
| 11/04/2004 | US20040218175 Engine spectrometer probe and method of use |
| 11/04/2004 | US20040216464 Pulse combustion device |
| 11/03/2004 | EP1473457A2 Pulse combustor device |