Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02K - Jet-propulsion plants › F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689)
09/2010
09/07/2010US7789018 Gas generator assembly
09/07/2010US7788900 Electrically controlled extinguishable solid propellant motors
09/02/2010US20100218482 System and method for cooling rocket engines
09/02/2010DE102008006953B4 System und Verfahren zur Reduktion von Schadstoffen in Triebwerksabgasen System and method for reducing harmful substances in engine exhaust gases
09/01/2010EP2222565A1 Spacecraft afterbody device
09/01/2010CN101821492A Method and device enabling rocket engine pump to be driven by internal combustion engine
09/01/2010CN101821491A Device for powering the pump of rocket engine using inertia wheel
08/2010
08/31/2010US7784269 System and method for cooling rocket engines
08/31/2010US7784268 Partial superheat cycle for operating a pump in a rocket system
08/25/2010EP1446611B1 Use of an aerodynamic body and combustion device provided with an aerodynamic body of this type
08/25/2010CN201560862U Distributed jetting mechanism
08/19/2010US20100205933 Regeneratively cooled porous media jacket
08/19/2010US20100205929 Basalt fiber and nanoclay compositions, articles incorporating the same, and methods of insulating a rocket motor with the same
08/18/2010CN101806261A Method and device for measuring pneumatic thrust indirectly
08/18/2010CN101806260A Multitube parallel pulse detonation combustion chamber and ignition detonation method thereof
08/11/2010CN201546837U Engine for forest fire extinguishing bombs
08/10/2010US7770380 Methods of controlling solid propellant ignition, combustion, and extinguishment
08/05/2010WO2010086091A1 Jet engine, in particular a jet engine for an aircraft
08/05/2010US20100192539 Methods of controlling thrust in a rocket motor
08/05/2010CA2748891A1 Jet engine, in particular a jet engine for an aircraft
07/2010
07/29/2010US20100186368 Ignition/ chemical reaction promotion/ flame holding device, speed-type internal combustion engine, and furnace
07/29/2010DE102008022289B4 Flugkörper Missile
07/28/2010EP2209981A2 Propulsion nozzle for the expansion of a supersonic gas jet
07/28/2010CN101787939A Detonation chamber with jetting mechanism
07/27/2010US7762195 Slow cook off rocket igniter
07/27/2010US7762058 Ultra-compact, high performance aerovortical rocket thruster
07/27/2010US7762056 Aircraft combination engines exhaust thrust recovery
07/22/2010US20100180575 Engine wall structure and a method of producing an engine wall structure
07/22/2010US20100180443 Method For Fabricating Structural Propellants
07/22/2010DE102007008942B4 Einspritzkopf für die Brennkammer eines Raketentriebwerks Injection head for the combustion chamber of a rocket engine
07/21/2010EP2208012A1 Casing for insensitive munitions and process for making same
07/21/2010CN101782466A Cooling water system design for test bed
07/21/2010CN101782465A Gas pressure reduction system design
07/21/2010CN101782030A Multiunit coaxial injector component for test and manufacturing method
07/21/2010CN101782029A Device for testing flow characteristics of gas-gas nozzle
07/21/2010CN101782028A Hydrogen-oxygen fuel-rich precombustion chamber for full flow staged combustion cycle engine
07/21/2010CN101782027A Gas-gas injector suitable for mass flow and design method
07/20/2010US7757476 Catalytically activated transient decomposition propulsion system
07/15/2010US20100175367 Propellant device of enhanced performance
07/14/2010CN101776029A Combustion pursuing device
07/14/2010CN101776028A Hold-down and release simulation data source system
07/14/2010CN101776027A Air suction type liquid fuel pulse detonation engine
07/14/2010CN101776026A Air inlet of air-breathing pulse detonation engine
07/14/2010CN101539069B Pressure stability control device supplied with constant voltage by propellant
07/08/2010US20100170223 Control and/or drive device for a flying body
07/07/2010CN101769824A Quantitative feed electric control pressure reductor, characteristic test system for pressure reductor and automatic test method
07/07/2010CN101768716A Aeroengine combustor liner with surface coated with oxidation resistant coating
07/07/2010CN101768715A Method for preparing antioxidant coating of combustion liner of aeroengine
07/07/2010CN101412122B Vertical type method for processing nozzle cooling channel of liquid-propel land rocket engine
07/01/2010WO2010072681A1 Reusable module for a launcher
07/01/2010WO2010072002A1 Metal hydrazide materials
07/01/2010CA2747821A1 Metal hydrazide materials
06/2010
06/30/2010CN101761419A Baffled air-intake device of pulse detonation engine
06/30/2010CN101761418A Oil-supply system of pulse detonation engine
06/24/2010DE102008061917A1 Heißgaskammer Hot gas chamber
06/23/2010EP2199584A2 Rocket combustion chamber
06/23/2010EP2198145A2 Method and device enabling a rocket engine pump to be driven by an internal combustion engine
06/23/2010EP2198144A1 Device for powering the pump of a rocket engine using an inertia wheel
06/23/2010CN101749986A Multifunctional interceptor missile
06/23/2010CN101749143A Distribution-type spouting mechanism of secondary propellant of pulse detonation engine
06/23/2010CN101476523B Miniature propeller based on MEMS nozzle chip
06/17/2010WO2010068636A2 Regeneratively cooled porous media jacket
06/17/2010US20100146934 Hot Gas Chamber
06/16/2010CN101738319A Oxygen-enriched fuel gas supply device and method for fuel gas injector
06/16/2010CN101738316A Method for designing structure of low-cost test combustion chamber with reliable thermal protection
06/16/2010CN101737805A Low-cost inside diameter-variable combustion chamber and design and test method thereof
06/16/2010CN101737538A Flow control valve device and design method for flow control type hole
06/16/2010CN101737201A Laser propulsion device
06/16/2010CN101737200A Modularized heat-capacity type thrust chamber
06/16/2010CN101737199A Liquid propellant conveying system of blow-down rocket engine
06/16/2010CN101737198A Gas-gas nozzle with constriction section
06/16/2010CN101737197A Dual concentric gas-gas nozzle
06/10/2010DE19616838B4 Brennkammer mit Schwitzkühlung Combustion chamber with transpiration
06/02/2010CN201497435U Rocket type ice slush blasting missile and launching device and system thereof
06/02/2010CN101718236A Multitube pulse detonation combustion chamber communicated with jet deflector
06/01/2010CA2440063C Chemical vapour infiltration method for densifying porous substrates having a central passage
05/2010
05/20/2010DE102008058723A1 Drive system, particularly for small satellites for producing moment change of satellite and for use as sustainer engine for satellite, has engine operated with solid fuel and supplying device for solid fuel
05/19/2010EP2187031A1 Control system for a process factor of a rocket engine
05/19/2010EP2185805A1 Multi-functional pulse-divided rocket
05/13/2010US20100115917 Method and Device for Supplying a Space Propulsion Engine with Liquid Cryogenic Propellants
05/12/2010CN201461132U Rocket engine jet pipe with ignition device
05/06/2010US20100107602 Electrolytic igniter for rocket engines using liquid propellants
05/06/2010US20100107601 Electrolytic igniter for rocket engines using monopropellants
05/06/2010DE102008056056A1 Propulsion unit is worked on basis of catalytic or chemical decomposition of liquid source of energy, particularly hydrazine, and has flange arranged between injecting valve and combustion chamber
05/05/2010EP2182198A1 Pressure container for high-temperature use and a method for production of same
05/04/2010US7707820 Control and/or drive device for a flying body
04/2010
04/29/2010DE102009045704A1 Verfahren und Vorrichtung zur Berechnung einer Start- oder Stopsequenz eines Motors Method and apparatus for calculation of a start or stop sequence of a motor
04/28/2010EP2180166A1 Ignition and chemical reaction accelerator and flame stabilizer, speed-type internal combustion engine, and furnace
04/28/2010CN101699053A Oxygen-complementing type air-hydrogen/air-oxygen pneumatic resonance heat surface igniter
04/27/2010US7703274 Pintle injector
04/27/2010US7703273 Dual-mode chemical-electric thrusters for spacecraft
04/21/2010EP2176591A2 Device for injecting a fuel or a fuel/oxidiser pre-mixture, comprising means for passive control of the combustion instabilities
04/15/2010WO2010042095A2 Systems, methods and apparatus for propulsion
04/14/2010CN101694189A Super-conducting electromagnetic pump circulating system of liquid rocket engine
04/08/2010WO2010037561A1 Container for receiving and storing liquids and viscous substances and method for the production thereof
04/08/2010US20100083634 Solid fuel rocket, solid rocket fuel and method
04/08/2010DE102008049842A1 Einspritzelement für eine Raketenbrennkammer und Einspritzsystem Injection element for a rocket combustion chamber and injection system
04/07/2010EP2172636A2 Injector for a rocket combustion chamber and injection system
04/07/2010CN101691849A Combustion-supporting method by activating oxygen molecules by using laser
04/06/2010US7690601 Reversible space plane
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