| Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
|---|
| 11/05/2013 | US8572948 Rocket engine propulsion system |
| 10/31/2013 | WO2013162171A1 Shear coaxial atomization injector of the type which can separately inject three fluids |
| 10/31/2013 | US20130284149 Injection element |
| 10/29/2013 | US8567061 Combustion chamber comprising a cooling unit and method for producing said combustion chamber |
| 10/24/2013 | US20130276426 Cooling Jacket with Porous Matrix |
| 10/23/2013 | EP2525071B1 Continuous detonation wave engine and aircraft provided with such an engine |
| 10/17/2013 | WO2013153340A1 Launcher stage comprising a temporary support structure for temporarily supporting nozzle sections allowing access to the core of the engine |
| 10/17/2013 | US20130269313 Propulsion system for flying machine, particularly for a missile |
| 10/16/2013 | EP2649024A1 Materials and parts that can withstand high temperatures in an oxidising medium, and method for manufacturing same |
| 10/10/2013 | US20130263573 Rocket Stage Having Engine Thrust Frame Integrated With Tank |
| 10/09/2013 | CN203230505U Reverse osmosis type high temperature difference and high pressure thermal protection device |
| 10/03/2013 | WO2013103427A3 Linear detonation wave diverter |
| 10/03/2013 | US20130255223 Hypergolic hybrid motor igniter |
| 10/02/2013 | EP2643580A1 Rocket motor combustion chamber injection head |
| 10/02/2013 | CN203223308U Engine cable laying component of aircraft |
| 09/26/2013 | WO2013105988A3 Clustered, fixed cant, throttleable rocket assembly |
| 09/26/2013 | US20130247542 Space launcher propulsion system implementing a method of regulating propellant component consumption |
| 09/25/2013 | EP2640953A1 Propellant compositions and methods of making and using the same |
| 09/25/2013 | CN203214194U Adjustable straight-flow impact-type injecting apparatus |
| 09/25/2013 | CN203214193U Angle box for composite skirt of solid rocket engine |
| 09/24/2013 | US8539753 Hybrid rocket motor with annular, concentric solid fuel elements |
| 09/19/2013 | US20130239545 Rocket engine pressure sense line |
| 09/19/2013 | US20130239544 Distributed pressurization system |
| 09/18/2013 | CN203201685U Dynamic rocket booster |
| 09/18/2013 | CN103306853A Sandwich structure with shear stiffness between skins and compliance in the thickness direction |
| 09/18/2013 | CN102400815B Layer-board type injection device for oxygen/ methane low-thrust engine |
| 09/18/2013 | CN102400814B Solid-liquid hybrid rocket ramjet for test |
| 09/18/2013 | CN102192046B Thruster of hydrogen-oxygen catalytic ignition mini rocket |
| 09/17/2013 | US8534042 Modular MEMS thruster system utilizing rolled storage, selective deployment and independent initiator |
| 09/12/2013 | US20130233942 Engine apparatus and method for reducing a side load on a flying object |
| 09/12/2013 | US20130232950 Exit Manifold Flow Guide |
| 09/11/2013 | EP2636602A1 Fuel tank |
| 09/11/2013 | CN103291499A Method for achieving pulse detonation rocket engine high-frequency work |
| 09/11/2013 | CN103291498A Laser propulsion device and method based on principle of laser-induced water drop breakdown |
| 09/11/2013 | CN103291496A Cock engine |
| 09/10/2013 | US8528317 Method and system for detecting the ingestion of an object by an aircraft turbine engine during a mission |
| 09/10/2013 | US8528316 Solid propellant gas control system and method |
| 09/04/2013 | CN203175703U Tubular changing structure of solid rocket motor |
| 09/04/2013 | CN103282635A Propellant compositions and methods of making and using the same |
| 08/29/2013 | US20130219901 Combustion chamber provided with a tubular element |
| 08/29/2013 | US20130219719 Fluid injection system |
| 08/28/2013 | CN203161375U Centripetal jet pipe |
| 08/27/2013 | US8516821 Injection element |
| 08/22/2013 | US20130213005 System and method for zero reaction time combustion |
| 08/21/2013 | EP2627886A1 Improved thermal insulation of rocket engines |
| 08/15/2013 | US20130205751 Fast Ignition and Sustained Combustion of Ionic Liquids |
| 08/15/2013 | US20130205750 Igniter for a rocket engine, method for ignition of a rocket engine |
| 08/14/2013 | DE19829810B4 Induktoreinrichtung für eine Pumpe mit hoher Saugkapazität Inductor means for a pump with a high suction capacity |
| 08/14/2013 | CN203130283U Flow equalizer for suppressing flow distortion |
| 08/14/2013 | CN203130282U Integral injector |
| 08/14/2013 | CN103244310A Propellant management system for liquid metal ion propeller |
| 08/14/2013 | CN103244309A Solid rocket punching composite engine shell |
| 08/13/2013 | US8505577 Pnumatically actuated bi-propellant valve (PABV) system for a throttling vortex engine |
| 08/08/2013 | WO2013116390A1 Thermal pressurant |
| 08/08/2013 | US20130199203 Linear Detonation Wave Diverter |
| 08/08/2013 | US20130199155 Rocket Propulsion Systems, and Related Methods |
| 08/06/2013 | US8499543 Casing for insensitive munitions and process for making same |
| 07/31/2013 | CN203098076U Novel recoil type power rotor |
| 07/25/2013 | WO2013107981A1 Rocket engine with optimized fuel supply |
| 07/25/2013 | US20130186059 Dual fuel aircraft system and method for operating same |
| 07/24/2013 | CN102168631B Aluminum film baffle device and pulse solid engine applying same |
| 07/18/2013 | WO2013105988A2 Clustered, fixed cant, throttleable rocket assembly |
| 07/18/2013 | DE112011103264T5 Antriebssystem einer Trägerrakete, das ein Verfahren zur Regelung des Treibstoffverbrauchs verwendet Drive system of a launch vehicle that uses a method for controlling the fuel consumption |
| 07/17/2013 | EP2615400A2 Multi-channel cooling bond pad and corresponding cooling method |
| 07/17/2013 | EP2614242A1 Propulsion system for a flying machine, particularly for a missile |
| 07/16/2013 | US8486541 Co-sintered multi-system tungsten alloy composite |
| 07/11/2013 | WO2013103427A2 Linear detonation wave diverter |
| 07/10/2013 | CN103195613A Pulse detonation rocket engine frequency doubling work control device and control method thereof |
| 07/10/2013 | CN103192997A Method for actively regulating mixture ratio of spacecraft propellant |
| 07/04/2013 | DE112010005752T5 Kühlvorrichtung zum Kühlen von Verbrennungsgasen aus rückstoßfreien Antipanzerwaffen Cooling means for cooling combustion gases from recoilless anti-tank weapons |
| 07/03/2013 | CN103184936A Engine and aircraft |
| 06/27/2013 | US20130160427 Cooling device for cooling combustion gases from recoilless anti-tank weapons |
| 06/27/2013 | US20130160426 Rocket engine injector assembly with cryogenic cavity insulation |
| 06/20/2013 | WO2013088030A1 Pressurizing device and method |
| 06/19/2013 | EP2604840A1 Conveyor device for cryogenic liquids |
| 06/19/2013 | EP2604839A1 Engine |
| 06/19/2013 | EP2604838A1 Dual fuel engine |
| 06/19/2013 | CN103161609A Burning and spraying device |
| 06/19/2013 | CN102207043B Gaseous hydrogen/gaseous oxygen eddy current cooling thrust chamber injector |
| 06/19/2013 | CN102155332B Internal-heating nitrous oxide single component fuel gas generator |
| 06/19/2013 | CN101936240B Coarse and fine adjustment combined pressure annunciator |
| 06/18/2013 | US8465820 Method and plant for the production of a casing for a solid-propellant engine, and casing made according to said method |
| 06/18/2013 | US8465607 Higher-performance solid-rocket propellants and methods of utilizing them |
| 06/18/2013 | US8464640 Controllable digital solid state cluster thrusters for rocket propulsion and gas generation |
| 06/13/2013 | US20130146675 Thrust vector control |
| 06/13/2013 | US20130145746 Vortex cannon with enhanced ring vortex generation |
| 06/13/2013 | US20130145742 Catalytically enhanced gas generator system for rocket applications |
| 06/12/2013 | EP2602466A1 A bomb for deployment from an air vehicle |
| 06/12/2013 | EP2602465A2 Methods and systems for propelling an external powered vehicle |
| 06/06/2013 | WO2013024361A3 Improved rocket engine systems and devices |
| 06/06/2013 | US20130140402 Methods and systems for propelling an externally powered vehicle |
| 06/05/2013 | CN103133183A Safe processing device of low-temperature hydrogen in rocket engine thrust chamber |
| 06/05/2013 | CN101975125B Device for measuring linear burning rate of liquid propellant in high pressure environment |
| 06/05/2013 | CN101907043B High-frequency combustion instability coverall process simulation test automatic regulating system and method |
| 05/29/2013 | EP2597293A2 Rocket stage with liquid propulsion system |
| 05/29/2013 | DE112011102511T5 Mit einem rohrförmigen Element ausgestattete Brennkammer With a tubular element equipped combustor |
| 05/29/2013 | CN202954896U Rocket engine jet pipe expanding section |
| 05/29/2013 | CN103122807A Multichannel solid rocket engine ignition sequence control method |
| 05/28/2013 | US8448881 Fuel injector |
| 05/23/2013 | US20130125527 Reversible flow discharge orifice |