| Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
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| 10/16/2007 | US7281367 Steerable, intermittently operable rocket propulsion system |
| 10/11/2007 | DE102006012977A1 Thermal-insulating layer system for use in e.g. gas turbine, has active thermal-insulating layer counteracting heat flow, which is defined by intrinsic thermal conductivity of passive poor heat conducting thermal-insulating layer |
| 10/10/2007 | EP1843124A1 Generic initiation and control structure for trajectory control systems comprising a crown of gas generators |
| 10/04/2007 | DE3601957B3 Wärmeschutzauskleidung für Brennkammern von Strahltriebwerken Heat resistant lining for combustion chambers of jet engines |
| 09/27/2007 | US20070220860 Apparatus and method for controlling leakage in steam turbines |
| 09/27/2007 | DE19719777B4 Vorrichtung zur Begrenzung der Brandgefahr im Inneren einer Turbomaschine A device for limiting the risk of fire in the interior of a turbomachine |
| 09/26/2007 | EP1837277A2 Multifunctional launch vehicle of combined scheme with cruise liquid rocket engine systems (LRESs) |
| 09/26/2007 | CN101042096A Plasma recombination boosting turbine fan jet aerial engine |
| 09/25/2007 | US7273352 Inlet partial blades for structural integrity and performance |
| 09/25/2007 | CA2350150C Support system for a motorized flying machine in a wind tunnel |
| 09/20/2007 | WO2007105552A1 Resin-made cage and bearing |
| 09/20/2007 | DE102006010804A1 Hochtemperatur-Drucksensorelement, insbesondere zur Messung von Drücken innerhalb von Triebwerken, Verfahren zu dessen Herstellung und Bauteil für Triebwerke High-temperature pressure sensor element, in particular for measuring pressures within engines, process for its preparation and component for engines |
| 09/18/2007 | US7270044 Plasma firing mechanism and method for firing ammunition |
| 09/13/2007 | DE102005030437B4 Antriebsvorrichtung auf Basis gelförmigen Treibstoffs und Verfahren zur Treibstoff-Förderung Drive device based gel fuel and process for fuel-promotion |
| 09/11/2007 | CA2262059C Dual-fuel engine capable of operating at least in a ramjet mode and a superramjet mode |
| 09/06/2007 | DE10206701B4 Antriebsvorrichtung Driving device |
| 08/23/2007 | US20070193250 Side thruster module |
| 08/22/2007 | EP1820955A2 Integrated airbreathing and non-airbreathing engine system |
| 08/21/2007 | US7257939 Sliding-action magneto-mechanical injector throttling device |
| 08/15/2007 | CA2578554A1 Integrated airbreathing and non-airbreathing engine system |
| 08/14/2007 | US7254936 Simple solid propellant rocket engine and super-staged rocket |
| 08/08/2007 | CN101012786A High-frequency pulse pinking engine and control method thereof |
| 08/07/2007 | US7251941 Ablative afterburner |
| 08/07/2007 | US7251928 Pulse detonation engine and valve |
| 08/02/2007 | US20070175222 Multipurpose gas generator ramjet/scramjet cold start system |
| 07/25/2007 | EP1811163A2 Gas augmented rocket engine |
| 07/19/2007 | US20070163228 Gas augmented rocket engine |
| 07/19/2007 | US20070163227 Nozzles with rotatable sections for variable thrust |
| 07/19/2007 | CA2568545A1 Gas augmented rocket engine |
| 07/18/2007 | EP1807621A1 Device for the supply of a rocket motor with fuel and oxidiser |
| 07/18/2007 | EP1458968B1 A component for being subjected to high thermal load during operation and a method for manufacturing such a component |
| 07/18/2007 | CN101000136A Cooling of a multimode injection device for a combustion chamber, particularly for a gas turbine |
| 07/18/2007 | CN101000135A Multimode injection system for a combustion chamber, particularly of a gas turbine |
| 07/18/2007 | CN101000023A Extremum oxydizing fuel |
| 07/12/2007 | WO2007002517A3 Methods and systems for controlling multi-body vehicles with fuel slosh |
| 07/11/2007 | CN1325784C Impulse administration plan of solid propellant gas generator having high quality flow regulating rate |
| 07/05/2007 | WO2007023449A3 Engine |
| 07/05/2007 | US20070152096 Rocket engine having guide vanes in the nozzle of the engine |
| 07/05/2007 | DE10230231B4 Mehrschichtiger Verbundwerkstoff The multi-layered composite material |
| 06/28/2007 | US20070144140 High propellant mass fraction hybrid rocket propulsion |
| 06/28/2007 | DE19924907B4 Feststofftriebwerk für eine Staustrahlrakete Solid engine for a ramjet missile |
| 06/27/2007 | EP1801404A2 Heat shield for rocket nozzle |
| 06/27/2007 | EP1801011A1 Propellant tank |
| 06/27/2007 | CN1987077A Explosion auxiliary jet engine |
| 06/21/2007 | US20070137176 Thrust termination device for solid rocket motor |
| 06/21/2007 | DE102005062030B3 Hitzeschild zur Montage an einem wärmestrahlenden Gegenstand, insbesondere an einem Raketentriebwerk A heat shield for mounting on a heat-radiating object, in particular a rocket engine |
| 06/21/2007 | DE102004006665B4 Einspritzelement in Koaxialbauweise mit zwei Brennzonen Injection element in coaxial design with two firing zones |
| 06/20/2007 | CN1321950C Dinitramide based liquid mono-propellants |
| 06/19/2007 | CA2347300C Manufacturing method of ceramic matrix composite |
| 06/14/2007 | WO2007065220A1 Hybrid rocket system |
| 06/14/2007 | DE102005059502A1 Heißkammer Hot chamber |
| 06/13/2007 | EP1795806A2 Warm chamber |
| 06/12/2007 | CA2266936C Thermal protection structure |
| 06/07/2007 | WO2007033043A3 Thrust augmentation in plug nozzles and expansion-deflection nozzles |
| 06/06/2007 | DE10346836B4 Verfahren zum Aufbringen eines Beschichtungsmaterials und Herstellungsverfahren einer Raketentriebwerk-Verteilereinrichtung mit einer Kupferauflage A method for applying a coating material and method of manufacturing a rocket engine-distributing device having a copper layer |
| 06/06/2007 | DE102005005156B4 Triebwerk Engine |
| 06/06/2007 | CN2908821Y Nozzle of rocket engine |
| 06/06/2007 | CN2908820Y Combustion chamber of rocket engine |
| 06/05/2007 | CA2378915C Method for fabricating ceramic matrix composite |
| 05/24/2007 | US20070113537 Thrust termination device for solid rocket motor |
| 05/23/2007 | CN2903956Y Low-turbulent gas supply pipe for micro-pushing force tester |
| 05/23/2007 | CN1317238C Method for preparing composite rail control thrust chamber by pioneer impregnating cracking technology |
| 05/18/2007 | WO2007022771A3 Propelling nozzle for missiles with a deployable nozzle extension |
| 05/17/2007 | US20070112091 Low density rocket motor insulation |
| 05/15/2007 | US7216477 Method and apparatus for a rocket engine power cycle |
| 05/15/2007 | US7216476 Two-axis thrust vectoring nozzle |
| 05/09/2007 | EP1783350A2 Non axi-symmetric shaped cooling liner within a gas turbine engine exhaust duct |
| 05/08/2007 | US7213392 Rocket engine combustion chamber |
| 05/03/2007 | US20070095048 Propulsion device with enclosed plenum |
| 05/02/2007 | EP1780395A1 Injector in particular for a rocket engine |
| 05/02/2007 | CN1313769C Streamlined body, use thereof, and combustion apparatus for burning fuel mixture |
| 05/01/2007 | US7210282 Case burning rocket |
| 04/26/2007 | US20070089397 Injection element |
| 04/26/2007 | US20070089396 Eductor swirl buster |
| 04/25/2007 | EP1511930B1 Wall structure |
| 04/19/2007 | DE112005000795T5 Gaserzeugeranordnung Gas generator assembly |
| 04/19/2007 | DE102005049686A1 Injection element for a rocket engine comprises an inner element with a first outlet opening provided with a unit for splitting a fuel component into at least two media streams |
| 04/11/2007 | EP1771700A2 Beam control surface and method for the production of a beam control surface |
| 04/10/2007 | US7200987 Off-axis pulse detonation configuration for gas turbine engine |
| 03/29/2007 | US20070068138 Rocket vehicle and engine |
| 03/29/2007 | US20070068137 Injection device for combustion chambers of liquid-fueled rocket engines |
| 03/29/2007 | US20070068136 Structural turbine engine casing |
| 03/28/2007 | EP1766220A1 Method for detecting complete draining of a propellant tank and for propellant management onboard a satellite |
| 03/27/2007 | US7194853 Pressurizer for a rocket engine |
| 03/27/2007 | US7194852 Propulsion from combustion of solid propellant pellet-projectiles |
| 03/22/2007 | WO2007033043A2 Thrust augmentation in plug nozzles and expansion-deflection nozzles |
| 03/22/2007 | US20070062176 Liquid propellant rocket engine with pintle injector and acoustic dampening |
| 03/15/2007 | WO2007030039A1 A method of producing an engine wall structure |
| 03/15/2007 | WO2007030038A1 An engine wall structure and a method of producing an engine wall structure |
| 03/15/2007 | US20070056262 Laser propulsion thruster |
| 03/15/2007 | US20070056261 Thrust augmentation in plug nozzles and expansion-deflection nozzles |
| 03/15/2007 | DE102005039742A1 Schubdüse für Raketen mit ausfahrbarer Düsenverlängerung The thruster rocket with extendable nozzle extension |
| 03/13/2007 | US7188417 Advanced L-channel welded nozzle design |
| 03/06/2007 | US7185857 Thrust vector actuation control system and method |
| 03/06/2007 | US7185675 Reduced gain thrust control valve |
| 03/01/2007 | US20070044450 Powder propellant-based space propulsion device |
| 02/27/2007 | US7182980 Annular substrates are stacked in an enclosure; gas containing at least one precursor of a matrix material to be deposited within the pores of the substrates is channeled inside the enclosure; residual gas is extracted |
| 02/13/2007 | US7174704 Split shroud exhaust nozzle |
| 02/08/2007 | DE4337581B4 System zur Versorgung von Motoren eines Raumfahrzeuges mit flüssigem Treibstoff System for the supply of engines of a spacecraft with liquid fuel |
| 02/06/2007 | CA2275767C A deployable diverging part for a thruster |