Patents
Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689)
01/2011
01/13/2011CA2769293A1 Tiered porosity flashback suppressing elements for monopropellant or pre-mixed bipropellant systems
01/12/2011CN101943082A Heating gasification device for liquefied gas micro-propulsion system
01/11/2011US7866041 Method of manufacturing a duct for a gas turbine engine
01/06/2011WO2009150069A3 Combustion chamber device, and method for the operation of a combustion chamber device
01/05/2011EP1689996B1 Injection element
01/05/2011EP1668236B1 Combustion chamber comprising a cooling unit and method for producing said combustion chamber
01/05/2011DE102007007568B4 Vorrichtung zur Steuerung der Düsenschubrichtung eines Raketentriebwerks Device for controlling the direction of thrust nozzle of a rocket engine
01/05/2011CN201696167U Multi-tube parallel-connection pulse detonation combustion chamber
01/05/2011CN101936241A Method for identifying combustion end of solid-propellant rocket engine in real time
01/05/2011CN101936240A Coarse and fine adjustment combined pressure annunciator
01/05/2011CN101576024B Heat returning closed cooling recirculation system of Brighton scramjet
12/2010
12/30/2010US20100327110 Guiding system for aircraft nacelle maintenance
12/30/2010US20100326045 Multiple-use rocket engines and associated systems and methods
12/30/2010US20100326044 Method for cooling rocket engines
12/30/2010US20100326043 Expander cycle rocket engine nozzle
12/29/2010EP2265891A1 Flying object
12/28/2010US7856806 Propulsion system with canted multinozzle grid
12/23/2010WO2010147912A1 Eyeball seals for gimbaled rocket engines, and associated systems and mtehods
12/23/2010DE4493074B4 Einspritzsystem mit konzentrischen Schlitzen und zugehörigen Einspritzelementen Injection with concentric slots and associated injection elements
12/23/2010DE102008058722A1 Solid propellant element for pulsed plasma thruster-type electrical driving mechanism of satellite drive system, serves as monolithic helix provided with complete coils, where solid propellant includes polymer material as main component
12/22/2010EP2263938A2 Cooling device for effusion or transpiration cooling
12/16/2010US20100313544 Propulsion system with canted multinozzle grid
12/16/2010DE102009025457A1 Kühlvorrichtung für eine Effusions- oder Transpirationskühlung Cooling device for a effusion or transpiration
12/15/2010CN201671725U Low-flow resistance detonation wave reinforcing device and detonation combustion chamber with reinforcing device
12/15/2010CN201671724U Detonation chamber with secondary distributed injection mechanism
12/15/2010CN101915184A Double operating mode squeezing type conveying system and design method thereof
12/15/2010CN101915183A Double-working-condition stepped flow control valve and design method of control structure thereof
12/15/2010CN101915182A Solid-propellant rocket engine
12/15/2010CN101915181A Controller for initiating explosive device
12/15/2010CN101545416B Solid rocket engine
12/09/2010WO2010141111A2 Multiple-use rocket engines and associated systems and methods
12/09/2010US20100307131 Cartridge-Loaded Rocket Motor with Castellated Grain Segments
12/08/2010EP1319123B1 Use of a composition, feeding method, and device for pressurizing a propellant tank
12/08/2010CN101910002A Spacecraft afterbody device
12/08/2010CN101907043A High-frequency combustion instability coverall process simulation test automatic regulating system and method
12/08/2010CN101907042A Aspirated engine combustion chamber for eliminating combustion oscillation in suction type
12/08/2010CN101907041A Propane liquid gas micro propulsion device suitable for micro-nano satellite
12/08/2010CN101907040A Nitrogen cold gas micro propulsion device adopting ring storage tank
12/08/2010CN101907039A Nitrogen cold air micro-propeller adopting three cylindrical propelling agent storage boxes
12/02/2010WO2010136691A1 Part for attaching together the mobile portion of a deployable divergent nozzle of a propulsive unit and a mechanism for deploying said mobile portion
12/02/2010US20100303673 Solar energy powered molecular engine
12/02/2010US20100301159 Mounting set, system and method
12/02/2010US20100300067 Component configured for being subjected to high thermal load during operation
11/2010
11/30/2010US7841166 Jet-type steam engine
11/25/2010DE102010016327A1 Treibstoffeinspritzdüse Fuel injector
11/24/2010CN101892925A Aircraft range-extending technique
11/23/2010US7836678 Propulsion system
11/17/2010EP2250363A1 A component configured for being subjected to high thermal load during operation
11/11/2010US20100281850 Buried radial flow stereolithographic rocket motor
11/10/2010EP2249018A2 Missile with a ram jet engine
11/10/2010CN201627650U Detonation chamber with secondary propellant distributed injection mechanism
11/10/2010CN101881238A Air-breathing pulse detonation engine and detonation method thereof
11/09/2010US7827781 Liquid propellant rocket engine with pintle injector and acoustic dampening
11/04/2010US20100275576 System and method for maneuvering rockets
11/04/2010DE102008061917B4 Heißgaskammer Hot gas chamber
11/04/2010DE102007036883B4 Raketenmotor Rocket motor
11/03/2010EP2245291A2 Pellet loaded attitude control rocket motor
11/03/2010CN101539073B Multi-pin micro-Newton colloid thrustor
11/03/2010CN101539070B Propellant blowing device in engine pipelines
11/02/2010US7823836 Optimal sun safe attitude for satellite ground tracking
11/02/2010US7823376 Thrust augmentation in plug nozzles and expansion-deflection nozzles
10/2010
10/28/2010US20100272577 Jet vane and method for manufacturing a jet vane
10/28/2010US20100269487 Thermally-integrated fluid storage and pressurization system
10/28/2010US20100269484 Solid propellant gas control system and method
10/27/2010CN201614995U 一种吸气式脉冲爆震发动机防反流机构 One kind of air-breathing pulse detonation engine anti-reflux mechanism
10/20/2010CN201610802U 螺旋式脉冲爆震发动机的爆震管 Spiral tube pulse detonation engine knock
10/20/2010CN201610801U 一种脉冲爆震发动机的折流式进气装置 A pulsed detonation engine's intake system Baffled
10/19/2010US7815146 Combustible outgassing material lined altitude compensating rocket nozzle
10/19/2010US7814835 Propulsion enhancement arrangement for rocket
10/14/2010WO2010068636A3 Regeneratively cooled porous media jacket
10/14/2010US20100257840 Injection device for combustion chambers of liquid-fueled rocket engines
10/13/2010CN201606164U 一种脉冲爆震增强装置 A pulsed detonation enhancement device
10/13/2010CN201606163U 一种吸气式脉冲爆震发动机进气道 One kind of air-breathing pulse detonation engine inlet
10/13/2010CN201606162U 一种脉冲爆震发动机的供油系统 A pulsed detonation engine fuel supply system
10/13/2010CN201606161U 一种脉冲爆震火箭发动机远程无线控制装置 A pulsed detonation rocket engine remote radio control device
10/13/2010CN101858278A Multi-tube detonation lateral wave ignition device
10/07/2010WO2010112766A1 Deployable divergent nozzle for a propulsive unit
10/07/2010US20100252686 Method and device enabling a rocket engine pump to be driven by an internal combustion engine
10/07/2010US20100251920 Casing for insensitive munitions and process for making same
10/07/2010US20100251695 Rocket engine for use with aerodynamic fuel ribbon, and fuel ribbon for rocket and method
10/07/2010US20100251694 Solid composite propellants and methods of making propellants
10/06/2010CN101852148A Oxygen/kerosene ignitor using pneumatic resonance ignition technology
10/06/2010CN101852147A Hydrogen-oxygen gas dynamic resonance surface igniter
10/06/2010CN101852146A Novel small hydrogen-oxygen engine head
10/05/2010CA2482001C Protection against oxidation of parts made of composite material
09/2010
09/30/2010WO2010082971A3 Insensitive rocket motor
09/29/2010EP2233727A2 Fuel-cooled flexible heat exchanger with thermoelectric device compression
09/22/2010EP2230394A2 Component for use in hot gas flows
09/22/2010CN201588707U Detonation chamber provided with secondary propellant distribution spouting mechanism
09/22/2010CN101539072B Visual device of filling state of liquid pipeline
09/16/2010US20100229389 Combustion chamber comprising a cooling unit and method for producing said combustion chamber
09/16/2010DE102009013150A1 Bauteil zum Einsatz in Heißgasströmungen Component for use in streams of hot gas
09/15/2010EP2227629A2 Combustion chamber device
09/15/2010CN101832198A Hydrogen-oxygen oxygen-rich preburner of full flow staged combustion cycle engine
09/09/2010US20100224731 Propulsion system and method using a combustion chamber discharging a concentrated mass
09/09/2010US20100223904 Gas turbine engine
09/08/2010CN101825042A Pulse detonation engine (PDE) magnetic valve high frequency oil supply and ignition system
09/08/2010CN101539068B Filling device of liquid propellant and method thereof
09/08/2010CN101539067B Hole type micro-Newton colloid thrustor
09/08/2010CN101244455B Method for shaping throat liner lining
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