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)
09/2014
09/03/2014EP2772638A2 Rocket engine fuel supply system and method for eliminating the POGO effect
08/2014
08/27/2014EP2769918A1 Detecting propellant levels in spacecraft
08/27/2014EP2768731A1 Device for expelling/containing liquids for a spacecraft tank
08/21/2014US20140230678 Rocket delay apparatuses, systems and methods
08/20/2014EP2766591A1 Jet propulsion device and fuel supply method
08/14/2014US20140223915 Vectored-thrust propulsor
08/14/2014DE102012112867B4 Befestigungsanordnung für Bauteile mit unterschiedlichen thermischen Ausdehnungskoeffizienten Fastening arrangement for components having different coefficients of thermal expansion
08/13/2014CN203769964U 能尾部点火的固体燃料火箭发动机 Energy tail of the solid fuel rocket motor ignition
08/13/2014CN103982332A 一种切换燃料的火箭推力室及其供应系统 A handover rocket thrust chamber and the fuel supply system
08/13/2014CN103982303A 一种基于微透镜阵列实现可燃气体多点激光等离子体点火的方法及装置 A realization of combustible gas multi-point laser plasma ignition method and apparatus based on a microlens array
08/07/2014WO2014120526A2 Enhanced rocket engine fueling systems and methods
08/07/2014WO2014120299A2 Electrically operated propellants
08/06/2014EP2762705A2 Fuel supply system, scramjet engine and method for operating the same
08/06/2014EP2761159A1 Propulsion system
08/06/2014CN103967653A 一种轴向喷注端燃固液火箭发动机结构 An axially end fuel injection hybrid rocket engine structure
07/2014
07/31/2014US20140208767 Fuel supply system, scramjet engine and method for operating the same
07/30/2014CN103953464A 一种对双组元姿控推力器在轨性能进行地面标定的方法 Bipropellant kind of attitude control thruster performance in orbit ground calibration methods
07/30/2014CN103953463A 一种低流阻锥阀 A low flow resistance Poppet
07/30/2014CN103953462A 一种可调汽蚀管 An adjustable tube cavitation
07/30/2014CN103953461A 一种减小吸气式脉冲爆震发动机进气道反压的机械阀 A method for reducing the intake pulse detonation engine inlet anti-pressure mechanical valve
07/30/2014CN103953459A 一种短距起爆高频爆震波的装置及其控制方法 An apparatus and method for controlling short-range high frequency detonating detonation
07/30/2014CN101910002B 空间飞行器尾部装置 Spacecraft tail unit
07/24/2014WO2014113149A1 Antivortex device for multi-outlet liquid reservoir
07/24/2014WO2014111709A1 Rocket motors and their use
07/24/2014US20140202164 Gas turbine engine nozzle including housing having scalloped root regions
07/24/2014US20140202132 High performance liquid rocket propellant
07/23/2014EP2757243A1 Injector element
07/23/2014EP2757242A1 Injector element for rocket engines
07/17/2014US20140196435 Space Impulse Drive
07/16/2014CN203717161U 发动机推进剂温度调节装置 Propellant engine temperature adjusting means
07/16/2014CN103925116A 滑动弧点火装置 Gliding arc ignition device
07/09/2014EP2751415A2 Thermal phase separation
07/09/2014CN203702370U 一种液态空气混合动力的火箭发动机设备 A liquid air hybrid rocket engine equipment
07/02/2014CN203685415U 固体火箭发动机笼式骨架结构扩散段 Solid rocket motor cage skeleton structure diffuser
07/02/2014CN103899438A 一种运载火箭三选二点火装置 One kind of three selected two rocket ignition device
07/02/2014CN103899436A 一种螺旋式多通道脉冲爆震发动机 In a spiral multi-channel pulse detonation engine
07/01/2014US8763362 Injector element which maintains a constant mean spray angle and optimum pressure drop during throttling by varying the geometry of tangential inlets
07/01/2014US8763360 Hollow fan blade tuning using distinct filler materials
06/2014
06/26/2014US20140175191 System for reducing the dynamic behavior of the movable segment of a deployable nozzle for a rocket engine
06/26/2014US20140174054 Feed system and a method of suppressing the pogo effect
06/26/2014DE102012112867A1 Mounting arrangement for connecting e.g. radomes of missiles with different coefficients of thermal expansion, has connecting portion including openings into which fastening elements engage, so that elements prevents movement of components
06/25/2014CN203670027U 整体式喷注器 Integral Injector
06/25/2014CN103883428A 一种吸气式脉冲爆震发动机防反流进气结构 One kind of air-breathing pulse detonation engine anti-reflux intake structure
06/25/2014CN102278233B 超音速转子发动机 Supersonic rotary engine
06/25/2014CN101821491B 使用惯性轮驱动火箭发动机的泵的驱动设备 Use rocket engine flywheel driving a pump drive device
06/18/2014CN103868098A Film cooled flame stabilizer
06/18/2014CN103867341A Space vector torsion resistant device of ball socket wobble nozzle of small solid rocket engine
06/18/2014CN103867340A Dual-rotational-flow inspirator
06/18/2014CN103867339A Ablation-proof structure of solid rocket engine
06/18/2014CN102817745B Low-cost and simple unit round-to-square plug nozzle test device
06/18/2014CN102080607B Motor for forest fire extinguishing bomb
06/05/2014WO2014084344A1 Liquid propellant
06/05/2014WO2014083287A1 Propulsion assembly for rocket
06/05/2014DE102012111681A1 Raumflugantrieb und Flugkörper Spacecraft propulsion and missile
06/04/2014CN103835837A Thermojet generating device based on rotational flow mixing and continuous combustion of gaseous fuels
05/2014
05/30/2014WO2014080126A1 Injection element for the combustion chamber of a rocket engine
05/27/2014US8733079 Electric thruster for a spacecraft
05/22/2014WO2014077889A1 Thrust-producing device with detonation motor
05/22/2014US20140137542 Controlled pyrotechnic train
05/21/2014EP2733340A1 Threaded rod of a system for deploying a deployable propellant nozzle
05/21/2014CN203604065U 一种无催化床的中等浓度过氧化氢/煤油燃烧室 A non-catalytic bed moderate concentrations of hydrogen peroxide / kerosene combustion
05/15/2014WO2014072624A1 Method and device for powering a rocket motor
05/15/2014US20140130603 Device and method relating to a sensing device
05/15/2014US20140130480 Strain measurement device, a solid rocket motor including same, and related methods
05/14/2014EP2729691A1 Injection element
05/14/2014CN203594528U 一种碳纤维复合材料金属膜片贮箱 A carbon fiber composite metal diaphragm tank
05/14/2014CN103790735A 一种火箭基组合循环发动机变结构尾喷管 Rocket based combined cycle engine tailpipe variable structure
05/14/2014CN103790734A 一种液态空气加力助推火箭发动机设备及方法 A liquid booster engine afterburner air apparatus and method
05/07/2014EP2726725A1 A bomb for deployment from an air vehicle
05/07/2014EP2726375A1 Cryogenic fluid tank and its use
05/07/2014CN103775246A 过氧化氢/液氢气体发生器和推力室 Hydrogen peroxide / liquid hydrogen gas generator and thrust chamber
05/06/2014US8713912 Solid propellant rocket motors employing tungsten alloy burst discs and methods for the manufacture thereof
04/2014
04/30/2014CN203570457U Two-stage mixing type nozzle device
04/30/2014CN103758663A Rocket-based combined cycle ejector mode performance test engine
04/30/2014CN103758662A Liquid air hybrid power rocket engine method and equipment
04/30/2014CN102852669B Modularized reusable multiunit circle-to-square compression ratio plug nozzle testing device
04/29/2014US8707676 Radial flow rapid prototyping rocket motors
04/24/2014US20140109552 In-Flight Attitude Control and Direct Thrust Flight Control System of a Vehicle and Craft Comprising Such a System
04/24/2014US20140109551 Solid chemical rocket propulsion system
04/23/2014EP2721278A1 Cryogenic propulsion assembly and method of supplying a tank of such an assembly
04/23/2014CN103742296A Air film cooling spray pipe
04/23/2014CN103738001A Rhenium-based refractory metal hybrid material and structure thereof
04/22/2014US8701414 Injection device for combustion chambers of liquid-fueled rocket engines
04/17/2014WO2014058525A1 Slotted multi-nozzle grid with integrated cooling channels
04/17/2014US20140102109 Propulsion system and rocket having the same
04/17/2014DE102012020159A1 Method for recurring depression of tank gas chamber for liquid hydrogen, particularly for re-ignition of main rocket engine, involves driving main rocket engine with mixture of liquid hydrogen and liquid oxygen
04/16/2014CN103726954A Rocket based combined cycle engine rocket ejector T-type layout
04/16/2014CN103722806A Preparation method of multilayer molybdenum-based heat-proof material
04/16/2014CN102619644B Structure for reducing back pressure of air-breathing type pulse detonation air inlet passage
04/10/2014US20140096510 Slotted multi-nozzle grid with integrated cooling channels
04/09/2014EP2715100A1 System for reducing the dynamics of the mobile segment of a deployable rocket motor nozzle
04/09/2014CN103711610A RBCC fuel gas generator integrated supplying and adjusting system based on liquid oxygen
04/09/2014CN103711609A Method for improving interface bonding performance of EPDM (ethylene prophlenediene monomer) heat insulating layer, HTPB (hydroxyl-terminated polybutadiene) lining and NEPE (nitrate ester plasticized polyether propellant)
04/09/2014CN101821492B Method and device enabling rocket engine pump to be driven by internal combustion engine
04/08/2014US8690000 Cryogenic tank and space launcher including such a tank
04/08/2014US8689540 Component configured for being subjected to high thermal load during operation
04/03/2014WO2014051671A1 Geared gas turbine engine integrated with a variable area fan nozzle with reduced noise
04/02/2014CN203515859U Spray pipe test device
04/02/2014CN203515858U Powder forming press cover for standard test engine
04/02/2014CN103696883A Hydrogen-peroxide-based RBCC (Rocket Based Combined Cycle) engine pressure pumping and squeezing integrated fuel system
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