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)
04/2014
04/02/2014CN103696882A Fast reactor propeller
04/02/2014CN102635463B Cold-flow test device for one-unit linear plug spray pipe
03/2014
03/27/2014WO2014046842A1 System for decoupling drive shaft of variable area fan nozzle
03/27/2014WO2014044939A1 Cooling method
03/27/2014US20140083081 Rocket engine systems
03/27/2014DE102013110435A1 Divergierendes Düsenteil mit Strahlablenkern für Feststofftriebwerke Divergent nozzle part with beam deflectors for solid fuel engines
03/27/2014DE102007048527B4 Schubtriebwerk Thruster
03/26/2014EP2710248A2 Power supply system and method for eliminating the pogo effect
03/26/2014CN203499854U Engine fuel supply system
03/26/2014CN203499853U Rocket propellant grain fixing device
03/26/2014CN103670802A Small air pillow pressurization system
03/26/2014CN103670801A Multi-redundancypump control servo mechanism for thrust vector control of liquid oxygen kerosene engine
03/26/2014CN103670800A Propellant pipe cross conveying system
03/26/2014CN103670799A Normal temperature pressure supplementing system with redundancy function
03/26/2014CN103670798A Method for improving interface adhesive performance of NEPE propellant and lining
03/20/2014WO2014040998A1 Anaerobic hybrid propulsion device with fuel present in the form of divided solids
03/19/2014CN103649511A Injection element
03/19/2014CN103644047A Igniting and starting device of solid rocket engine
03/19/2014CN103644046A Charging grain structure of solid rocket engine
03/19/2014CN103644045A Charging grain structure of solid rocket engine
03/19/2014CN103644044A Multi-component simulative engine applied to vacuum plume effect experimental research and ignition scheme thereof
03/13/2014US20140069289 Distributed ordnance system, multiple stage ordnance system, and related methods
03/11/2014US8667776 Pellet-loaded multiple impulse rocket motor
03/06/2014WO2014011279A3 Turbine engine exhaust nozzle flap
02/2014
02/27/2014WO2014031190A2 Method to produce high specific impulse and moderate thrust from a fusion-powered rocket engine
02/27/2014WO2014029937A1 Bimodal igniter and injection method for a rocket engine igniter
02/26/2014CN103603746A Continuous gel and pasty propellant supply device for rocket engine
02/19/2014DE202013011092U1 Variables Kontraktionsdüsentriebwerk Variables contraction jet engine
02/19/2014CN103590924A High-rigidity propellant management device for large surface tension storage box
02/19/2014CN103590923A Bubble filter for bubble trap of surface tension storage tank
02/19/2014CN103590922A Surface tension storage tank low flow resistance channel
02/19/2014CN103590921A Adjustable gel propellant three-time jet flow impact atomizing device
02/19/2014CN103590905A Method for realizing efficient heat-work conversion and engine applying same
02/12/2014CN102434316B Bipropellant micro chemical propulsion array device
02/06/2014WO2014022836A2 Universal elliptical-sliced solid grain geometry and coupled grill-feedthrough featured assembly for solid rocket motor and coaxial hybrid rocket design
02/05/2014EP2693033A1 Aircraft/spacecraft fluid cooling system and aircraft/spacecraft fluid cooling device
02/05/2014CN103557094A High-concentration hydrogen peroxide catalysis bed structure used for ground test of solid-liquid hybrid rocket motor
02/05/2014CN103557093A Multiple-combustor continuous pouring dosage accurate control device
02/05/2014CN102292264B Reusable module for launcher
01/2014
01/30/2014US20140026537 Multiple Use Hybrid Rocket Motor
01/30/2014US20140026535 High specific impulse superfluid and nanotube propulsion device, system and propulsion method
01/29/2014CN103541833A Single-spray-pipe rocket combustion-gas stream drainage device
01/29/2014CN103541832A Engine fuel supplying system
01/28/2014US8635875 Gas turbine engine exhaust mixer including circumferentially spaced-apart radial rows of tabs extending downstream on the radial walls, crests and troughs
01/22/2014CN103527347A Turbine generator assembly for thrust vector control
01/22/2014CN102056864B Process for producing a self-healing layer on a part made of a C/C composite
01/16/2014WO2014009659A1 Method for supplying a missile engine with a storable propellant
01/16/2014US20140013724 Electromagnetic thruster
01/15/2014EP2683930A1 Injector for mixing two propellants comprising at least one injection element with a tricoaxial structure
01/15/2014CN103511125A Resistor top-mounted type micro-thruster and manufacturing method thereof
01/09/2014WO2014006303A1 Method for controlling a variable nozzle section of an aircraft
01/09/2014US20140007555 Turbine generator assembly for thrust vector control
01/09/2014CA2877836A1 Method for controlling a variable nozzle section of an aircraft
01/08/2014EP2682590A2 Turbine generator assembly for thrust vector control
01/08/2014EP2681439A1 Engine for use in an aerial vehicle
01/03/2014WO2014001686A1 Turbopump
01/03/2014WO2013158195A3 In-tank propellant mixing
01/02/2014DE102012012536A1 Feststoffantrieb Solid drive
01/01/2014EP2679794A2 Solid-fuel propulsion device
01/01/2014CN103485934A Thrust boosting system and method for engine
12/2013
12/26/2013US20130340407 Clustered, fixed cant, throttleable rocket assembly
12/25/2013EP2676026A1 Propulsion and maneuvering system with axial thrusters and method for axial divert attitude and control
12/25/2013EP2676025A1 Rocket engine with augmented expander cycle
12/25/2013EP2676024A2 Clustered, fixed cant, throttleable rocket assembly
12/25/2013CN103470401A Nuclear fusion impulse-type direct injection engine
12/24/2013US8613190 Pressure vessels for high temperature applications and a method for their manufacture
12/24/2013US8613189 Centrifugal impeller for a rocket engine having high and low pressure outlets
12/18/2013CN203347941U Anti-electromagnetic interference engine ignition tool
12/18/2013CN102062020B Transparent combustion chamber with square interior passage
12/18/2013CN101059097B Ring-shape cylinder piston wheel engine
12/12/2013US20130327016 Ignition device for two-pulse rocket motor with thermal barrier membrane
12/12/2013US20130327015 Dual use hydrazine propulsion thruster system
12/11/2013EP2672099A1 Device for closing and opening a nozzle, in particular an expansion nozzle of a rocket engine
12/11/2013CN203335276U Direction-adjustable spray pipe used for solid attitude and orbit control power system
12/11/2013CN103437914A Variable-cycle air turbine combined engine of rocket
12/11/2013CN103437913A Metal diaphragm storage box made of carbon-fiber composite materials and manufacturing method thereof
12/10/2013US8601790 Buried radial flow rapid prototyping rocket motors
12/10/2013US8601787 Rocket nozzles for unconventional vehicles
12/05/2013US20130318943 Rocket motor combustion chamber injection head
12/05/2013DE102007055239B4 Messung der Rotationsgeschwindigkeit einer Hohlwelle einer Strömungsmaschine Measuring the rotational speed of a hollow shaft of a turbomachine
12/04/2013CN103423032A Solid rocket ramjet fuel gas flow regulation device driven by linear motor
12/04/2013CN102619643B Jet ignition device of pulse detonation engine
12/03/2013US8596039 Device for injecting a mono-propellant with a large amount of flow rate modulation
12/03/2013US8596038 Liquid propellant tank and vapor jet emitting device including same
11/2013
11/28/2013WO2013177368A1 Solid state ignition safety device
11/27/2013EP2666723A1 Propulsion system for satellite attitude control and orbit control
11/27/2013CN103410632A Electric conical valve type gas flow regulator for solid rocket ramjets
11/21/2013US20130305687 Thruster and Spacecraft
11/20/2013EP2664774A2 Thruster and spacecraft
11/20/2013EP2604838B1 Dual fuel engine
11/20/2013CN103402948A Materials and parts that can withstand high temperatures in an oxidising medium, and method for manufacturing same
11/19/2013US8584588 Ammunition comprising means for neutralizing its explosive charge
11/19/2013US8584443 Method and system for controlling solid propellant thrust
11/14/2013WO2013169193A1 Improved reactor for ammonium dinitramide-based liquid monopropellants, and thruster including the reactor
11/14/2013WO2013169192A1 Improved reactor for ammonium dinitramide-based liquid mono-propellants, and thruster including the reactor
11/13/2013CN203285567U Combined type spray pipe structure
11/13/2013CN203285566U Solid rocket ramjet subsection motor case connection structure
11/13/2013CN203285565U Shock-resisting solid ramjet engine shell body connecting lug structure
11/12/2013US8578700 Gas turbine engine with fluid mixing arrangement
11/06/2013CN101907042B Aspirated engine combustion chamber for eliminating combustion oscillation in suction type
1 2 3 4 5 6 7 8 9 10 11 12 13 ... 47