Patents
Patents for F02K 7 - Plants in which the working-fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof (1,599)
04/2011
04/27/2011EP2313635A1 Thruster comprising a plurality of rocket motors
04/21/2011US20110088370 Pulsed detonation engine
04/20/2011CN201802507U Supersonic-speed rotor engine
04/20/2011CN102022223A An eddy current ramjet engine
04/20/2011CN101446301B Miniature high-speed air turbine pump
04/19/2011US7927568 Method of and apparatus for CO2 capture in oxy-combustion
04/14/2011WO2011041822A1 Optimal feedback heat energy internal combustion engine and its applications
04/14/2011US20110083420 Subsonic and Stationary Ramjet Engines
04/14/2011CA2811529A1 Optimal feedback heat energy internal combustion engine and its applications
04/13/2011CN201794667U Air suction pulse detonation engine inlet
04/07/2011WO2011041049A2 Internally nested variable-area fuel nozzle
04/07/2011CA2776136A1 Internally nested variable-area fuel nozzle
04/06/2011CN102003302A Air intake cone of air-breathing pulse detonation engine
04/06/2011CN102003301A 粒子发动机 Particle Engine
03/2011
03/31/2011WO2011037597A1 A system and method of combustion for sustaining a continuous detonation wave with transient plasma
03/16/2011CN101985904A Detonation pipe for high-frequency pulse detonation engine and control method thereof
03/15/2011US7905084 Rotary pressure rise combustor for a gas turbine engine
03/03/2011US20110047962 Pulse detonation combustor configuration for deflagration to detonation transition enhancement
03/03/2011DE102010037173A1 Pulsdetonationseinlasssteuersystem Pulse detonation intake control system
03/03/2011DE102010037039A1 Pulsdetonations-Brennerkonfiguration zur Verbesserung des Übergangs von Verpuffung zur Detonation Pulse detonation burner configuration to improve the transition from deflagration to detonation
02/2011
02/24/2011DE102009019789A1 Jet engine is provided with nozzle outlet of pressure chamber with mutually open sleeve, where negative pressure in gas outlet and surrounding medium are accelerated
02/16/2011CN101975122A Stabilized knocking engine with magnetic fluid energy bypath system
02/10/2011US20110030379 Energy- deposition sytems,eguipment and method for modifying and controling shock waves and supersonic flow
02/09/2011CN101968013A Single-tube rotary valve type double-bypass pulse detonation engine
02/02/2011CN201730700U Free fan stress application jet engine
02/02/2011CN201730699U Gas piston pulse engine
01/2011
01/27/2011WO2010136402A3 Hydrogen engine
01/26/2011EP2276920A2 Subsonic and stationary ramjet engines
01/26/2011CN101956631A Air inlet channel of air-breathing type pulse detonation engine
01/26/2011CN101956630A Flywheel machine
01/26/2011CN101377307B Flight-shaped two-phase mixing and intensified burning apparatus
01/05/2011CN201696166U Aspirated impulse knocking engine
01/05/2011CN201696165U Pulse detonation engine with side-intake rotating drum
01/05/2011CN101936239A Centrifugal rotor fan driver
01/05/2011CN101936238A Jet engine with electric propulsion function
01/05/2011CN101934860A Helicopter using centrifugal rotor engine
01/05/2011CN101576024B Heat returning closed cooling recirculation system of Brighton scramjet
12/2010
12/29/2010CN101929407A Centrifugal rotor engine
12/22/2010EP2264296A2 System for altering fluid flow
12/14/2010US7849670 Propulsion system with integrated rocket accelerator
12/08/2010CN101907038A Jet-type ramjet combustion chamber for eliminating combustion oscillation
12/02/2010WO2010136402A2 Hydrogen engine
11/2010
11/25/2010DE102009019916A1 Flugkörper mit einem Staustrahltriebwerk Missile with a ramjet
11/11/2010US20100281873 Variable Supersonic Mach Number Air Heater Utilizing Supersonic Combustion
11/10/2010EP2249018A2 Missile with a ram jet engine
11/10/2010CN101881238A Air-breathing pulse detonation engine and detonation method thereof
11/10/2010CN101509438B Self-adapting strengthened heat exchange system heat exchange method of ultra-burning ramjet
11/09/2010US7828243 SCRAMjet arrangement for hypersonic aircraft
11/03/2010CN101576025B Multi-mode spraying pipe with adjustable throat for ramjet engine
11/02/2010US7823836 Optimal sun safe attitude for satellite ground tracking
10/2010
10/20/2010CN101865050A Balancing a ram air turbine
10/13/2010CN101858279A Secondary-burning stamping combustion chamber having rectangular section channel with wide working range
10/13/2010CN101858278A Multi-tube detonation lateral wave ignition device
10/07/2010US20100251692 Methods of combining a series of more efficient aircraft engines into a unit, or modular units
09/2010
09/30/2010WO2009133304A8 Pulse detonation engine
09/30/2010US20100242486 Fuel-cooled heat exchanger with thermoelectric device compression
09/30/2010US20100242437 Fuel-cooled flexible heat exchanger with thermoelectric device compression
09/29/2010EP2233728A2 Fuel-cooled heat exchanger with thermoelectric device compression
09/29/2010EP2233727A2 Fuel-cooled flexible heat exchanger with thermoelectric device compression
09/21/2010US7797943 Core burning for scramjet engines
09/19/2010CA2696289A1 Rotary air valve firing patterns for resonance detuning
09/16/2010US20100229529 Timing control system for pulse detonation engines
09/08/2010CN101825041A Gas piston pulse engine
09/01/2010CN101818704A Ground-based simple cycle pulse detonation combustor based hybrid engine for power generation
08/2010
08/31/2010US7784267 Detonation engine and flying object provided therewith
08/25/2010EP1446611B1 Use of an aerodynamic body and combustion device provided with an aerodynamic body of this type
08/25/2010CN101560929B Variable incidence scramjet engine outboard cowl
08/24/2010US7780099 High-efficiency jet ejector and propulsive jet
08/19/2010US20100205932 Partial filling of a pulse detonation combustor in a pulse detonation combustor based hybrid engine
08/18/2010CN101806260A Multitube parallel pulse detonation combustion chamber and ignition detonation method thereof
08/18/2010CN101806259A Inner culvert turbofan and ram-type double-mode engine
08/05/2010WO2010086091A1 Jet engine, in particular a jet engine for an aircraft
08/05/2010CA2748891A1 Jet engine, in particular a jet engine for an aircraft
07/2010
07/29/2010US20100186370 Pulse detonation engine operating with an air-fuel mixture
07/29/2010DE102009059223A1 Steuerungssystem für ein landgestütztes Einfachzyklus-PDC-Hybridtriebwerk zur Energieerzeugung Control system for a land-based PDC simple-cycle hybrid engine for power generation
07/28/2010CN101787938A 能动机 Can be motivated
07/27/2010US7762077 Single-stage hypersonic vehicle featuring advanced swirl combustion
07/27/2010US7762056 Aircraft combination engines exhaust thrust recovery
07/21/2010CN101205851B Combustion jet engine
07/20/2010US7758334 Valveless pulsed detonation combustor
07/06/2010US7748211 Vapor cooling of detonation engines
06/2010
06/24/2010WO2010046704A3 Method and system for altering engine air intake geometry
06/23/2010CN1961142B Pulse jet engines
06/23/2010CN101749142A Integrated burner with back step precombustion stage and V-groove main combustion stage
06/22/2010US7739867 Compact, low pressure-drop shock-driven combustor
06/16/2010CN101737196A Air-ejection heat protection structure of front edge of support plate of scramjet engine
06/16/2010CN101737195A Rotary punching engine
06/09/2010CN101725432A Jet engine of seaplane
06/09/2010CN101725431A Electric fuel oil jet propeller
06/02/2010CN101718226A Non-intermittent detonation rotor of engine
06/02/2010CN101716995A Waved wing and waved surface of object
05/2010
05/27/2010US20100126178 Hybrid propulsive engine including at least one independently rotatable turbine stator
05/27/2010US20100126140 Millimetre-scale engine
05/19/2010CN101709680A Air jet engine using piston engine as air compressor and application thereof
05/12/2010CN201461131U Self-priming jet engine for aircraft
05/12/2010CN101705883A Stamping rotor engine
04/2010
04/28/2010EP2180164A1 Method and system for altering engine air intake geometry
04/28/2010CN101699052A Curve injection engine and application thereof
04/08/2010US20100083668 Hybrid propulsive engine including at least one independently rotatable compressor stator
04/07/2010CN101691201A Novel power device for generating electric energy and thrust based on micro-combustion
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