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)
01/2013
01/02/2013CN101497372B External cowling of scramjet engine and design method thereof
01/01/2013US8341932 Rotary air valve firing patterns for resonance detuning
12/2012
12/20/2012WO2012171094A1 Combustion systems and combustion system components for rotary ramjet engines
12/20/2012US20120318886 Micro-nozzle thruster
12/20/2012CA2839456A1 Combustion systems and combustion system components for rotary ramjet engines
12/19/2012CN202611856U High-pressure air source compression system
12/06/2012WO2012165742A1 Rotating fuel injection device for ramjet engine and ramjet engine provided with same
12/06/2012DE102011103221A1 Vorrichtung zur Schuberzeugung Apparatus for generating thrust
12/05/2012CN202578943U Jet ignition device for pulse detonation engine
12/05/2012CN202578942U Detonation chamber for pulse detonation engine
11/2012
11/28/2012CN102797590A Plasma excitation-based method for restraining separation of boundary layer in air inlet passageway
11/27/2012US8319357 Starter system for portable internal combustion engine electric generators using a portable universal battery pack
11/22/2012WO2012156597A1 Turbine engine including a detonation chamber and aircraft provided with such a turbine engine
11/22/2012WO2012156596A1 Continuous detonation wave engine and aircraft provided with such an engine
11/22/2012WO2012156595A1 Ramjet including a detonation chamber and aircraft comprising such a ramjet
11/21/2012EP2525071A1 Continuous detonation wave engine and aircraft provided with such an engine
11/21/2012EP2525070A1 Ramjet engine with detonation chamber and aircraft comprising such a ramjet engine
11/21/2012EP2525062A1 Turbomachine with detonation chamber and aircraft provided with such a turbomachine
11/20/2012US8312706 Pulse combustor including acoustic elements
11/14/2012CN102777252A High-pressure gas source compression system
11/07/2012EP2519720A2 Integrated aero-engine flowpath structure
11/07/2012CN102052254B Power generator utilizing wind energy and fuel chemical energy
11/01/2012WO2012145836A1 Apparatus and method for controlling a pressure gain combustor
11/01/2012CA2834285A1 Apparatus and method for controlling a pressure gain combustor
10/2012
10/30/2012US8297058 Apparatus and method for processing airflow with flowfield molded hypersonic inlet
10/26/2012WO2012118994A3 Fault tolerant control system for distributed micro-thrusters
10/26/2012WO2012094351A3 Highly integrated inside-out ramjet
10/24/2012CN202500674U Gas taking liner used for ramjet engine
10/24/2012CN102748161A Particle engine
10/23/2012US8292217 Hypersonic inlet systems and methods
10/03/2012CN202468058U Disc generator of turbine
10/03/2012CN102705108A Periodic alternating current drive low-temperature plasma ignition method and system
10/03/2012CN102705107A Solid chemical micro-thruster
09/2012
09/27/2012WO2012129579A1 Engine
09/27/2012US20120240550 Vehicle Propulsion System
09/26/2012CN202451298U Flywheel turbine
09/26/2012CN101240756B Wheel engine
09/24/2012DE212010000200U1 Vorrichtung zur Schubleistungserzeugung für Fahrzeuge Apparatus for generating thrust for vehicles
09/12/2012EP2496819A1 Optimal feedback heat energy internal combustion engine and its applications
09/12/2012EP2496813A2 A method of controlling engine performance
09/07/2012WO2012116398A1 Engine for use in an aerial vehicle
09/07/2012WO2012075078A3 Hybrid variable area fuel injector with thermal protection
09/05/2012CN101575012B Power switching method for hypersonic lifting body aircraft and aircraft
08/2012
08/30/2012WO2012113523A1 Jet engine, in particular for an aircraft
08/29/2012CN101858278B Multi-tube detonation lateral wave ignition device
08/16/2012US20120204534 System and method for damping pressure oscillations within a pulse detonation engine
08/08/2012EP2483545A2 Internally nested variable-area fuel nozzle
08/08/2012EP1718857B1 Integrated air inlet system for multi-propulsion aircraft engines
08/02/2012US20120192546 Catalytic Converter for a Pulse Detonation Turbine Engine
08/01/2012EP2480771A1 A system and method of combustion for sustaining a continuous detonation wave with transient plasma
08/01/2012CN102619643A Jet ignition device of pulse detonation engine
07/2012
07/25/2012CN102606682A Spiral bevel gear set for ram air turbine
07/25/2012CN102606344A Electromagnetic aerospace engine
07/25/2012CN102606343A Detonation chamber of pulse detonation engine
07/25/2012CN102606342A Metal/water/air reaction feedback type engine and high-speed sea flitting aircraft with diving function
07/24/2012US8225505 Method of forming a rotating blade assembly
07/18/2012CN202338414U 一种新型脉冲发动机 A new impulse engines
07/18/2012CN102597481A Optimal feedback heat energy internal combustion engine and its applications
07/18/2012CN102588145A Air-breathing rotary detonation wave injection and multimode ram detonation coupled circulating propulsion system
07/18/2012CN102588144A Flywheel turbine
07/18/2012CN102588111A Backflow compression system for air compression
07/18/2012CN102588080A Dynamic fluid gas working medium compression system
07/12/2012WO2012094351A2 Highly integrated inside-out ramjet
07/11/2012CN102575584A Internally nested variable-area fuel nozzle
07/11/2012CN102563667A Turbojet injecting incineration device and incineration method
07/04/2012EP2472089A2 Flade discharge in 2-d exhaust nozzle
07/04/2012CN102536515A Miniature aircraft pulse detonation engine
07/04/2012CN101718226B Non-intermittent detonation rotor of engine
06/2012
06/28/2012US20120159956 Top cycle power generation with high radiant and emissivity exhaust
06/26/2012US8205433 Pulse detonation/deflagration apparatus and related methods for enhancing DDT wave production
06/21/2012US20120151898 System and method of combustion for sustaining a continuous detonation wave with transient plasma
06/14/2012US20120144836 Integrated aero-engine flowpath structure
06/14/2012US20120144798 Fluidic deflagration-to-detonation initiation obstacles
06/07/2012WO2012075078A2 Hybrid variable area fuel injector with thermal protection
06/07/2012CA2818430A1 Hybrid variable area fuel injector with thermal protection
05/2012
05/31/2012WO2012069729A1 Combined turbojet and ramjet engine
05/31/2012US20120131901 System and method for controlling a pulse detonation engine
05/23/2012CN202228211U Aviation air injection motor
05/16/2012CN202220677U Center rocket type bi-modal ramjet engine with circular structure
05/16/2012CN102452401A Ultrahigh-speed train with electromagnetic-induction turbine engine
05/10/2012WO2012058758A1 Multiple mode jet engine
05/09/2012EP2400137A9 Rotating ram-jet turbine with exhaust turbocharger
05/09/2012CN102444500A Hypersonic accelerator engine and application method
04/2012
04/25/2012CN202203066U Hot-punching engine
04/25/2012CN202202986U 引射喷气发动机 Ejector jet engine
04/05/2012US20120079806 Pulse detonation tube with local flexural wave modifying feature
04/04/2012EP2436903A2 Pulse detonation tube with local flexural wave modifying feature
04/04/2012EP2435660A2 Hydrogen engine
04/04/2012CN102400814A Solid-liquid hybrid rocket ramjet for test
03/2012
03/30/2012CA2753033A1 Pulse detonation tube with local flexural wave modifying feature
03/21/2012CN102383971A Multilevel hot stamping engine
03/14/2012CN102374071A Center rocket type bimodal ramjet with circular structure
03/14/2012CN102374070A Injection jet engine
03/14/2012CN102374069A Hot-stamping engine
03/08/2012WO2011131493A3 Air breathing reaction propulsion engine
03/06/2012US8127555 Flowpath heat exchanger for thermal management and power generation within a hypersonic vehicle
03/06/2012US8127533 System and method for power production using a hybrid helical detonation device
03/06/2012US8127527 Methods and systems for operating oxidizer systems
03/01/2012US20120047873 Duplex tab obstacles for enhancement of deflagration-to-detonation transition
02/2012
02/29/2012CA2749478A1 Duplex tab obstacles for enhancement of deflagration-to-detonation transition
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