| Patents for F02C 5 - Gas-turbine plants characterised by the working fluid being generated by intermittent combustion (717) |
|---|
| 03/05/2015 | US20150059348 System and method for controlling fuel distributions in a combustor in a gas turbine engine |
| 02/17/2015 | US8955303 Pulse detonation system |
| 02/10/2015 | US8950169 Rotary expansible chamber devices having adjustable working-fluid ports, and systems incorporating the same |
| 01/28/2015 | CN104321515A 每个旋转周期内多喷射燃烧的单阀推进热力学喷气发动机及其方法 Within each rotation cycle multi-injection combustion of single valve jet engine propulsion and thermodynamic methods |
| 01/27/2015 | US8938942 External-combustion, closed-cycle thermal engine |
| 01/06/2015 | US8925296 Jet engine, in particular a jet engine for an aircraft |
| 12/31/2014 | CN1800610B 具有改进的核心机系统的燃气涡轮发动机 Having improved core system of a gas turbine engine |
| 12/02/2014 | US8899010 Pulse detonation combustor |
| 11/25/2014 | US8893467 Direct injection of a discrete quantity of fuel into channels of a wave rotor engine |
| 11/18/2014 | US8887482 Active flow control with pulse detonation actuators |
| 11/11/2014 | US8881500 Duplex tab obstacles for enhancement of deflagration-to-detonation transition |
| 10/09/2014 | WO2014163731A1 Generating energy through physical and chemical energy |
| 10/09/2014 | DE112012005264T5 Rotations-Pulsdetonationstriebwerk Rotation pulse detonation engine |
| 09/23/2014 | US8839599 Axial combustion engine |
| 09/09/2014 | US8826638 Hybrid supercritical carbon dioxide geothermal systems |
| 08/07/2014 | US20140216045 Gas turbine with improved power output |
| 08/07/2014 | US20140216000 Indexed Positive Displacement Rotary Motion Device |
| 08/06/2014 | CN103975141A 具有同心安排的涡轮机部分、冷却通道以及加强壁的转子组件 Having a concentric arrangement of the turbine section, as well as strengthen the walls of the cooling channels of the rotor assembly |
| 07/31/2014 | WO2014114980A2 Standing detonation wave engine |
| 07/15/2014 | US8776946 Gas turbine exhaust cone |
| 06/25/2014 | EP2744993A1 Rotor assembly having a concentric arrangement of a turbine portion, a cooling channel and a reinforcement wall |
| 05/20/2014 | US8726630 System and method for passive valving for pulse detonation combustors |
| 05/13/2014 | CA2517772C High thrust gas turbine engine having improved core system |
| 05/07/2014 | CN102165168B 用于非连续燃烧的燃气透平 For non-continuous combustion of the gas turbine |
| 05/01/2014 | WO2012142485A3 Continuous detonation combustion engine and system |
| 04/29/2014 | US8707674 Pulse detonation tube with local flexural wave modifying feature |
| 04/22/2014 | US8701421 Dynamic combustion chamber |
| 04/17/2014 | WO2014057227A1 Heat engine for driving a drive shaft |
| 04/01/2014 | US8683780 Gas turbine engine and pulse detonation combustion system |
| 03/27/2014 | WO2011152912A3 Supersonic combustor rocket nozzle |
| 03/26/2014 | CN103688037A Apparatus and method for controlling a pressure gain combustor |
| 03/19/2014 | CN103649468A Power augmentation system with dynamics damping |
| 03/05/2014 | EP2702258A1 Apparatus and method for controlling a pressure gain combustor |
| 03/04/2014 | US8661782 Rotating valve assembly for high temperature and high pressure operation |
| 02/12/2014 | CN103573412A Pulse knocking flywheel type engine |
| 02/05/2014 | EP2691609A1 Power augmentation system with dynamics damping |
| 01/30/2014 | WO2013184042A3 Multistage turbomachine (variants) |
| 01/03/2014 | WO2014000072A1 Heat engine operating in accordance with carnot's thermodynamic cycle and control process |
| 12/17/2013 | US8607542 Valveless pulse combustor |
| 12/12/2013 | WO2013182301A1 Method and thermal reactor for single-valve propulsion with multiple injections and combustions per rotation cycle |
| 12/12/2013 | CA2875910A1 Method and thermal reactor for single-valve propulsion with multiple injections and combustions per rotation cycle |
| 12/05/2013 | US20130318990 External Combustion Engine with a General Wheel Power Rotation Motor |
| 11/27/2013 | EP2665898A2 Gas turbine exhaust cone |
| 11/12/2013 | US8578695 Methods and designs for increasing efficiency in engines |
| 10/24/2013 | DE102012103523A1 Internal combustion engine for conversion of combustion of fuel e.g. hydrogen peroxide mixture, has igniter that is provided to ignite fuel in explosion chamber, and turbine is connected with explosion chamber using connecting tube |
| 10/17/2013 | DE102012206123A1 Wärmekraftmaschine mit Freikolbenverdichter Heat engine with free piston compressor |
| 10/16/2013 | EP2650510A2 Thermal engine a for free piston compressor |
| 10/01/2013 | US8544280 Continuous detonation wave engine with quenching structure |
| 09/25/2013 | EP2641025A1 Pulse detonation combustor |
| 09/17/2013 | CA2500522C Rotary pulse detonation system with aerodynamic detonation passages for use in a gas turbine engine |
| 08/29/2013 | US20130219905 Method of optimizing the specific fuel consumption of a twin engine helicopter and twin engine architecture with control system for implementing it |
| 08/27/2013 | US8516788 Pulse detonation engine operating with an air-fuel mixture |
| 08/20/2013 | US8511060 External combustion engine with a general wheel rotation power motor |
| 08/08/2013 | US20130199186 Fan-less Thrust Generating Component for Air-bypass Engine |
| 07/10/2013 | CN103201563A Pulse detonation combustor |
| 07/10/2013 | CN101652549B 旋转装置 Rotating device |
| 06/25/2013 | CA2479235C Gas turbine engine system |
| 06/20/2013 | WO2013089593A1 Turbo-rotary engine |
| 06/20/2013 | WO2013086625A1 Rotary pulse detonation engine |
| 06/20/2013 | CA2857377A1 Rotary pulse detonation engine |
| 06/13/2013 | WO2013083271A1 Method for thermal ignition of a pulsed combustion engine, and thermoreactor with thermal ignition |
| 06/06/2013 | US20130139487 Variable initiation location system for pulse detonation combustor |
| 06/06/2013 | US20130139486 Variable initiation location system for pulse detonation combustor |
| 05/28/2013 | US8448417 Pistonless, rotary internal combustion engine and associated support systems |
| 05/14/2013 | CA2516717C Integral cooling system for rotary engine |
| 05/07/2013 | CA2502796C High efficiency rotor for the first phase of a gas turbine |
| 04/23/2013 | US8424284 High efficiency positive displacement thermodynamic system |
| 04/09/2013 | US8413418 Gas turbine engine |
| 04/04/2013 | DE10347588B4 Gleichraum-Gasturbine Constant-volume gas turbine |
| 04/04/2013 | DE102012019127A1 Method for operating combustion device of gas turbine, involves opening valve by holding device such that compressor air flows to turbine as rinsing and cooling air, and closing valve by holding device at freely-selectable time point |
| 03/28/2013 | WO2013040679A1 Rotor assembly having a concentric arrangement of a turbine portion, a cooling channel and a reinforcement wall |
| 03/28/2013 | CA2849525A1 Rotor assembly having a concentric arrangement of a turbine portion, a cooling channel and a reinforcement wall |
| 03/14/2013 | WO2013035367A1 Working gas-generating device |
| 02/28/2013 | US20130047625 Enhanced pulse detonation engine system |
| 02/12/2013 | US8371103 Valve assembly and method for high temperature internal combustion engines |
| 02/12/2013 | CA2517182C Gas turbine engine having improved core system |
| 01/31/2013 | WO2012116285A3 Wave disc engine apparatus |
| 01/22/2013 | US8356469 Gas turbine engine with dual compression rotor |
| 01/01/2013 | US8341932 Rotary air valve firing patterns for resonance detuning |
| 12/27/2012 | US20120324860 Gas turbine engine and pulse detonation combustion system |
| 11/13/2012 | CA2502791C High efficiency stator for the first phase of a gas turbine |
| 11/01/2012 | WO2012145836A1 Apparatus and method for controlling a pressure gain combustor |
| 11/01/2012 | CA2834285A1 Apparatus and method for controlling a pressure gain combustor |
| 10/04/2012 | WO2012134325A1 Power augmentation system with dynamics damping |
| 09/20/2012 | WO2012097997A3 Gas turbine exhaust cone |
| 09/19/2012 | CN102678387A Rotary-cone blade jet engine and rotary-cone blade combustion engine |
| 09/18/2012 | US8266884 Asynchronous combustion system |
| 08/30/2012 | WO2012113523A1 Jet engine, in particular for an aircraft |
| 08/30/2012 | US20120216503 Engine and combustion system |
| 08/28/2012 | US8250850 Engine using hydrogen as a fuel |
| 08/08/2012 | EP2484881A1 Turbine engine tailcone resonator |
| 07/05/2012 | WO2012092285A1 Gas turbine engine and pulse detonation combustion system |
| 06/21/2012 | US20120151896 Hot gas path component cooling for hybrid pulse detonation combustion systems |
| 06/21/2012 | US20120151895 Hot gas path component cooling for hybrid pulse detonation combustion systems |
| 06/05/2012 | US8191350 Compressed-air or gas and/or additional-energy engine having an active expansion chamber |
| 05/24/2012 | WO2012067885A1 Pulse detonation combustor |
| 05/24/2012 | CA2816893A1 Pulse detonation combustor |
| 04/24/2012 | CA2516720C Low volumetric compression ratio integrated turbo-compound rotary engine |
| 04/19/2012 | DE102011005032A1 Sensorvorrichtung zur Erfassung einer Rotationseigenschaft eines rotierenden Elements Sensor device for detecting a rotation property of a rotating element |
| 04/17/2012 | US8159081 Controlling propeller rotor overspeed |