F02C 5 - Gas-turbine plants characterised by the working fluid being generated by intermittent combustion

Patents for F02C 5 - Gas-turbine plants characterised by the working fluid being generated by intermittent combustion (717)
02/2007
02/15/2007	WO2007018521A1 An improved rotary internal combustion engine
01/2007
01/25/2007	US20070017202 Internal Combustion Engine and Method
01/25/2007	US20070017201 Internal Combustion Engine and Method
01/25/2007	US20070017200 Internal Combustion Engine and Method
01/17/2007	CN1898499A Thermal power plant with sequential combustion and reduced co2 emissions and method for operating a plant of this type
01/10/2007	CN2856447Y Jet
12/2006
12/27/2006	EP1736649A1 Method for converting low-grade energy and a fuelless jet engine for carrying out said method
12/19/2006	US7150143 Hybrid fuel cell-pulse detonation power system
12/14/2006	DE102004058928B4 Konzentrierter Turbinen Antriebsmotor Concentrated turbines drive motor
12/13/2006	CN1878935A Latching mechanism for combustion chamber plate of a fastener driving tool
11/2006
11/23/2006	US20060260291 Pulse detonation assembly with cooling enhancements
11/21/2006	US7137243 Constant volume combustor
11/16/2006	US20060254252 Pulse detonation assembly and hybrid engine
11/14/2006	US7134285 Adiabatic power generating system
11/14/2006	US7134270 External combustion engine
11/07/2006	US7131260 Multiple detonation initiator for frequency multiplied pulsed detonation combustion
11/02/2006	US20060242940 Rotary engine using traditional pistons of flexible motion
10/2006
10/24/2006	US7124573 Rotary pulse detonation system with aerodynamic detonation passages for use in a gas turbine engine
10/24/2006	US7124571 Rotary internal combustion engine
10/18/2006	EP1483489B1 Gas turbine with intermittent combustion
10/11/2006	EP1710425A1 Pulse combustion device
10/11/2006	EP1710417A2 Pulse combustion device
10/10/2006	US7117663 Air breathing, hydrogen fueled jet engine for high speed aircraft
09/2006
09/28/2006	WO2006083320A3 Ultra micro gas turbine
09/28/2006	US20060213201 Pulse combustion device
09/26/2006	US7111463 Combustion wave ignition for combustors
09/21/2006	US20060207261 Rotary pulse detonation system with aerodynamic detonation passages for use in a gas turbine engine
09/14/2006	DE112004000709T5 Pulsierendes Gasturbinentriebwerk Pulsating gas turbine engine
09/05/2006	US7100377 Methods for operating gas turbine engines
09/05/2006	US7100360 Pulsed combustion engine
08/2006
08/31/2006	US20060191501 Flywheel vane combustion engine
08/24/2006	US20060185347 Air breathing, hydrogen fueled jet engine for high speed aircraft
07/2006
07/12/2006	CN1800610A Gas turbine engine having improved core system
06/2006
06/28/2006	CN1793629A Full steam-operation internal combustion engine
06/21/2006	CN1789686A Pulsating flow gas turbine
06/21/2006	CN1789685A High-thrust gas turbine engine including improved core system
06/06/2006	US7055308 Detonation damper for pulse detonation engines
05/2006
05/30/2006	US7051510 Method of operating a pulsejet
05/24/2006	EP1658422A1 Revolving toroidal motor
05/23/2006	US7047724 Combustion ignition
05/17/2006	CN1773079A High efficiency rotor for the first phase of a gas turbine
05/11/2006	US20060096295 Methods for operating gas turbine engines
05/11/2006	US20060096293 Pulsed combustion engine
05/04/2006	WO2006047241A2 Gerotor apparatus for a quasi-isothermal brayton cycle engine
05/04/2006	CA2584964A1 Gerotor apparatus for a quasi-isothermal brayton cycle engine
03/2006
03/22/2006	EP1637712A2 Gas turbine engine having improved core system
03/22/2006	EP1637711A2 High thrust gas turbine engine with modified core system
03/21/2006	US7013633 External combustion thermal engine
03/16/2006	US20060053804 Gas turbine engine having improved core system
03/15/2006	CA2517772A1 High thrust gas turbine engine having improved core system
03/15/2006	CA2517182A1 Gas turbine engine having improved core system
03/07/2006	US7007455 Methods and apparatus for operating gas turbine engines
02/2006
02/21/2006	US7000402 Compound gas turbine engines and methods of operation thereof
02/01/2006	CN1727645A High efficiency stator for the first phase of a gas turbine
01/2006
01/26/2006	WO2006008353A1 Revolving toroidal motor
01/26/2006	US20060016170 Methods and apparatus for generating gas turbine engine thrust
01/10/2006	US6983604 Thermodynamic pressure generator
01/05/2006	DE102004029538A1 Aufladeeinrichtung für Verbrennungskraftmaschinen mit Pulse-Jet-Unterstützung Charger for internal combustion engines with pulse jet Support
01/04/2006	EP1611331A1 Low volumetric compression ratio integrated turbo-compound rotary engine
12/2005
12/22/2005	US20050279078 Multiple detonation initiator for frequency multiplied pulsed detonation combustion
12/22/2005	US20050279077 Off-axis pulse detonation configuration for gas turbine engine
12/08/2005	US20050269886 Alternators and improvements to rotary internal combustion engines
12/08/2005	DE102004058928A1 Drive motor for concentrated turbine, has free flight dual piston and drive block for hydrodynamically transferring basis energy to turbine with external teeth, and axle directly connected with motor and mutually containing air bag
12/07/2005	EP1601865A1 Compact compound engine package
12/07/2005	EP1601864A1 Integral cooling system for rotary engine
11/2005
11/17/2005	WO2005035963A3 Method and apparatus using jets to initiate detonations
11/15/2005	US6964171 Method and apparatus using jets to initiate detonations
11/03/2005	US20050241288 High efficiency rotor for the first phase of a gas turbine
11/03/2005	US20050241287 High efficiency stator for the first phase of a gas turbine
10/2005
10/27/2005	US20050235624 External combustion thermal engine
10/18/2005	US6955052 Thermal gas compression engine
10/13/2005	US20050223711 Closed-loop cooling system for a hydrogen/oxygen based combustor
10/12/2005	EP1584795A2 High efficiency stator for the first phase of a gas turbine
10/12/2005	EP1584787A2 High efficiency rotor for the first phase of a gas turbine
10/09/2005	CA2502796A1 High efficiency rotor for the first phase of a gas turbine
09/2005
09/29/2005	US20050210879 Pulse detonation engine system for driving turbine
09/21/2005	EP1577531A2 Gas turbine engine comprising a rotary pulse detonation system
09/18/2005	CA2500522A1 Rotary pulse detonation system with aerodynamic detonation passages for use in a gas turbine engine
09/15/2005	WO2005085614A1 Hydrogen motor
09/01/2005	US20050188675 Rotary engine
08/2005
08/31/2005	CN1662733A High efficiency gas turbine power generator systems
08/25/2005	US20050183413 Pulse detonation engine and valve
08/23/2005	US6931858 Rotating pulse detonation system for a gas turbine engine
08/23/2005	US6931833 Pulse combustion device
08/11/2005	US20050172631 Adiabatic power generating system
07/2005
07/27/2005	EP0961872B1 Micro-combustion chamber heat engine
07/27/2005	CN1644906A Pulse detonation power system and plant with fuel preconditioning
07/26/2005	US6920761 High efficiency low hydrocarbon emmisson hybrid power plant using operational aspects of both internal combustion and jet engines
07/21/2005	US20050155339 Rotary combustor, and electricity generator comprising such a combustor
07/14/2005	CA2550675A1 Thermal power plant with sequential combustion and reduced-co2 emission, and a method for operating a plant of this type
07/13/2005	EP1553682A2 Improvements to alternators and improvements to rotary combustion engines
07/13/2005	CN1637345A Rotary combustor, and electricity generator comprising such a combustor
07/07/2005	US20050144959 Scalable power generation using a pulsed detonation engine
06/2005
06/30/2005	DE10350259A1 Spiral engine, has combustion chambers in which fuel-air mixture is intermittently burnt so that energy, based on which helices of rotor are rotated, created is in form of pressure along with high velocity flow of gas
06/29/2005	EP1548365A2 Rotary combustor, and electricity generator comprising such a combustor
06/16/2005	US20050126755 Method and apparatus for improved flame stabilization
06/16/2005	US20050126177 Thermal gas compression engine
06/16/2005	US20050126155 Hydrogen motor
06/14/2005	US6904750 Integral pulse detonation system for a gas turbine engine
06/11/2005	CA2490759A1 Thermal gas compression engine

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