F02K 5 - Plants including an engine, other than a gas turbine, driving a compressor or a ducted fan

Patents for F02K 5 - Plants including an engine, other than a gas turbine, driving a compressor or a ducted fan (170)
09/2008
09/03/2008	EP1965053A2 Combination engines for aircraft
08/2008
08/07/2008	WO2008070210A9 Pilot fuel injection for a wave rotor engine
07/2008
07/30/2008	EP1664505A4 Gas turbine engine system
06/2008
06/26/2008	WO2008076688A2 Two-piece aft closure for a rocket motor case
06/25/2008	CN101208509A Turbo rocket with real Carnot cycle
06/19/2008	US20080143058 Two-piece aft closure for a rocket motor case
06/12/2008	WO2008070210A2 Pilot fuel injection for a wave rotor engine
04/2008
04/17/2008	DE19600679B4 Schubtriebwerk für Flugzeuge mit Verbundzyklus Thrust engine for aircraft with composite cycle
03/2008
03/27/2008	US20080072572 Turbomachine fan duct
03/06/2008	WO2001009063A3 Premixed liquid monopropellant solutions and mixtures
02/2008
02/12/2008	US7328570 Pulse detonation system for a gas turbine engine having multiple spools
09/2007
09/05/2007	CN101029596A Methods and systems for partial moderator bypass
08/2007
08/08/2007	CN101014495A Air jetting propeller
07/2007
07/19/2007	WO2005012714A3 Turbo rocket with real carnot cycle
07/11/2007	EP1806286A1 Air-jet propeller
06/2007
06/14/2007	DE102005060516A1 Fahrzeug und Verfahren zum Betrieb eines Fahrzeugs Vehicle and method for operating a vehicle
04/2007
04/10/2007	US7200987 Off-axis pulse detonation configuration for gas turbine engine
03/2007
03/08/2007	US20070051087 Gas turbine engine system
02/2007
02/27/2007	US7182290 Methods and systems for starting propeller-driven devices
11/2006
11/21/2006	US7137243 Constant volume combustor
08/2006
08/09/2006	EP1687200A2 Methods and systems for starting propeller-driven devices
06/2006
06/29/2006	WO2005042342A3 Methods and systems for starting propeller-driven devices
06/07/2006	EP1664505A2 Gas turbine engine system
06/06/2006	US7055308 Detonation damper for pulse detonation engines
05/2006
05/18/2006	US20060101800 Gas turbine engine system
05/04/2006	CA2570542A1 Air-jet propeller
03/2006
03/02/2006	US20060042228 Pulse detonation system for a gas turbine engine having multiple spools
02/2006
02/16/2006	WO2005021949A3 Gas turbine engine system
12/2005
12/29/2005	US20050284127 Detonation engine and flying object provided therewith
12/22/2005	US20050279077 Off-axis pulse detonation configuration for gas turbine engine
07/2005
07/19/2005	US6918243 Bi-propellant injector with flame-holding zone igniter
05/2005
05/12/2005	WO2005042342A2 Methods and systems for starting propeller-driven devices
05/05/2005	US20050093507 Methods and systems for starting propeller-driven devices
03/2005
03/10/2005	WO2005021949A2 Gas turbine engine system
12/2004
12/29/2004	EP1490587A1 Gas turbine engine system
11/2004
11/25/2004	US20040231318 Bi-propellant injector with flame-holding zone igniter
09/2004
09/07/2004	US6786036 Bimodal fan, heat exchanger and bypass air supercharging for piston or rotary driven turbine
06/2004
06/22/2004	US6751946 Ducted fan integrated power plant unit having propeller with central blade wheel
10/2003
10/28/2003	US6637187 Rotary inlet flow controller for pulse detonation combustion engines
10/23/2003	US20030196426 Ducted fan integrated power plant unit having propeller with central blade wheel
09/2003
09/18/2003	WO2003076779A1 Gas turbine engine system
09/18/2003	CA2479235A1 Gas turbine engine system
08/2003
08/21/2003	US20030154707 Rotary inlet flow controller for pulse detonation combustion engines
07/2003
07/24/2003	US20030136112 Central turbo ducted fan integrated power plant unit
12/2002
12/31/2002	US6499286 Method for the operation of a supersonic jet-engine combined power unit
11/2002
11/21/2002	DE10124056A1 Internal combustion engine without crankshaft, consists of casing, turbine-flywheel, pushrod, springs, pistons and cylinders
11/07/2002	US20020162318 Bimodal fan, heat exchanger and bypass air supercharging for piston or rotary driven turbine
10/2002
10/17/2002	DE10115766A1 Thrust generator, for a glider or jet models, has a drive motor within the inner zone of the housing to be coupled to the turbine compressor, in a simple structure which can be controlled easily
10/09/2002	CN1092288C Method for operation of supersonic jet-engine combined power unit
12/1999
12/22/1999	CN1239534A Method for operation of supersonic jet-engine combined power unit
03/1999
03/31/1999	CN1212324A Combined jet engine
11/1998
11/05/1998	WO1998014367A3 Method for the operation of a supersonic jet-engine combined power unit
09/1998
09/02/1998	EP0754142B1 Integrated power and cooling environmental control system
04/1998
04/09/1998	WO1998014367A2 Method for the operation of a supersonic jet-engine combined power unit
02/1998
02/16/1998	CA2183378A1 Turbine booster
09/1997
09/16/1997	US5666803 Vectored thrust compressor for remote controlled aircraft
01/1997
01/22/1997	EP0754142A1 Integrated power and cooling environmental control system
03/1996
03/12/1996	USRE35172 Pulsed piston-compressor jet engine
12/1995
12/05/1995	US5471834 Engine driven propulsion fan with turbochargers in series
10/1995
10/19/1995	WO1995027655A1 Integrated power and cooling environmental control system
10/19/1995	CA2185924A1 Integrated power and cooling environmental control system
08/1995
08/22/1995	US5442905 Integrated power and cooling environmental control system
11/1994
11/08/1994	US5361581 Pulsed piston-compressor jet engine
05/1994
05/11/1994	DE4237910A1 Jet engine burning alternative fuels - has IC engine to drive compressor feeding high pressure ambient air into combustion tube
03/1991
03/05/1991	US4996839 For aircraft
11/1990
11/15/1990	DE4021576A1 Jet engine for aircraft propulsion - has free piston air compressors arranged around combustion chamber and thrust nozzle
03/1989
03/28/1989	US4815282 Turbocharged compund cycle ducted fan engine system
05/1988
05/25/1988	CN86107822A Differential pressure thruster
08/1987
08/11/1987	US4685289 Power plant for model jet aircraft
12/1985
12/10/1985	US4557107 Power plant for model jet aircraft

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