Patents
Patents for F02K 99 - Subject matter not provided for in other groups of this subclass (464)
03/2012
03/06/2012US8127527 Methods and systems for operating oxidizer systems
03/01/2012US20120048389 Aircraft nacelle including an optimised acoustic processing system
01/2012
01/24/2012CA2467842C Nozzle flap for aircraft turbojets
01/04/2012CN102308078A A microsatellite comprising a propulsion module and an imaging device
12/2011
12/22/2011US20110308634 Turbojet nacelle having a removable air intake structure
12/22/2011US20110308231 System, method and apparatus for cooling rocket motor components using a saturated liquid vapor coolant mixture
12/15/2011US20110303298 Method for closing a mobile cradle element
12/06/2011US8069646 Gas turbine system having an air intake bypass system and an air discharge bypass system
12/01/2011US20110290333 Method for manufacturing a structure with cellular cores for a turbojet nacelle
11/2011
11/24/2011WO2011144210A2 Heating and cleaning apparatus for surface treatment
10/2011
10/12/2011EP2373878A1 A microsatellite comprising a propulsion module and an imaging device
10/05/2011EP2372697A1 Method of retrofitting an acoustic treatment into a fluid handling module
09/2011
09/15/2011US20110220217 Air inlet of an aeroengine having unducted pusher propellers
09/13/2011US8015795 Aircraft combination engines plural airflow conveyances system
09/07/2011CN101389849B Rotary heat engine
08/2011
08/31/2011EP2361350A1 Magnetic advanced generation jet electric turbine
08/23/2011US8001764 Vibration isolation engine mount system and method for ducted fans
08/18/2011US20110197973 Inlet section of an aircraft engine nacelle
08/16/2011US7997062 Dual channel regulated fuel-oil heat exchanger
07/2011
07/28/2011US20110179766 Heat recovery system
07/26/2011US7984606 Systems and methods for thermal management in a gas turbine powerplant
07/21/2011WO2010068174A8 A microsatellite comprising a propulsion module and an imaging device
07/21/2011US20110173947 System and method for gas turbine power augmentation
07/14/2011US20110171006 Turbine engine bypass fan-bleed noise reduction
06/2011
06/15/2011EP2062059B1 Measuring arrangement for detecting a rotary momentum of an engine rotor, and associated method
06/14/2011CA2463180C Process for replacing an abradable on the fan case of a turbojet
06/07/2011US7955568 Chemical reaction-based thermal management system and method
03/2011
03/08/2011US7900438 Heat transfer system and method for turbine engine using heat pipes
03/08/2011US7900437 Heat transfer system and method for turbine engine using heat pipes
03/01/2011US7895823 Heat exchanger for a rocket engine
02/2011
02/15/2011US7886520 Gas turbine engine
02/10/2011DE102004007632B4 Katalysatorlaserantrieb mit Hochfrequenzresonanzanlage Catalyst laser driver with high frequency resonant system
01/2011
01/13/2011US20110005192 Cooling system for an aircraft, aircraft comprising the cooling system and cooling method
01/04/2011US7862293 Low profile bleed air cooler
12/2010
12/30/2010US20100326049 Cooling systems for rotorcraft engines
12/30/2010US20100326043 Expander cycle rocket engine nozzle
12/07/2010US7845159 Heat pipe-based cooling apparatus and method for turbine engine
12/02/2010US20100300066 Turbojet engine for aircraft
12/02/2010US20100300065 Closed-cycle rocket engine assemblies and methods of operating such rocket engine assemblies
11/2010
11/04/2010US20100276007 Cambered aero-engine inlet
11/04/2010US20100275578 Cooling exchanger duct
11/04/2010US20100275577 Rocket engine injectorhead with flashback barrier
10/2010
10/21/2010US20100263350 Apparatus and method for cooling a turbine using heat pipes
10/14/2010US20100258199 Intake cone in a fiber compound material for a gas-turbine engine
10/14/2010US20100257839 Hydrocarbon-fueled rocket engine with endothermic fuel cooling
10/12/2010US7810312 Heat exchanger arrangement
10/12/2010US7810311 Cooling exchanger ducts
09/2010
09/23/2010US20100237200 Turbojet engine for aircraft, propulsion unit comprising such a turbojet engine and aircraft comprising such a propulsion unit
09/23/2010US20100236217 Heat transfer system and method for turbine engine using heat pipes
08/2010
08/26/2010WO2010096087A1 Magnetic advanced generation jet electric turbine
08/03/2010US7765788 Cooling exchanger duct
07/2010
07/27/2010US7762056 Aircraft combination engines exhaust thrust recovery
07/22/2010US20100180570 Reactionless Motion (RM)
07/20/2010US7757477 Convergent divergent nozzle with slot cooled nozzle liner
07/13/2010US7752847 Liquid injection in a gas turbine during a cooling down phase
07/01/2010US20100162685 A method for cooling air and devices
06/2010
06/24/2010DE102008062088A1 Vorrichtung und Verfahren zur Energie-Rückgewinnung in Flugzeugtriebwerken beim Landeanflug. Apparatus and method for energy recovery in aircraft engines during the landing approach.
06/17/2010WO2010068174A1 A microsatellite comprising a propulsion module and an imaging device
05/2010
05/18/2010US7716913 Engine
05/13/2010US20100115947 Rotary heat engine powered by radiant energy
05/04/2010US7708522 Rotary heat engine
04/2010
04/06/2010US7690189 Aircraft combination engines inlet airflow control system
04/06/2010US7690188 Combination engines for aircraft
02/2010
02/25/2010US20100043396 Gas turbine engine fan bleed heat exchanger system
02/25/2010US20100043389 Low shock strength propulsion system
02/16/2010US7661723 Fluid line assembly
02/02/2010US7654087 Compact compound engine package
01/2010
01/07/2010US20100000200 Impingement cooling device
01/06/2010EP2141400A1 Fluid line assembly
12/2009
12/17/2009US20090308051 Heat exchanger tube and air-to-air intercooler
12/10/2009US20090301057 Turboreactor for aircraft
12/03/2009US20090293448 Simplified thrust chamber recirculating cooling system
11/2009
11/26/2009US20090288390 Simplified thrust chamber recirculating cooling system
10/2009
10/20/2009US7603843 Combustion chamber comprising a cooling unit and method for producing said combustion chamber
10/15/2009US20090256556 Measuring arrangement for detecting a 1/rotary momentum of an engine rotor, and associated method
09/2009
09/11/2009WO2006011978A3 Propulsion device with enclosed plenum
08/2009
08/20/2009US20090205314 Combustion Chamber Wall
08/18/2009US7575014 Control of engine intake door
07/2009
07/02/2009US20090165437 Drive device on the basis of a gel-type propellant and method for conveying propellant
05/2009
05/28/2009US20090134621 Fluid line assembly
05/27/2009EP2062059A2 Measuring arrangement for detecting a 1/ rotary momentum of an engine rotor, and associated method
05/14/2009US20090120056 Microthruster, in particular for use as a position adjustment thruster, thruster and method for producing a microthruster
05/06/2009CN101427018A Propulsion device with enclosed plenum
04/2009
04/09/2009WO2007035124A8 Plasma vehicle engine
03/2009
03/19/2009US20090072044 Convergent Divergent Nozzle With Slot Cooled Nozzle Liner
03/18/2009CN101389849A Rotary heat engine
03/17/2009US7503590 Fluid line assembly
01/2009
01/29/2009US20090025366 Propulsion unit for aircraft and aircraft comprising at least one such propulsion unit
12/2008
12/16/2008US7464537 Heat transfer enhancement features for a tubular wall combustion chamber
12/02/2008US7458201 Propulsion device with enclosed plenum
11/2008
11/12/2008EP1718857A4 Integrated air inlet system for multi-propulsion aircraft engines
11/06/2008US20080271433 Low profile bleed air cooler
11/03/2008CA2630249A1 Low profile bleed air cooler
10/2008
10/30/2008US20080265197 Gate valve for a system for circulating cooling air through a turbomachine
10/30/2008US20080264035 Coolant flow swirler for a rocket engine
10/29/2008EP1985834A1 Flap valve for a cooling system in a turbojet
10/27/2008CA2629798A1 Check valve for a cooling system in a turbine engine
10/22/2008EP1982067A2 Rotary heat engine
10/09/2008US20080245054 Cooling System for an Aircraft, Aircraft Comprising the Cooling System and Cooling Method
10/07/2008US7431126 Support means for an acoustic liner used in an auxiliary power unit exhaust muffler
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