| Patents for F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants (30,889) |
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| 01/08/2009 | WO2009004062A1 Microturbine assembly |
| 01/08/2009 | WO2008138797A3 Pressure dynamics reduction within a gas turbine engine |
| 01/08/2009 | US20090007570 Methods and systems for cooling fluid in a turbine engine |
| 01/08/2009 | US20090007568 Emergency power engine restart system |
| 01/08/2009 | US20090007567 Dual Flow Turbine Engine Equipped with a Precooler |
| 01/08/2009 | US20090007566 NOx ADJUSTMENT METHOD FOR GAS TURBINE COMBUSTORS |
| 01/08/2009 | US20090007540 Pintle-controlled propulsion system with external dynamic seal |
| 01/08/2009 | DE102007030277A1 Turbolader für eine Brennkraftmaschine Turbocharger for an internal combustion engine |
| 01/07/2009 | EP2011988A2 Heat exchanger for a turbine engine |
| 01/07/2009 | EP2011987A2 Turbomachine with variable contour nacelle assembly and corresponding operating method |
| 01/07/2009 | EP2011979A2 Generator with separate Oil System |
| 01/07/2009 | EP2011978A1 Microturbine assembly |
| 01/07/2009 | EP2011967A1 Rotor shaft assembly and manufacturing method therefore |
| 01/07/2009 | EP2010429A1 Inlet distortion and recovery control system |
| 01/07/2009 | EP1917421B1 Compressor, compressor wheel, cleaning attachment and exhaust turbocharger |
| 01/07/2009 | EP1444428B1 Method and system for preventing surge events in a gas turbine engine |
| 01/07/2009 | EP1412618B1 Seal element for sealing a gap and combustion turbine having a seal element |
| 01/07/2009 | CN101338702A Pulse knock rotor spindle engine |
| 01/07/2009 | CN101338701A Methods and systems for cooling fluid in a turbine engine |
| 01/06/2009 | US7472542 Gas-turbine power generating installation and method of operating the same |
| 01/06/2009 | US7472541 Compressor control unit and gas turbine power plant including this unit |
| 01/06/2009 | CA2628519A1 Electric motor driven lubrication pump control system and method that accommodates turbomachine windmill operation |
| 01/04/2009 | CA2636661A1 Combustion chamber with heat protection deflectors for chamber floor and gas turbine engine so equipped |
| 01/02/2009 | DE102008022911A1 Steuerung der Turboladerschmierung für Hybridelektrofahrzeug Control of the turbocharger lubrication for hybrid electric vehicle |
| 01/02/2009 | DE102007030519A1 Gas turbine i.e. aircraft engine, module e.g. compressor module, has vane rings including outer diameter that is aligned with inner diameter of housing such that rotor together with vane rings is insertable into housing |
| 01/01/2009 | US20090003996 Labyrinth Seal in a Stationary Gas Turbine |
| 01/01/2009 | US20090003987 Airfoil with improved cooling slot arrangement |
| 01/01/2009 | US20090000306 Stator assembly including bleed ports for turbine engine compressor |
| 12/31/2008 | WO2009001415A1 Stator blade ring and axial flow compressor using the same |
| 12/31/2008 | WO2009000618A1 Nose dome for a turbomachine rotor |
| 12/31/2008 | WO2008135702A3 Method for producing an acoustically resistive structure, resulting acoustically resistive structure and skin using one such structure |
| 12/31/2008 | WO2008130725A3 Comb for inlet barrier filter system |
| 12/31/2008 | EP2009333A1 Dynamic brush seal |
| 12/31/2008 | EP2009290A1 Nose dome for a turbo machine rotor |
| 12/31/2008 | EP2009262A2 Gas turbine with multiple gas flow paths |
| 12/31/2008 | EP2009261A2 Engine accessory drive system for a gasturbine |
| 12/31/2008 | EP2009260A2 Cooling system for use on aircraft |
| 12/31/2008 | EP2009249A2 Control system of the axial bearing load of a gas turbine engine and corresponding method of regulating this load |
| 12/31/2008 | EP1509631B1 Thermal spray compositions for abradable seals |
| 12/31/2008 | EP1392957B1 Abradeable seal system |
| 12/31/2008 | EP1313932B1 Thermal barrier coating system |
| 12/31/2008 | EP1107867B1 Removal of thermal barrier coatings |
| 12/31/2008 | CN101335473A 发电机 Generator |
| 12/31/2008 | CN101333965A Microminiature turbine jet rotor swirling control method |
| 12/31/2008 | CN100447388C Jet motor or turbine motor |
| 12/31/2008 | CN100447374C Turbine vane and casting assemble for mfg. same |
| 12/30/2008 | US7470110 Turbine or compressor device and method for assembling the device |
| 12/30/2008 | US7469739 Apparatus and method for reducing operating stress in a turbine blade and the like |
| 12/30/2008 | US7469545 Auxiliary power unit inlet door position control system and method |
| 12/28/2008 | CA2635632A1 Dual turbofan |
| 12/26/2008 | CA2635633A1 Damping device adapted to turbine engine |
| 12/25/2008 | US20080315589 Energy Recovery System |
| 12/25/2008 | US20080314047 Cooling systems for use on aircraft |
| 12/25/2008 | US20080314044 Heat shields for use in combustors |
| 12/25/2008 | CA2634986A1 Assembly of shaft in bearing with auto-extraction nut |
| 12/25/2008 | CA2634967A1 Suspension of turbine engine on aircraft structure |
| 12/24/2008 | WO2008156890A2 Composite case armor for jet engine fan case containment |
| 12/24/2008 | EP2006512A2 Electric drive fuel control system for a gas turbine and method |
| 12/24/2008 | EP2006511A2 Turbine cooling air centrifugal particle separator |
| 12/24/2008 | EP2006496A1 Gas turbine engine start up method |
| 12/24/2008 | EP2006493A2 Aircraft combination engines thermal management system |
| 12/24/2008 | EP1861610B1 Method of operating a gas engine plant and fuel feeding system of a gas engine |
| 12/24/2008 | DE10393125B4 Kühlanordnung eines Übergangsstücks einer Gasturbine Cooling structure of a transition piece of a gas turbine |
| 12/24/2008 | DE102008002890A1 Wechselseitig gekühltes Turbinenleitrad Mutually-cooled turbine nozzle |
| 12/24/2008 | CN101328814A Reciprocal cooled turbine nozzle |
| 12/24/2008 | CN100445536C Fuel gas heating control equipment and gas turbine power generation facility provided with the fuel gas heating control equipment |
| 12/24/2008 | CN100445535C Improved high-temperature turbine nozzle with light decreasement by light reflection and manufactuirng process |
| 12/24/2008 | CN100445534C Improved high-temperature central body utilizing light reflection to reduce temperature and its manufacturing method |
| 12/23/2008 | US7467519 Electricity and synthesis gas generation method |
| 12/18/2008 | WO2008152259A2 Acoustic panel having a variable acoustic characteristic |
| 12/18/2008 | WO2008151441A1 Fuel nozzle providing shaped fuel spray |
| 12/18/2008 | US20080310950 Flow cavity arrangement |
| 12/18/2008 | US20080310949 Casing and Gas Turbine |
| 12/18/2008 | US20080308684 Nacelle with articulating leading edge slates |
| 12/18/2008 | US20080308345 Assembly for Reducing Noise in Turbofan Engines |
| 12/18/2008 | US20080307795 Exhaust casing hub comprising stress-distributing ribs |
| 12/18/2008 | US20080307769 Gas turbine engine anti-ice formation device and system |
| 12/18/2008 | DE102007027639A1 Heat exchanger for aircraft gas turbine, has pipe concentrically enclosed with radial distance by another pipe for transmission of fluid, and another pipe is provided for transmission of another fluid through ring channel |
| 12/18/2008 | CA2690431A1 Fuel nozzle providing shaped fuel spray |
| 12/18/2008 | CA2685287A1 Acoustic panel having a variable acoustic characteristic |
| 12/18/2008 | CA2635193A1 Turbine cooling air centrifugal particle separator |
| 12/17/2008 | EP2003312A1 Hub of an exhaust case comprising stress-distribution ribs |
| 12/17/2008 | EP2003311A2 Hybrid cooling of a gas turbine engine |
| 12/17/2008 | EP2003310A2 Variable geometry nacelle for an aircraft engine |
| 12/17/2008 | EP2003309A2 Variable geometry nacelle with nanoelectromechanical system for an aircraft engine and corresponding operating method |
| 12/17/2008 | EP2002087A1 Jet engine with detachably arranged generator unit |
| 12/17/2008 | EP1677888A4 System and method for thermal management |
| 12/17/2008 | EP0862493B1 Microcomponent chemical process sheet architecture |
| 12/17/2008 | CN201165904Y Gas turbine entrance air pre-filtration apparatus |
| 12/17/2008 | CN101324206A Cross flame holder for rotor engine |
| 12/17/2008 | CN101324205A Exhaust casing for a turbomachine |
| 12/17/2008 | CN101323077A Restrike nozzle body mechanical workout technique |
| 12/17/2008 | CN101323055A Restrike nozzle body welding process |
| 12/16/2008 | US7465148 Air-guiding system between compressor and turbine of a gas turbine engine |
| 12/16/2008 | US7464555 Catalytic combustor for integrated gasification combined cycle power plant |
| 12/16/2008 | US7464552 Acoustically stiffened gas-turbine fuel nozzle |
| 12/16/2008 | US7464532 Apparatus for elimination of transient pressure spikes on stiff fluid systems |
| 12/13/2008 | CA2634732A1 Exhaust casing hub having stress distribution ribs |
| 12/11/2008 | WO2008150213A1 A mounting element for a gas turbine engine, and a structure and an aircraft with such a mounting element |
| 12/11/2008 | WO2008150202A1 A structure for transferring loads at a gas turbine engine, and an engine and an aircraft with such a structure |