| 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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| 05/28/2013 | US8448445 Method for the start-up of a gas turbine |
| 05/28/2013 | US8448418 Method for controlling a flowrate of a recirculated exhaust gas |
| 05/28/2013 | CA2770728A1 Support for electric machine in a turbine engine |
| 05/28/2013 | CA2554264C Reversible driving apparatus for pcu pumps |
| 05/23/2013 | WO2013073549A1 Gas turbine combustor |
| 05/23/2013 | WO2013072291A1 Device and method for slow turning of an aeroderivative gas turbine |
| 05/23/2013 | US20130125560 Lateral turbojet improved in order to limit the deformation thereof |
| 05/23/2013 | US20130125559 Gas turbine engine comprising a tension stud |
| 05/23/2013 | US20130125558 Preheating a spark plug |
| 05/23/2013 | US20130125556 Fuel-air mixture distribution for gas turbine engine combustors |
| 05/23/2013 | US20130125549 Gas turbine combustor endcover with adjustable flow restrictor and related method |
| 05/23/2013 | DE102012221166A1 Turbolader-Ölzufuhrsystem Turbocharger oil supply system |
| 05/23/2013 | DE102011118735A1 Diffusor, insbesondere für eine axiale strömungsmaschine Diffuser, in particular for an axial fluid machine |
| 05/23/2013 | CA2854423A1 Device and method for slow turning of an aeroderivative gas turbine |
| 05/23/2013 | CA2794888A1 Gas turbine engine architecture with low pressure compressor hub between high and low rotor thrust bearings |
| 05/22/2013 | EP2594776A1 Integrated accessory gearbox and engine starter |
| 05/22/2013 | EP2594766A1 Integrated permanent magnet alternator and cooling fan |
| 05/22/2013 | EP2594765A2 Compressor having a cooling circuit and corresponding cooling method |
| 05/22/2013 | EP2594746A1 Gas turbine power plant with a gas turbine assembly and method for operating a gas turbine power plant |
| 05/22/2013 | EP2593648A2 A solution for controlling a turbo compressor |
| 05/22/2013 | EP2593647A2 Generating power using an ion transport membrane |
| 05/22/2013 | CN202946246U Fuel switching device |
| 05/22/2013 | CN202946245U Centrifugal micro gas turbine arrayed in cross |
| 05/22/2013 | CN103119267A Oil supply system for a stationary turbomachine |
| 05/22/2013 | CN103119255A Architecture for a non-lubricated turboshaft engine |
| 05/22/2013 | CN103114913A Method for cooling gas turbine inlet gas by indirect evaporation |
| 05/22/2013 | CN101818690B Gas turbine combustion system cooling arrangement |
| 05/22/2013 | CN101737167B Methods, apparatus and systems concerning the circumferential clocking of turbine airfoils and the flow of cooling air |
| 05/21/2013 | US8443612 Engine mounting arrangement |
| 05/21/2013 | US8443609 Gas-turbine burner for a gas turbine with purging mechanism for a fuel nozzle |
| 05/21/2013 | US8443607 Coaxial fuel and air premixer for a gas turbine combustor |
| 05/21/2013 | US8443582 Gas turbine engine with geared turbofan and oil thermal management system |
| 05/21/2013 | CA2544458C Hybrid vane island diffuser |
| 05/21/2013 | CA2513054C Multi-point seal |
| 05/16/2013 | WO2013069775A1 Seal assembly and gas turbine provided therewith |
| 05/16/2013 | WO2013069724A1 Film cooling structure and turbine wing |
| 05/16/2013 | WO2013069694A1 Impingement cooling mechanism, turbine blade, and combustor |
| 05/16/2013 | WO2013069637A1 Combustor liner |
| 05/16/2013 | WO2013069111A1 Gas turbine electricity generation device and operating method therefor |
| 05/16/2013 | WO2013068607A1 Solar collector including a solar turbine or a turbocompressor |
| 05/16/2013 | US20130119613 Leaf seal |
| 05/16/2013 | US20130119612 Leaf seal |
| 05/16/2013 | US20130118594 Low shock strength inlet |
| 05/16/2013 | US20130118183 Optical sensor system for a gas turbine engine and method of operating the same |
| 05/16/2013 | US20130118181 Procedure for igniting a turbine engine combustion chamber |
| 05/16/2013 | US20130118177 Fuel injection system for turbojet engine and method of assembling such an injection system |
| 05/16/2013 | US20130118145 Hybrid fossil fuel and solar heated supercritical carbon dioxide power generating system and method |
| 05/16/2013 | DE102011086310A1 Abgasturbolader mit einer variablen Turbinengeometrie und einer Tellerfeder zur Abdichtung Exhaust gas turbocharger with a variable turbine geometry and a disc spring for sealing |
| 05/16/2013 | CA2854708A1 Combustor liner |
| 05/15/2013 | EP2592252A2 Gearbox deoiler with pre-pressuring component |
| 05/15/2013 | EP2592251A2 Bleed system for heating the compressor inlet air |
| 05/15/2013 | EP2592250A2 System for purging gas fuel circuit for a gas turbine engine |
| 05/15/2013 | EP2592236A2 Bleed system for heating the inlet air of a compressor |
| 05/15/2013 | EP2592228A1 Turbine blade and engine component |
| 05/15/2013 | EP2592226A2 Turbomachine component and method of connecting cooling circuits of a turbomacine component |
| 05/15/2013 | EP2591220A2 Heat-exchange architecture built into the exhaust of a turbine engine |
| 05/15/2013 | CN202937353U High-pressure air starting device of aero-engine |
| 05/15/2013 | CN103109078A Electrical arrangement of hybrid ignition device |
| 05/15/2013 | CN103109059A Gas turbine and gas turbine plant provided with same |
| 05/15/2013 | CN103109045A 燃气涡轮 Gas Turbine |
| 05/15/2013 | CN103108805A Method for optimizing the overall energy efficiency of an aircraft, and main power package for implementing same |
| 05/15/2013 | CN103104349A Flexible metallic seal for transition duct in turbine system |
| 05/15/2013 | CN103104348A Convolution seal for transition duct in turbine system |
| 05/15/2013 | CN103104347A High energy solid state discharge igniting module |
| 05/15/2013 | CN103104346A Clack valve assembly and assembling method thereof, fuel system and airport having the same |
| 05/15/2013 | CN103104345A System for purging gas fuel circuit for a gas turbine engine |
| 05/15/2013 | CN103104344A System for cooling fluid flow within an engine |
| 05/15/2013 | CN103104343A Leaf seal for transition duct in turbine system |
| 05/15/2013 | CN103100266A Design and shape for pulse cartridges |
| 05/14/2013 | US8439637 Bellows preload and centering spring for a fan drive gear system |
| 05/14/2013 | US8438874 Natural gas liquefaction plant and motive power supply equipment for same |
| 05/14/2013 | US8438859 Integrated bypass engine structure |
| 05/14/2013 | US8438850 Waste heat utilization for pre-heating fuel |
| 05/14/2013 | US8438831 Piezo-resonance igniter and ignition method for propellant liquid rocket engine |
| 05/14/2013 | US8438828 Flow divider having breaking points for a fan engine |
| 05/14/2013 | CA2694573C Turbine rotor blade repair method |
| 05/14/2013 | CA2688099C Centrifugal compressor forward thrust and turbine cooling apparatus |
| 05/14/2013 | CA2516717C Integral cooling system for rotary engine |
| 05/14/2013 | CA2513079C Lightweight annular interturbine duct |
| 05/10/2013 | WO2013067361A1 Tie-rod nut including a nut flange with a plurality of mounting apertures |
| 05/10/2013 | WO2013067149A1 Power generating system and corresponding method |
| 05/10/2013 | WO2013065624A1 Gas turbine system |
| 05/10/2013 | CA2854402A1 Power generating system and corresponding method |
| 05/10/2013 | CA2854079A1 Gas turbine system |
| 05/09/2013 | US20130115049 Assembly comprising a shaft seal |
| 05/09/2013 | US20130111924 Flexible printed circuit board harness |
| 05/09/2013 | US20130111923 Gas turbine engine component axis configurations |
| 05/09/2013 | US20130111919 Gas turbine engine with structure for directing compressed air on a blade ring |
| 05/09/2013 | US20130111918 Combustor assembly for a gas turbomachine |
| 05/09/2013 | US20130111917 Apparatus for aircraft with high peak power equipment |
| 05/09/2013 | US20130111916 System for operating a power plant |
| 05/09/2013 | US20130111914 Aircraft ignition system and method of operating the same |
| 05/09/2013 | US20130111913 Multi-combustor turbine |
| 05/09/2013 | US20130111859 Design and shape for pulse cartridges to allow hydrophobic media to drain and generally increase working surface area |
| 05/08/2013 | EP2589778A2 System for operating a power plant |
| 05/08/2013 | EP2589777A2 Gas turbine engine with intercooling turbine section |
| 05/08/2013 | EP2589776A2 Gas turbine engine comprising a flexible printed circuit board harness |
| 05/08/2013 | EP2589775A2 Flexible printed circuit board harness |
| 05/08/2013 | EP2589774A1 Shroud segment producing method and shroud segment |
| 05/08/2013 | EP2588794A1 Compensator for connecting pipes for dust-laden flue gas |