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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04/25/2013 | US20130098039 Exhaust diffuser adjustment system for a gas turbine engine |
04/25/2013 | US20130098002 Exhaust gas treatment device, method for producing a tube for an exhaust gas treatment device and watercraft having an exhaust gas treatment device |
04/25/2013 | US20130097996 Ram air fan inlet housing |
04/25/2013 | US20130097992 Integrated thermal management system and environmental control system for a gas turbine engine |
04/25/2013 | US20130097991 System for turbine combustor fuel mixing |
04/25/2013 | US20130097990 Rotary oil degradation byproducts removal system |
04/25/2013 | DE102011085105A1 Rotor shaft of a turbomachine, includes two shaft sections, where first shaft section comprises hollow plug receptacle, and second shaft section comprises plug-in projection for intervening the plug receptacle of the first shaft section |
04/25/2013 | DE102011085037A1 Ramjet engine for aircraft, has adjustment device which is arranged for varying the geometry of the suction channel arranged between diffuser element and ramp |
04/25/2013 | DE10163649B4 Turboverdichter und Gasturbine mit Einlaufschwingungswarnung bei Axialschwingung der Luftsäule im Einlauf sowie Auswerteverfahren hierfür Turbo compressor and gas turbine inlet vibration warning axial vibration of the air column in the inlet and evaluation of this |
04/24/2013 | EP2584173A1 Gas Turbine Engine |
04/24/2013 | EP2584172A2 Constant speed transmission for gas turbine engine |
04/24/2013 | EP2584171A2 Split accessory drive system |
04/24/2013 | EP2584170A2 Compartment cooling for a gas turbine engine |
04/24/2013 | EP2584169A2 Integrated thermal management system and environment control system for a gas turbine engine |
04/24/2013 | EP2584168A2 Integrated thermal system for a gas turbine engine |
04/24/2013 | EP2583032A1 Damping device for damping pressure oscillations within a combustion chamber of a turbine |
04/24/2013 | EP2582923A1 Architecture for a non-lubricated turboshaft engine |
04/24/2013 | EP2582922A1 Guiding and sealing device for a turbine engine, having a carbon seal and built-in journal bearing |
04/24/2013 | EP2582921A2 Noise-reduced turbomachine |
04/24/2013 | EP2582580A1 Airflow-straightening structure for the nacelle of an aircraft engine |
04/24/2013 | CN202900419U Fuel supply device capable of flexibly mixing and changing fuels of internal combustion turbine |
04/24/2013 | CN202900418U Fuel stable-combustion high-pressure air way system applied to gas turbine |
04/24/2013 | CN202900417U 断油装置 Off oil installations |
04/24/2013 | CN202900416U Jet-flow high-efficiency thermal power system |
04/24/2013 | CN103069219A Secondary water injection for diffusion combustion systems |
04/24/2013 | CN103069132A Integral plus proportional dual pump switching system |
04/24/2013 | CN103069131A Gas turbine system, control device for gas turbine system, and control method for gas turbine system |
04/24/2013 | CN103069113A Multi-piece turbocharger casing |
04/24/2013 | CN103069028A Co-based alloy |
04/24/2013 | CN103061918A Gas turbine engine assembly and method of assembling same |
04/24/2013 | CN103061890A Starting control system of engine |
04/24/2013 | CN103061889A Thermal insulating structure |
04/24/2013 | CN103061888A Wet compression method for small and medium size turbine |
04/24/2013 | CN103061887A Intercooling gas turbine |
04/24/2013 | CN103061886A System and method for heating inlet air of gas turbine |
04/24/2013 | CN103061824A Method and system for use in regulating temperature of component |
04/24/2013 | CN103056604A Components with laser cladding and methods of manufacture |
04/24/2013 | CN101909998B Aircraft nacelle guidance system installation |
04/24/2013 | CN101688474B Integrated gasification combined generation plant |
04/24/2013 | CN101676536B Elastic mounting flange used for combustion gas turbine engine |
04/24/2013 | CN101556045B Cooling apparatus for combustor transition piece |
04/24/2013 | CN101344036B Turbo engine |
04/23/2013 | US8424285 Cooling system for electronic device in a gas turbine engine system |
04/23/2013 | CA2678324C Bearing suppport flexible ring |
04/23/2013 | CA2597272C Optimized internal manifold heat shield attachment |
04/23/2013 | CA2529530C Method and apparatus for balancing gas turbine engines |
04/19/2013 | DE202013101510U1 Flüssigkeitsgekühlte Turbine Liquid-cooled turbine |
04/18/2013 | WO2013054798A1 Ceramic matrix composite member and method for producing same |
04/18/2013 | WO2011124322A3 Power plant line having a variable-speed pump |
04/18/2013 | US20130094951 Mid turbine frame (mtf) for a gas turbine engine |
04/18/2013 | US20130091864 Quick disengaging field joint for exhaust system components of gas turbine engines |
04/18/2013 | US20130091863 Planet gear for air turbine starter system |
04/18/2013 | US20130091861 Turbine |
04/18/2013 | US20130091858 Effusion cooled nozzle and related method |
04/18/2013 | US20130091851 Method and a device for producing a setpoint signal |
04/18/2013 | US20130091850 Method and system for reducing hot soakback |
04/18/2013 | US20130091845 Power plant and method for retrofit |
04/18/2013 | US20130091824 Gas turbine and gas-turbine plant having the same |
04/18/2013 | DE102010024291B4 Gleitringdichtung mit rotierendem Gegenring mit exakt definierter Einspannung Mechanical seal with rotating seal ring with a precisely defined clamping |
04/17/2013 | EP2581916A1 Ignition cable for high mechanical and/or thermal loads |
04/17/2013 | EP2581586A2 Starting an aircraft engine of a multi-engine system |
04/17/2013 | EP2581585A2 Fluid separator |
04/17/2013 | EP2581584A1 Compressed air energy storage system and method for operating this system |
04/17/2013 | EP2581565A2 A System for use in Controlling the Operation of Power Generation Systems |
04/17/2013 | EP2581564A2 A Control System and Methods for Controlling the Operation of Power Generation Systems |
04/17/2013 | EP2581554A2 System for cooling fluid flow within an engine |
04/17/2013 | EP2580448A2 Gas turbine and method for operating said gas turbine |
04/17/2013 | EP2580447A1 Cooling system for controlling cooling of rotor cooling air and heating of fuel gas |
04/17/2013 | CN202883124U Automatic constant temperature control device of combustible gas supply system |
04/17/2013 | CN202883122U Solar, gas turbine and stored energy unitized cogeneration device with adjustable power |
04/17/2013 | CN202883121U Industrial combustible gas generating system |
04/17/2013 | CN103047372A Planet gear for air turbine starter system |
04/17/2013 | CN103047044A Low temperature cold source heat engine |
04/17/2013 | CN103047016A Power plant and method for retrofit |
04/17/2013 | CN103047015A System for sealing a shaft |
04/17/2013 | CN103047014A Heat insulation plate structure |
04/17/2013 | CN103047013A Laminate thermal insulation blanket for aircraft applications and process therefor |
04/17/2013 | CN103047012A Ejection intercooling gas turbine |
04/17/2013 | CN103047011A System and method for heating inlet gas of gas turbine |
04/17/2013 | CN103047010A Anti-icing system and anti-icing control method of inlet lip of engine |
04/17/2013 | CN103046975A Exhaust gas diffuser |
04/17/2013 | CA2792159A1 Power plant and method for retrofit |
04/16/2013 | US8418475 Attachment structure of combustion oscillation detecting device |
04/16/2013 | US8418474 Altering a natural frequency of a gas turbine transition duct |
04/16/2013 | US8418473 Pivoting liner hanger |
04/11/2013 | WO2010142573A3 Method and device for the recirculation of exhaust gases in a gas turbine |
04/11/2013 | US20130089409 Non-lubricated architecture for a turboshaft engine |
04/11/2013 | US20130087413 Dynamically-lubricated bearing and method of dynamically lubricating a bearing |
04/11/2013 | US20130087412 Dynamically-lubricated bearing and method of dynamically lubricating a bearing |
04/11/2013 | US20130086921 Combustor and method for supplying flow to a combustor |
04/11/2013 | US20130086920 Combustor and method for supplying flow to a combustor |
04/11/2013 | US20130086919 Starting of aircraft engine |
04/11/2013 | US20130086916 Low Emission Power Generation Systems and Methods |
04/11/2013 | US20130086915 Film cooled combustion liner assembly |
04/11/2013 | US20130086914 Turbine system |
04/11/2013 | US20130086913 Turbomachine combustor assembly including a combustion dynamics mitigation system |
04/11/2013 | US20130086912 System for cooling a multi-tube fuel nozzle |
04/11/2013 | US20130086911 Process and apparatus for overlay welding |
04/11/2013 | US20130086909 Oil cooling system |
04/11/2013 | US20130086907 Jet flow nozzle and jet engine |