Patents
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)
10/2013
10/31/2013WO2013163604A1 Fuel injector with purged insulating air cavity
10/31/2013WO2013163049A1 Airfoil including loose damper
10/31/2013WO2013163048A1 Airfoil with powder damper
10/31/2013WO2013163047A1 Airfoil including damper member
10/31/2013WO2013163046A1 Airfoil having tapered buttress
10/31/2013WO2013163037A1 Gas turbine engine airfoil impingement cooling
10/31/2013WO2013163032A1 Gas turbine engine airfoil geometries and cores for manufacturing process
10/31/2013WO2013163029A1 Airfoil cooling enhancement and method of making the same
10/31/2013WO2013163020A1 Gas turbine engine core providing exterior airfoil portion
10/31/2013WO2013162946A1 Blade having porous, abradable element
10/31/2013WO2013162887A1 Airfoil with break-way, free-floating damper member
10/31/2013WO2013162866A1 Airfoil support method and apparatus
10/31/2013WO2013162752A1 Thermal management system for a gas turbine engine
10/31/2013WO2013162672A2 Gas turbine engine sump pressurization system
10/31/2013WO2013162665A2 Engine hot section vane with tapered flame holder surface
10/31/2013WO2013160625A1 Gas filter device provided with a means for attaching and removing the filtering elements for maintenance
10/31/2013WO2013160602A1 Turbine engine incorporating thermoelectric generators
10/31/2013WO2013160590A1 Method and system for the emergency start-up of an energy generator set
10/31/2013WO2010093512A3 System and method for operating power generation systems
10/31/2013US20130287575 Geared Architecture for High Speed and Small Volume Fan Drive Turbine
10/31/2013US20130287565 TEC Mount Redundant Fastening
10/31/2013US20130287549 Rotary machine and mounting method of atmosphere relief mechanism for rotary machine
10/31/2013US20130284398 Gas turbine engine thermal management system
10/31/2013US20130283852 Method and systems for co2 separation
10/31/2013US20130283818 Convolution seal for transition duct in turbine system
10/31/2013US20130283817 Flexible seal for transition duct in turbine system
10/31/2013US20130283816 Turboprop-powered aircraft
10/31/2013US20130283815 Integral cooling for servo valve
10/31/2013US20130283814 Turbine cooling system
10/31/2013US20130283812 Systems and methods for reconditioning turbine engines in power generation systems
10/31/2013US20130283811 Fuel circuit for an aviation turbine engine, the circuit having a fuel pressure regulator valve
10/31/2013US20130283809 Fuel injector with purged insulating air cavity
10/31/2013US20130283808 System and method for cooling a gas turbine with an exhaust gas provided by the gas turbine
10/31/2013US20130283804 Transition duct with late injection in turbine system
10/31/2013US20130283800 System for supplying fuel to a combustor
10/31/2013US20130283799 Resonance damper for damping acoustic oscillations from combustor
10/31/2013US20130283758 Oil Scoop Manifold
10/31/2013US20130283757 Mitigating vortex pumping effect upstream of oil seal
10/31/2013US20130283756 Manifold for gas turbine engine
10/31/2013DE19814442B4 Gasturbinen-Dichtungsvorrichtung Gas turbine sealing device
10/31/2013DE19811294B4 Gasturbinen-Dichtungssystem zwischen Schaufelumhüllung und -plattform Gas turbine sealing system between the blade enclosure and deck
10/31/2013DE102012207104A1 Abgasturbolader für eine Brennkraftmaschine Exhaust gas turbocharger for an internal combustion engine
10/31/2013DE102012207010A1 Exhaust gas turbocharger has lubricating oil collecting space that is provided between both floating bush bodies and stands in connection with lubricating oil supplying bore, from which radial bearing is guided from lubricating oil
10/31/2013CA2844741A1 Gas turbine engine sump pressurization system
10/30/2013EP2657483A2 System for supplying fuel to a combustor
10/30/2013EP2657482A1 Flow path structure and gas turbine exhaust diffuser
10/30/2013EP2657465A1 Mitigating Vortex Pumping Effect Upstream of Oil Seal
10/30/2013EP2657457A2 Electricity generation system
10/30/2013EP2657455A1 Heat shield and a method for construction thereof
10/30/2013EP2657134A2 A fuel supply of a motor of a rotorcraft, comprising means for initiating a suction pump for fuel from a distributor
10/30/2013EP2655834A1 Injection aperture for a steam power plant
10/30/2013EP2655833A1 Gas turbine engine flow path member
10/30/2013EP2655832A2 Method for operating a small gas turbine assembly and small gas turbine assembly
10/30/2013EP2655806A1 Filtering chamber and method for maintaining same
10/30/2013CN203257541U Combined heat and power compressed air energy storage system
10/30/2013CN103380279A Driveshaft for the gearbox of auxiliary machines of a turbojet engine
10/30/2013CN103375271A Apparatus relating to reheat combustion turbine engines with exhaust gas recirculation system
10/30/2013CN103375270A Fluid flow network for feeding fuel to a motor of a rotorcraft and method for operating the network
10/30/2013CN103375269A Metering valve
10/30/2013CN103375268A Micromixer assembly of a turbine system and method of assembly
10/30/2013CN103375267A 油勺歧管 Spoon oil manifold
10/30/2013CN103375266A Gas turbine inlet system and method
10/30/2013CN103375265A Turboshaft engine and use method thereof
10/30/2013CN103375264A Method of transition piece cross sectional area convergence reduction and selection
10/30/2013CN103375263A Systems and apparatuses for hot gas flow in a transition piece
10/30/2013CN103375262A Transition duct with late injection in turbine system
10/30/2013CN103375261A Convolution seal for transition duct in turbine system
10/30/2013CN103375260A Mica-based seals for gas turbine shroud retaining clip
10/30/2013CN103375255A Method and system for controlling a powerplant during low-load operations
10/30/2013CN103375247A Turbocharger for an internal combustion engine and method for operating a turbocharged internal combustion engine
10/30/2013CN103375201A System and method for reconditioning turbine engines in power generation systems
10/30/2013CN102287268B State transition valve and system
10/30/2013CN102042087B Systems and methods for bypassing inlet air treatment filter
10/30/2013CN102032003B Drain for exhaust gas duct
10/30/2013CN101558224B Device for improving effectiveness of acoustic treatments in aircraft drive duct
10/30/2013CN101311509B Methods and apparatus for operating gas turbine engines
10/29/2013US8567201 Ecology system for draining the manifold of a gas turbine engine
10/29/2013US8567197 Acoustic damper
10/29/2013US8567174 Valve assembly for draining oil, moisture, or water from a gas turbine engine
10/29/2013CA2625851C Gas turbine engine with power transfer and method
10/27/2013CA2813519A1 Separable seal assembly for a gas turbine engine
10/27/2013CA2813341A1 Mitigating vortex pumping effect upstream of oil seal
10/27/2013CA2813259A1 Oil scoop manifold
10/27/2013CA2813139A1 Wide discourager tooth
10/26/2013CA2813966A1 Thermally response controlled gap seal device
10/24/2013WO2013158536A1 Electronic means for detecting buffered main shaft seal wear or failure in a turbine engine
10/24/2013WO2013158192A2 Internally cooled spoke
10/24/2013WO2013158191A1 Geared turbofan gas turbine engine architecture
10/24/2013US20130280028 Thermal management system for a gas turbine engine
10/24/2013US20130277447 Method and system to control a fuel injector
10/24/2013US20130276459 Resistive band for turbomachine blade
10/24/2013US20130276454 Method of flange alignment
10/24/2013US20130276452 Gas turbine purge process
10/24/2013US20130276444 Turbine for an exhaust turbocharger of an internal combustion engine
10/24/2013US20130276423 Gas turbine
10/24/2013DE202013008843U1 Lagergehäuse eines Abgasturboladers An exhaust gas turbocharger bearing housing
10/24/2013DE102013103785A1 Korrosionsüberwachungsvorrichtung Corrosion monitoring device
10/24/2013DE102012206556A1 Lagereinheit für einen Turbolader Bearing unit for turbocharger
10/24/2013DE102012007832A1 Verfahren zum Betrieb einer Gasturbineneinheit A method of operating a gas turbine unit
10/24/2013CA2857351A1 Geared turbofan gas turbine engine architecture
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