| 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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| 12/20/2012 | WO2012174240A1 Aircraft powerplant |
| 12/20/2012 | WO2012173651A1 Aircraft engine fuel system and method of operating the same |
| 12/20/2012 | WO2012173236A1 Member covered with hard coating film |
| 12/20/2012 | WO2012171094A1 Combustion systems and combustion system components for rotary ramjet engines |
| 12/20/2012 | WO2012103112A3 Em energy application for combustion engines |
| 12/20/2012 | US20120321459 Support structure forming method |
| 12/20/2012 | US20120321451 Bearing Housing Cooling System |
| 12/20/2012 | US20120317990 Systems and methods for detecting combustor casing flame holding in a gas turbine engine |
| 12/20/2012 | US20120317989 Systems and methods for combustor emissions control |
| 12/20/2012 | US20120317986 Method for operating a combustion device and combustion device for implementing the method |
| 12/20/2012 | DE10350627B4 Turbinenrotor- und Schaufelanordnung, Vorspannfedersegment und zugehöriges Verfahren für Dampfturbinenschaufeln der Reaktionsbauart Turbine rotor and blade assembly, biasing spring segment and associated method for steam turbine blades of reaction type |
| 12/20/2012 | DE102012105188A1 Speiseinjektor für ein Vergasungssystem Speiseinjektor for a gasification system |
| 12/20/2012 | DE102012011294A1 Method for cooling gas turbine plant, involves sucking input side inlet air by compressor of gas turbine plant, where compressor compresses inlet air to output side compressor end air |
| 12/20/2012 | DE102009057100B4 Wartungsfreies Aggregat für die Kraftwärmekopplung Maintenance-free unit for combined heat and power |
| 12/20/2012 | CA2839456A1 Combustion systems and combustion system components for rotary ramjet engines |
| 12/20/2012 | CA2839411A1 Aircraft powerplant |
| 12/20/2012 | CA2838561A1 Aircraft engine fuel system and method of operating the same |
| 12/20/2012 | CA2831780A1 Member covered with hard coating |
| 12/20/2012 | CA2779761A1 Fail-safe manual rotator cover |
| 12/20/2012 | CA2778594A1 Support structure forming method |
| 12/19/2012 | EP2535643A2 Systems and methods for combustor emissions control |
| 12/19/2012 | EP2535548A2 Turbine section of high bypass turbofan |
| 12/19/2012 | EP2535544A2 Transverse mounted accessory gearbox |
| 12/19/2012 | EP2535543A1 Method for operating a fuel supply for a heat engine |
| 12/19/2012 | EP2535542A2 Systems and methods for improving the efficiency of a combined cycle power plant |
| 12/19/2012 | EP2535541A1 Aircraft |
| 12/19/2012 | EP2535528A2 Turbofan engine bearing support |
| 12/19/2012 | EP2535527A2 Turbofan engine comprising a fan rotor support |
| 12/19/2012 | EP2534361A1 Gas-guiding pipe comprising a noise-attenuating covering with variable porosity |
| 12/19/2012 | EP2534358A1 Device for ejecting gas from a gas turbine engine and gas turbine engine |
| 12/19/2012 | EP2534350A1 Link between the exhaust casing and a structural ring of the fan duct of a jet engine |
| 12/19/2012 | DE202011109219U1 Hitzeschild Heat shield |
| 12/19/2012 | CN202611880U Gas turbine coal gas inlet filtering device |
| 12/19/2012 | CN202611879U Combustible gas pressure boost and stabilization device for gas turbine generator |
| 12/19/2012 | CN202611856U High-pressure air source compression system |
| 12/19/2012 | CN102834318A Unitized engine nacelle structure |
| 12/19/2012 | CN102828832A Method for improving starting capability of fixed-geometry two-dimensional mixed-compression inlet |
| 12/19/2012 | CN102825898A Method for manufacturing a composite surface |
| 12/19/2012 | CN101542129B 压缩机 Compressor |
| 12/18/2012 | US8333544 Card seal for a turbomachine |
| 12/18/2012 | US8333077 Replaceable orifice for combustion tuning and related method |
| 12/18/2012 | US8333076 Isentropic compression inlet for supersonic aircraft |
| 12/18/2012 | US8333075 Gas turbine premixer with internal cooling |
| 12/18/2012 | CA2504168C High aspect ratio cavity cooling circuit for a gas turbine blade |
| 12/13/2012 | WO2012170404A1 System and method for mounting an aircraft engine |
| 12/13/2012 | WO2012168649A1 Turbine engine comprising a floating bearing for guiding a shaft of the turbine engine |
| 12/13/2012 | US20120315141 Flow mixer |
| 12/13/2012 | US20120315137 Bearing chamber apparatus |
| 12/13/2012 | US20120312025 Method and systems for adaptive ignition energy |
| 12/13/2012 | US20120312024 Late lean injection with adjustable air splits |
| 12/13/2012 | US20120312023 Thermal management systems and methods for auxiliary power units |
| 12/13/2012 | US20120312022 Coalescing filter |
| 12/13/2012 | DE102011104065A1 Exhaust gas turbocharger for internal combustion engine of motor vehicle, has housing part and adjusting element, which is movably mounted in translatory and rotational manner for influencing flow of medium through exhaust gas turbocharger |
| 12/13/2012 | CA2838417A1 Turbine engine comprising a floating bearing for guiding a shaft of the turbine engine |
| 12/13/2012 | CA2837740A1 System and method for mounting an aircraft engine |
| 12/12/2012 | EP2532859A1 Fuel supply device for gas turbine engine |
| 12/12/2012 | EP2532858A2 Flexible support structure for a geared architecture gas turbine engine |
| 12/12/2012 | EP2532841A2 Flexible support structure for a geared architecture gas turbine engine |
| 12/12/2012 | EP2532840A1 Method and device for assisted monitoring of an aircraft turbine engine. |
| 12/12/2012 | EP2531709A2 Cooling of turbine components using combustor shell air |
| 12/12/2012 | CN202596899U Sound-proof device of gas engine |
| 12/12/2012 | CN202596898U Shockproof leg of gas engine |
| 12/12/2012 | CN202596897U Bleed air baffle plate structure |
| 12/12/2012 | CN202596896U Sand-prevention air-guide valve control circuit for helicopter |
| 12/12/2012 | CN202596895U Anti-icing bleed air device |
| 12/12/2012 | CN202596894U Reinforcing rib structure for outer casing wall of gas turbine |
| 12/12/2012 | CN102822475A Method for increasing the efficiency of a power plant equipped with a gas turbine, and power plant for carrying out the method |
| 12/12/2012 | CN102822450A Seal structure, turbine machine equipped with same, and power plant equipped with said turbine machine |
| 12/12/2012 | CN102817719A Aircraft engine cowl and process therefor |
| 12/12/2012 | CN102817718A Flexible support structure for a geared architecture gas turbine engine |
| 12/12/2012 | CN102817717A Flexible support structure for a geared architecture gas turbine engine |
| 12/12/2012 | CN102817716A Binary mixed pressure intake duct applied to supersonic solid ramjet |
| 12/12/2012 | CN102817715A Third-generation heavy fighter novel gas inlet channel lip |
| 12/12/2012 | CN102817714A Combustion gas turbine circulating device with intermediate water spray cooling and steam reinjection |
| 12/12/2012 | CN102817713A Combustible-ice power generation equipment |
| 12/12/2012 | CN102817641A Seal assembly for gas turbine |
| 12/12/2012 | CN101300406B 涡轮的清洁 Clean turbine |
| 12/11/2012 | US8332910 Method and apparatus for selective data control |
| 12/11/2012 | US8327649 Gas turbine fuel injector assembly with overlapping frictionally engaged members for damping vibrations |
| 12/11/2012 | US8327645 Isentropic compression inlet for supersonic aircraft |
| 12/11/2012 | US8327642 Multiple tube premixing device |
| 12/11/2012 | US8327616 Burner having a protective element for ignition electrodes |
| 12/11/2012 | CA2713209C System and method for the reduction of harmful substances in engine exhaust gases |
| 12/11/2012 | CA2544158C Integrated labyrinth and carbon seal |
| 12/11/2012 | CA2524594C Device for lubrication of a turbine engine component |
| 12/11/2012 | CA2496189C Method for refurbishing surfaces subjected to high compression contact |
| 12/06/2012 | WO2012165742A1 Rotating fuel injection device for ramjet engine and ramjet engine provided with same |
| 12/06/2012 | WO2012164204A1 Turbomachine fan case |
| 12/06/2012 | WO2012163538A1 Gas-turbine engine with a telescopic air inlet in the engine lining |
| 12/06/2012 | WO2012162923A1 Gas and steam turbine system |
| 12/06/2012 | US20120304666 Aircraft control system |
| 12/06/2012 | US20120304665 Mount device for transition duct in turbine system |
| 12/06/2012 | US20120304664 System for mounting combustor transition piece to frame of gas turbine engine |
| 12/06/2012 | US20120304662 Fuel air heat exchanger |
| 12/06/2012 | US20120304659 Impingement sleeve and methods for designing and forming impingement sleeve |
| 12/06/2012 | US20120304657 Lock leaf hula seal |
| 12/06/2012 | US20120304654 Combustion liner having turbulators |
| 12/06/2012 | US20120304653 Load member for transition duct in turbine system |
| 12/06/2012 | US20120304652 Injector apparatus |
| 12/06/2012 | US20120304651 Integrated fuel nozzle and ignition assembly for gas turbine engines |