| 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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| 02/07/2013 | US20130033008 Outward bristle brush seal design for gas turbine application |
| 02/07/2013 | US20130032643 Combustor leaf seal arrangement |
| 02/07/2013 | US20130031914 Two stage serial impingement cooling for isogrid structures |
| 02/07/2013 | US20130031913 Movable strut cover for exhaust diffuser |
| 02/07/2013 | US20130031912 Gas turbine start architecture |
| 02/07/2013 | US20130031910 Efficient Selective Catalyst Reduction System |
| 02/07/2013 | US20130031907 Fuel injecting assembly for gas turbine engine |
| 02/07/2013 | US20130031904 Combustion chamber |
| 02/07/2013 | DE102011109704A1 Compressor i.e. radial compressor, for compressing air to be supplied to reciprocating internal combustion engine of passenger car, has noise ring including longitudinal areas that exhibit angle smaller than specific degrees |
| 02/06/2013 | EP2554907A1 Combustor and gas turbine |
| 02/06/2013 | EP2554874A2 Journal pin oil supply for gear system |
| 02/06/2013 | EP2554823A1 Fuel supply device of gas turbine engine |
| 02/06/2013 | EP2554822A2 Linking device more specifically suited to providing the link between an air intake and an engine of an aircraft nacelle |
| 02/06/2013 | EP2554792A1 Double-jet film cooling structure |
| 02/06/2013 | EP2554697A1 Ni-based alloy, and gas turbine rotor blade and stator blade each using same |
| 02/06/2013 | EP2554482A1 APU selective cool down cycle |
| 02/06/2013 | EP2554481A2 Linking device more specifically suited to providing the link between an air intake and an engine of an aircraft nacelle |
| 02/06/2013 | EP2554480A2 Linking device more specifically suited to providing the link between an air intake and an engine of an aircraft nacelle |
| 02/06/2013 | EP2554479A2 Linking device more specifically suited to providing the link between an air intake and an engine of an aircraft nacelle |
| 02/06/2013 | EP2553251A1 Adaptive fan system for a variable cycle turbofan engine |
| 02/06/2013 | EP2553244A1 Method for increasing the efficiency of a power plant equipped with a gas turbine, and power plant for carrying out the method |
| 02/06/2013 | CN202718760U Plasma ignitor with reusable cathode |
| 02/06/2013 | CN102918308A Axial seal structure and rotation mechanism provided with same |
| 02/06/2013 | CN102913329A Baffle door device used for air inlet channel of combustion engine |
| 02/05/2013 | US8370044 NOX compliant peak for gas turbine |
| 02/05/2013 | US8366382 Mid-turbine frame buffer system |
| 02/05/2013 | US8365699 Hybrid cycle rotary engine |
| 02/05/2013 | US8365538 High temperature-resistant sealing assembly, especially for gas turbines |
| 02/05/2013 | US8365534 Gas turbine combustor having a fuel nozzle for flame anchoring |
| 02/05/2013 | US8365530 System for conditioning the airflow entering a turbomachine |
| 02/05/2013 | CA2504167C Noise reduction assembly for aircraft turbojet engine |
| 02/01/2013 | CA2783488A1 A resistor and a method of manufacturing a resistor capable of operating at high temperatures |
| 01/31/2013 | WO2013014198A1 Turbo - compressor train with rolling bearings and related assembly method |
| 01/31/2013 | WO2013014176A1 Method for running up a stationary gas turbine |
| 01/31/2013 | WO2012116285A3 Wave disc engine apparatus |
| 01/31/2013 | US20130030064 Gasification system and method |
| 01/31/2013 | US20130029236 Device for Providing Hot Exhaust Gases |
| 01/31/2013 | US20130028718 Strut, a gas turbine engine frame comprising the strut and a gas turbine engine comprising the frame |
| 01/31/2013 | US20130028713 Seal for turbomachine segments |
| 01/31/2013 | US20130025291 System and method for protection of high temperature machinery components |
| 01/31/2013 | US20130025289 Combustor portion for a turbomachine and method of operating a turbomachine |
| 01/31/2013 | US20130025288 Microcircuit cooling for gas turbine engine combustor |
| 01/31/2013 | US20130025287 Distributed cooling for gas turbine engine combustor |
| 01/31/2013 | US20130025282 Resonator device for damping the pressure oscillation within a combustion chamber and a method for operating a combustion arrangement |
| 01/31/2013 | US20130025255 Electric discharge apparatus |
| 01/31/2013 | DE102012105753A1 Verfahren zur Befeuchtung von Verdunstungskühlermedien durch eine durchlässige Schicht Method for moistening of evaporative cooler media through a permeable layer |
| 01/31/2013 | DE102012014646A1 Kompressorrotor Compressor rotor |
| 01/31/2013 | DE102011108887A1 Gasturbinenzentripetalringbrennkammer sowie Verfahren zur Strömungsführung Gasturbinenzentripetalringbrennkammer and methods for guiding the flow |
| 01/31/2013 | DE102011108533A1 Abgasturbinenkonus mit dreidimensional profilierter Trennwand sowie plattenartiges Wandelement Turbine exhaust cone with three-dimensionally profiled partition wall and plate-like element |
| 01/31/2013 | DE102008052321B4 Turbolader mit Magnetlageranordnung Turbocharger with magnetic bearing assembly |
| 01/31/2013 | CA2843112A1 Turbo-compressor train with rolling bearings and related assembly method |
| 01/30/2013 | EP2551888A2 Electric discharge apparatus |
| 01/30/2013 | EP2551494A2 Motor-generator and prime mover gearing assembly |
| 01/30/2013 | EP2551493A2 Gearing assembly |
| 01/30/2013 | EP2551492A1 Seal structure for turbine rotor |
| 01/30/2013 | EP2551491A2 System for conditioning air flow into a multi-nozzle assembly |
| 01/30/2013 | EP2551490A1 Axial compressor with an injection device for injecting a fluid |
| 01/30/2013 | EP2551489A2 Gas turbine bearing arrangement |
| 01/30/2013 | EP2551488A2 Three spool engine bearing configuration |
| 01/30/2013 | EP2551486A1 Method for injecting water into a multistage axial compressor of a gas turbine |
| 01/30/2013 | EP2551470A1 Method for starting a stationary gas turbine |
| 01/30/2013 | CN202707277U Air exhaust heating nozzle used for gas turbine air intake filter |
| 01/30/2013 | CN202707252U Flame retardant adding device of fuel system and gas turbine generator unit |
| 01/30/2013 | CN202707251U Air intake desalting device of gas combustion engine of coke oven |
| 01/30/2013 | CN202707250U Air inlet anti-icing control system for gas turbine |
| 01/30/2013 | CN202707249U Gas turbine recirculation device with intermediate spraying cooling and steam reinjection |
| 01/30/2013 | CN202700881U Descaling device and gas turbine with the same |
| 01/30/2013 | CN102906376A Combined cycle power generator |
| 01/30/2013 | CN102900542A Motor-generator and prime mover gearing assembly |
| 01/30/2013 | CN102900541A System and method for supporting a shaft inside a turbine |
| 01/30/2013 | CN102900540A System for ventilating a gas turbine enclosure |
| 01/30/2013 | CN102900539A Anti-icing and denoising assembly |
| 01/30/2013 | CN102900538A Double-working-medium combined cycle turbine annular combustion phase change chamber |
| 01/30/2013 | CN102900536A System and method for power generation by using oxy-fuel combustion |
| 01/30/2013 | CN102900532A Intermittent-cold back-heat main pipe type split compressor gas turbine unit |
| 01/30/2013 | CN102900531A Combustion gas turbine system with inlet cooling and indirect cooling |
| 01/30/2013 | CN102900529A Method for cooling and efficiency improvement of double-working-medium combined cycle turbine |
| 01/30/2013 | CN102900528A Self power consumption reduction method of double-working-medium combined cycle turbine |
| 01/30/2013 | CN102900471A Efficient low-resistant structural or efficient energy-gathered structural or efficient engine |
| 01/29/2013 | US8359870 Automatic fuel nozzle flame-holding quench |
| 01/29/2013 | CA2761998C Improved bearing chamber pressurization system |
| 01/29/2013 | CA2690216C Turbine wash port for a gas turbine engine |
| 01/29/2013 | CA2549748C Pressurized oil supply for propeller engine system |
| 01/29/2013 | CA2525189C Gas turbine engine fuel injector |
| 01/24/2013 | WO2013010935A1 Method for operating a static gas turbine, and intake duct for intake air of a gas turbine |
| 01/24/2013 | US20130019609 Gas turbine engine systems involving i-beam struts |
| 01/24/2013 | US20130019608 Method of inhibiting ice accretion within a turbine engine and control system therefor |
| 01/24/2013 | US20130019605 Method for operating a firing plant |
| 01/24/2013 | US20130019604 Multi-stage amplification vortex mixture for gas turbine engine combustor |
| 01/24/2013 | US20130019602 System for damping oscillations in a turbine combustor |
| 01/24/2013 | US20130019584 Burner, gas turbine combustor, burner cooling method, and burner modifying method |
| 01/24/2013 | DE102012013198A1 Assembly for holding turbo-supercharger at e.g. crankcase of reciprocating internal combustion engine of motor vehicle, has holding element partially made of material that has larger thermal expansion coefficient than another material |
| 01/24/2013 | DE102011079677A1 Charging device, particularly exhaust gas turbocharger of internal combustion engine, comprises bearing housing for supporting rotor, where bearing housing is formed as composite component and has compressor section or light metal |
| 01/23/2013 | EP2549080A2 Method of inhibiting ice accretion within a turbine engine and control system therefor |
| 01/23/2013 | EP2549079A1 Engine generator device |
| 01/23/2013 | EP2549078A1 Suction duct for intake air of a gas turbine and method for operating a stationary gas turbine |
| 01/23/2013 | EP2549077A1 Gas turbine equipment utilizing high humidity |
| 01/23/2013 | EP2547889A2 Optical monitoring system for a turbine engine |
| 01/23/2013 | CN202690228U Silencing box |
| 01/23/2013 | CN102892996A Turbomachine fueling system with jet pump |