| 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) |
|---|
| 04/29/2009 | CN100482864C Highly oxidation resistant component |
| 04/28/2009 | US7524161 Gas turbine engine blade containment assembly |
| 04/28/2009 | US7523616 Methods and apparatuses for assembling a gas turbine engine |
| 04/28/2009 | US7523602 Turbine exhaust catalyst |
| 04/28/2009 | CA2308062C A method for producing matched fluidic surfaces |
| 04/23/2009 | WO2009051236A1 Gas turbine |
| 04/23/2009 | WO2009051031A1 Method of repair |
| 04/23/2009 | WO2004033871A3 Leak resistant vane cluster |
| 04/23/2009 | US20090104028 Method and apparatus for distributing fluid into a turbomachine |
| 04/23/2009 | US20090104026 Control of clearance at blade tips in a high-pressure turbine of a turbine engine |
| 04/23/2009 | US20090104024 Air intake for a turbocharger for an internal combustion engine |
| 04/23/2009 | US20090104019 Offset drive for gas turbine engine |
| 04/23/2009 | US20090102203 System and method for power production using a hybrid helical detonation device |
| 04/23/2009 | US20090100839 Combustion chamber wall with optimized dilution and cooling, and combustion chamber and turbomachine both provided therewith |
| 04/23/2009 | US20090100821 Managing leaks in a gas turbine system |
| 04/23/2009 | DE102008037481A1 System zur Zuführung von Luft von einem Mehrstufenverdichter zu einem Turbinenabschnitt einer Gastrubine System for supplying air from a multistage compressor to a turbine section of a guest rubies |
| 04/23/2009 | DE102007050231A1 Exhaust-gas turbocharger, has spacer element and pressure element provided between antifriction bearings, where inner bearing ring of one of bearings is fastened to shaft and outer bearing ring of other bearing is fastened to pipe |
| 04/23/2009 | CA2639025A1 Gas turbine oil scavenging system |
| 04/22/2009 | EP1444491B1 Vibration monitoring system for gas turbine engines |
| 04/22/2009 | CN201225195Y Biological stalk gasification combined circulation power generation system |
| 04/22/2009 | CN101415607A Air inlet lip for a pod with electric defrosting |
| 04/22/2009 | CN101413440A Minitype gas turbine electric generating set |
| 04/22/2009 | CA2641963A1 Blade tip clearance control for a turbine engine high-pressure turbine |
| 04/21/2009 | US7520369 Soundproofing panel with beads, and a method of manufacture |
| 04/21/2009 | US7520137 Method of controlling the injection of liquid into an inflow duct of a prime mover or driven machine |
| 04/21/2009 | US7520136 Method and system for protecting gas turbine fuel injectors |
| 04/21/2009 | US7520055 Method for manufacturing a stator or rotor component |
| 04/21/2009 | CA2449339C Turbine nozzle segment and method of repairing same |
| 04/21/2009 | CA2430511C Method of removing ceramic coatings |
| 04/16/2009 | WO2009048129A1 Closed cycle plant |
| 04/16/2009 | WO2009047543A1 Device for inhibiting the flow of oil along a rotating shaft |
| 04/16/2009 | WO2009047538A1 Turbomachine |
| 04/16/2009 | WO2007015847A3 Turbine engine with interstage heat transfer |
| 04/16/2009 | WO2006107828A3 Toroidal intersecting vane gas management system |
| 04/16/2009 | US20090097972 Gas Turbine Engine Systems and Related Methods Involving Heat Exchange |
| 04/16/2009 | US20090097963 Vane and a Vane assembly for a gas turbine engine |
| 04/16/2009 | US20090096174 Blade outer air seal for a gas turbine engine |
| 04/16/2009 | US20090094989 Apparatus and method for suppressing dynamic pressure instability in bleed duct |
| 04/16/2009 | US20090094984 Staging for rich catalytic combustion |
| 04/16/2009 | US20090094960 Method for operating a gas turbine, method of operation of a combined cycle power plant, and combined cycle power plant |
| 04/16/2009 | DE102008037423A1 Ringeinsatz für Brennkammerauskleidung und zugehöriges Verfahren Ring insert for combustor liner and associated method |
| 04/16/2009 | DE102007048527A1 Schubtriebwerk Thruster |
| 04/16/2009 | DE102007048484A1 Heißgasgeführte Komponente einer Strömungsmaschine Guided hot gas component of a turbomachine |
| 04/15/2009 | EP2048337A1 Fuel supply circuit for an aircraft engine |
| 04/15/2009 | EP2048330A2 Systems and methods involving multiple torque paths for gas turbine engines |
| 04/15/2009 | EP2048328A2 Seal assembly retention feature and assembly method |
| 04/15/2009 | EP2048324A1 Turbine stator for aircraft turbomachine including a vibration damper device |
| 04/15/2009 | EP2047085A1 Method for operating a power station with integrated coal gasification and power station |
| 04/15/2009 | EP1952003A4 Method and apparatus for spectroscopic measurements in the combustion zone of a gas turbine engine |
| 04/15/2009 | EP1943419A4 Infrared suppression system |
| 04/15/2009 | CN201221414Y Combined heat and power minitype gas turbine |
| 04/15/2009 | CN201221413Y Thermal power generation core machine |
| 04/15/2009 | CN101410591A Jet engine with detachably arranged generator unit |
| 04/15/2009 | CN101410300A Air inlet shroud structure |
| 04/15/2009 | CN100478559C High supersound air-intake air turbogenerator |
| 04/15/2009 | CN100478545C High efficiency rotor for the first phase of a gas turbine |
| 04/15/2009 | CN100478100C Method for forming cove on the metal parts surface and parts formed thereby |
| 04/14/2009 | US7516621 Modular LRU accessory mounting substrate for auxiliary power unit |
| 04/14/2009 | US7516609 Carbon dioxide recirculation |
| 04/14/2009 | CA2412906C Drainage system for gas turbine supporting bearings |
| 04/14/2009 | CA2407954C Device for controlling the cooling flows of gas turbines |
| 04/09/2009 | WO2009044093A2 Fuel supply system |
| 04/09/2009 | WO2009043694A2 Stationary gas turbine for generating power |
| 04/09/2009 | US20090090096 Epicyclic gear train for variable cycle engine |
| 04/09/2009 | DE102007036930A1 Gas-turbine engine e.g. civilian aircraft engine or military aircraft engine, has thermoelectric generator generating electrical energy from temperature difference between hot current via core engine and cold current via bypass channel |
| 04/08/2009 | EP2045907A2 Method to re-engage start of dynamoelectric machine |
| 04/08/2009 | EP2045448A1 Low-noise exhaust gas facility |
| 04/08/2009 | EP2045447A1 Turbofan engine intermediate casing and corresponding turbofan engine |
| 04/08/2009 | EP2044685A1 Voltage-controlled oscillator (vco) |
| 04/08/2009 | EP1899593B1 System for defrosting the leading edge of the inlet fairing of a turboengine |
| 04/08/2009 | CN101405478A Leak resistant vane cluster |
| 04/08/2009 | CN101405184A Structure for an air inlet lip of an electric de-icing pod comprising an acoustic attenuation zone |
| 04/07/2009 | US7513737 Gas turbine blade cooling circuit having a cavity with a high aspect ratio |
| 04/07/2009 | US7513119 Systems and methods for starting aircraft engines |
| 04/07/2009 | US7513117 Method for operating a furnace |
| 04/07/2009 | US7513099 Temperature measuring device and regulation of the temperature of hot gas of a gas turbine |
| 04/04/2009 | CA2640208A1 Turbojet intermediate housing and turbojet |
| 04/04/2009 | CA2637090A1 Faceted dome assemblies for gas turbine engine combustors |
| 04/02/2009 | WO2009042069A2 Improved ring segment coolant seal configuration |
| 04/02/2009 | WO2009041617A1 Turbine facility and power generating apparatus |
| 04/02/2009 | WO2009041436A1 Gas turbine combustor |
| 04/02/2009 | WO2009041435A1 Cooling structure for gas-turbine combustor |
| 04/02/2009 | WO2005086863A3 Mobile power system emissions control |
| 04/02/2009 | US20090087572 Gas turbines; intermetallics comprised of aluminum, nickel, and platinum; vapor deposition; heat treatment; electrodeposition |
| 04/02/2009 | US20090087309 Protective ring for the fan casing of a gas-turbine engine |
| 04/02/2009 | US20090084109 Fuel nozzle of gas turbine combustor for DME and design method thereof |
| 04/02/2009 | US20090084108 Integral heater for fuel conveying member |
| 04/02/2009 | US20090084100 Combustor assembly including one or more resonator assemblies and process for forming same |
| 04/02/2009 | DE102008037374A1 Torusförmiger Ringverteiler für die sekundäre Brennstoffdüse einer DLN-Gasturbine Toroidal ring manifold for the secondary fuel nozzle of a gas turbine DLN |
| 04/02/2009 | DE102007046687A1 Turboladeranordnung Turbocharger assembly |
| 04/02/2009 | DE102007043791A1 Verfahren zur Herstellung einer Wärmedämmschicht und Wärmedämmschicht A process for producing a thermal barrier coating and thermal barrier coating |
| 04/02/2009 | DE102007022922A1 Oil separator for airplane gas turbine, has vent line supplying oil air mixture to separator, where line is provided with angle region with respect to axle center and region is not essentially provided with transition roundings |
| 04/01/2009 | EP2042707A1 Stationary gas turbine for energy generation |
| 04/01/2009 | EP2041399A2 Aircraft engine inlet having zone of deformation |
| 04/01/2009 | EP2040818A2 Aircraft engine inlet pivotable barrier filter |
| 04/01/2009 | CN101397915A Airway type gas turbine |
| 04/01/2009 | CN100473806C Turbomachine having compact rolling bearing assembly |
| 03/31/2009 | US7509812 Dual ignition system for a gas turbine engine |
| 03/31/2009 | US7509811 Multi-point staging strategy for low emission and stable combustion |
| 03/31/2009 | US7509810 Inter-turbine temperature display compensation method |