| 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) |
|---|
| 09/11/2013 | CN103291455A Co-generation compressed air energy storage method and energy storage system |
| 09/11/2013 | CN103291388A Compression sleeve seal |
| 09/11/2013 | CN102057144B Method of depositing a coating for improving laminar flow |
| 09/11/2013 | CN102015450B Wave attenuation panel inserted between the motor and air inlet of an aircraft nacelle |
| 09/11/2013 | CN101960092B 涡轮盘及燃气轮机 Turbine and gas turbine disc |
| 09/10/2013 | US8528839 Combustor nozzle and method for fabricating the combustor nozzle |
| 09/10/2013 | US8528340 Turbine engine flow sleeve |
| 09/10/2013 | US8528335 Fuel heater system including hot and warm water sources |
| 09/10/2013 | US8528334 Flow conditioner for fuel injector for combustor and method for low-NOx combustor |
| 09/10/2013 | US8528315 Air cooling apparatus for a purge valve |
| 09/10/2013 | US8528314 Method and apparatus for combined cycle power plant startup |
| 09/10/2013 | CA2693314C Fluid conduit coupling with leakage detection |
| 09/09/2013 | CA2805833A1 Jet noise reduction using eduction effect |
| 09/08/2013 | CA2805837A1 Bleed noise reduction |
| 09/07/2013 | CA2808038A1 Apparatus for extracting input power from the low pressure spool of a turbine engine |
| 09/06/2013 | WO2013130945A1 Laser clad fuel injector premix barrel |
| 09/06/2013 | WO2013130575A1 Turbine nozzle insert |
| 09/06/2013 | WO2013130570A1 Turbine engine rotor blade groove |
| 09/06/2013 | WO2013130506A1 System and method for monitoring corrosive contaminants in a fluid |
| 09/06/2013 | WO2013130308A1 Buffer cooling system providing gas turbine engine architecture cooling |
| 09/06/2013 | WO2013130307A1 Gas turbine engine buffer cooling system |
| 09/06/2013 | WO2013130296A1 Gas turbine engine driving multiple fans |
| 09/06/2013 | WO2013130295A1 Geared gas turbine engine with reduced fan noise |
| 09/06/2013 | WO2013130291A1 Acoustic treatment in an unducted area of a geared turbomachine |
| 09/06/2013 | WO2013130290A1 Component blending tool assembly |
| 09/06/2013 | WO2013130289A1 Gas turbine engine thrust reverser system |
| 09/06/2013 | WO2013130246A1 Gas turbine engine buffer cooling system |
| 09/06/2013 | WO2013130245A1 Gas turbine engine cooling system |
| 09/06/2013 | WO2013129788A1 Turbine seal assembly and turbine apparatus comprising the turbine seal assembly |
| 09/06/2013 | WO2013127916A1 Method of operating a gas turbine power plant with exhaust gas recirculation and corresponding gas turbine power plant |
| 09/06/2013 | WO2013127833A1 Arrangement for a turbomachine |
| 09/05/2013 | US20130230388 Compressor |
| 09/05/2013 | US20130229012 Waste heat utilization for energy efficient carbon capture |
| 09/05/2013 | US20130227964 Transition piece aft frame assembly having a heat shield |
| 09/05/2013 | US20130227960 Liquid level monitoring and reporting system |
| 09/05/2013 | US20130227951 Laser clad fuel injector premix barrel |
| 09/05/2013 | US20130227930 Gas turbine frame stiffening rails |
| 09/05/2013 | US20130227929 System and device for monitoring contaminants in a fluid |
| 09/05/2013 | US20130227928 Fuel nozzle assembly for use in turbine engines and method of assembling same |
| 09/05/2013 | CA2807217A1 Gas turbine frame stiffening rails |
| 09/04/2013 | EP2634459A1 Shaft seal mechanism and rotary machine provided with same |
| 09/04/2013 | EP2634395A1 Gas turbine and gas turbine plant provided with same |
| 09/04/2013 | EP2634394A2 Combustion system for a gas turbine engine and method for directing fuel flow within the same |
| 09/04/2013 | EP2634380A1 Gas turbine burner fuel feeding system |
| 09/04/2013 | EP2634373A1 Arrangement for a turbomachine |
| 09/04/2013 | EP2633220A2 Disc damper for charge air lines of an internal combustion engine having a turbocharger |
| 09/04/2013 | EP2633167A1 Utilizing heat discarded from a gas turbine engine |
| 09/04/2013 | CN203175686U Countercurrent tangential type micro turbine jet-engine |
| 09/04/2013 | CN103277196A Igniter and improvement method of igniter |
| 09/04/2013 | CN103277195A Fuel supply switching system used between gas turbine generator units |
| 09/04/2013 | CN103277194A Method of servicing a gas turbine engine |
| 09/04/2013 | CN103277193A Combustion gas turbine power generation method adopting low calorific value gas to perform catalytic combustion |
| 09/04/2013 | CN102119280B Thrust bearing lubrication nozzle |
| 09/04/2013 | CN101868602B Damping device and gas turbine combustor |
| 09/03/2013 | US8522572 Adaptive power and thermal management system |
| 09/03/2013 | US8522561 Acoustically tuned combustion for a gas turbine engine |
| 09/03/2013 | US8522553 System and method for conditioning a working fluid in a combustor |
| 09/03/2013 | US8522527 Burner for a gas turbine and method for feeding a gaseous fuel in a burner |
| 09/03/2013 | US8522526 Two-shaft engine for aircraft with high electric power demand |
| 09/03/2013 | US8522525 Apparatus and method for drawing off and recirculating a cooling stream |
| 09/03/2013 | US8522524 Compressor for pressurising carbon dioxide |
| 09/03/2013 | US8522521 Combined air turbine starter, air-oil cooler, and fan |
| 09/02/2013 | CA2805192A1 Liquid level monitoring and reporting system |
| 08/29/2013 | WO2013126728A1 Turbine engine with thrust vectoring exhaust nozzle |
| 08/29/2013 | WO2013126514A1 Multi-electrode igniter for a gas turbine engine |
| 08/29/2013 | WO2013126471A1 Turbine frame fairing for a gas turbine engine |
| 08/29/2013 | WO2013126213A1 Vane assembly for a gas turbine engine |
| 08/29/2013 | WO2013126119A1 Accessory gearbox with tower shaft removal capability |
| 08/29/2013 | WO2013126116A2 Turbine engine monitoring system |
| 08/29/2013 | WO2013125948A1 Process to obtain a compressed gas |
| 08/29/2013 | WO2013124285A1 An inlet air filter device for a power plant |
| 08/29/2013 | WO2013103416A3 Filter systems for air intakes of aircraft engines and related methods |
| 08/29/2013 | US20130223989 Acoustic damper, combustor and gas turbine |
| 08/29/2013 | US20130223987 Turbine Nozzle Insert |
| 08/29/2013 | US20130223982 Thermal expansion joint connection for sheet metal assembly |
| 08/29/2013 | US20130219916 Apparatus and method for conditioning air received by a power generation system |
| 08/29/2013 | US20130219915 Fuel air heat exchanger |
| 08/29/2013 | US20130219913 Geared turbofan gas turbine engine with reliability check on gear connection |
| 08/29/2013 | US20130219912 Combustor and method for purging a combustor |
| 08/29/2013 | US20130219911 Combustion system for a gas turbine engine and method for directing fuel flow within the same |
| 08/29/2013 | US20130219902 Burner pressure transducer thermal management design |
| 08/29/2013 | US20130219900 Gas Turbine Combustor |
| 08/29/2013 | US20130219898 Combustor and gas turbine |
| 08/29/2013 | US20130219896 Flame holding boundary control |
| 08/29/2013 | US20130219854 Air-cooled oil cooler for turbofan engine |
| 08/29/2013 | DE102012203047A1 Lagervorrichtung und Turbomaschine mit Lagervorrichtung Storage device and turbomachinery bearing device |
| 08/29/2013 | DE102010034276B4 Kombinierter Kraftwerksprozess mit Abgasreinigungsvorrichtung Combined power plant process with an emission control device |
| 08/29/2013 | CA2805282A1 Counter rotating low pressure turbine with splitter gear system |
| 08/29/2013 | CA2805279A1 Counter-rotating low pressure turbine with gear system mounted to mid turbine frame |
| 08/29/2013 | CA2805186A1 Counter rotating low pressure compressor and turbine each having a gear system |
| 08/28/2013 | EP2631453A2 Fuel purging system for a turbine assembly |
| 08/28/2013 | EP2631452A2 Gas turbine inlet system with solid-state heat pump |
| 08/28/2013 | EP2631451A1 Gas turbine and operating method thereof |
| 08/28/2013 | EP2631450A1 Element for sound absorption in aircrafts nacelles |
| 08/28/2013 | EP2631324A1 Ni-based superalloy member having heat-resistant bond coat layer formed therein |
| 08/28/2013 | EP2630427A2 System and method for liquid air production, power storage and power release |
| 08/28/2013 | EP2630340A2 Lubricating device having a bypass valve |
| 08/28/2013 | CN103270276A Method for balancing rotating assembly of gas turbine engine |
| 08/28/2013 | CN103270250A Shaft sealing device, and rotary machine equipped therewith |
| 08/28/2013 | CN103266953A Gas turbine engine system |