| Patents for F02C 3 - Gas-turbine plants characterised by the use of combustion products as the working fluid (9,666) |
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| 01/15/2014 | CN103511082A Power station facility station based on liquid oxygen explosive power |
| 01/14/2014 | US8627668 System for fuel and diluent control |
| 01/09/2014 | WO2014008347A1 Non-symmetric arrangement of fuel nozzles in a combustor |
| 01/09/2014 | WO2014008053A1 Fuel flexible fuel injector |
| 01/09/2014 | WO2014008033A1 Functionally graded composite fan containment case |
| 01/09/2014 | WO2014007908A1 Turbine exhaust case duct |
| 01/09/2014 | WO2014007896A2 Geared turbofan with three co-rotating turbines |
| 01/09/2014 | WO2014007173A1 Wastewater treatment system and combined power generation equipment |
| 01/09/2014 | WO2014006564A1 A combustor |
| 01/09/2014 | WO2014006297A1 Device for simulating the ingestion of chunks of ice by an engine |
| 01/09/2014 | WO2014005921A1 Method for the production of water from the exhaust stream of a gas turbine system |
| 01/09/2014 | WO2013172906A3 Counter rotating low pressure turbine with splitter gear system |
| 01/09/2014 | US20140007591 Advanced tip-timing measurement blade mode identification |
| 01/09/2014 | US20140007590 Systems and Methods For Carbon Dioxide Capture In Low Emission Turbine Systems |
| 01/09/2014 | CA2878146A1 Device for simulating the ingestion of chunks of ice by an engine |
| 01/09/2014 | CA2820082A1 Gas turbine combustion system |
| 01/08/2014 | EP2682585A1 Gas turbine |
| 01/08/2014 | CN103502580A Integrated variable geometry flow restrictor and heat exchanger |
| 01/07/2014 | US8622714 Pressure exchanger |
| 01/07/2014 | US8621841 Gasification power generation system provided with carbon dioxide separation and recovery device |
| 01/03/2014 | WO2014004825A1 Turbine wheel catcher |
| 01/03/2014 | WO2014004266A1 Thrust reverser maintenance actuation system |
| 01/03/2014 | WO2014001230A1 Method for a part load co reduction operation for a sequential gas turbine |
| 01/02/2014 | US20140000282 Turbine blade platform with u-channel cooling holes |
| 01/02/2014 | US20140000281 Gas turbine engine turbine blade airfoil profile |
| 01/02/2014 | US20140000274 Methods and apparatus for co-firing fuel |
| 01/02/2014 | US20140000273 Low Emission Turbine Systems Incorporating Inlet Compressor Oxidant Control Apparatus And Methods Related Thereto |
| 01/02/2014 | US20140000272 Method and system for operating a turbine engine |
| 01/02/2014 | US20140000271 Systems and Methods For Controlling Stoichiometric Combustion In Low Emission Turbine Systems |
| 01/02/2014 | US20140000270 Stand-by operation of a gas turbine |
| 01/02/2014 | US20140000269 Combustion nozzle and an associated method thereof |
| 01/02/2014 | US20140000262 Gas turbine engine component with discharge slot having oval geometry |
| 01/02/2014 | US20140000236 Combustor |
| 01/02/2014 | US20140000235 Stirling cycle machine |
| 01/01/2014 | EP2679783A2 Spool for turbo machinery |
| 12/31/2013 | US8617293 Membranes suitable for gas separation, and related articles and processes |
| 12/31/2013 | US8616004 Quench jet arrangement for annular rich-quench-lean gas turbine combustors |
| 12/27/2013 | WO2013192540A1 Turbine engine combustor wall with non-uniform distribution of effusion apertures |
| 12/27/2013 | WO2013192523A1 Gas fuel turbine engine for reduced oscillations |
| 12/27/2013 | WO2013191954A1 Method of reducing combustion induced oscillations in a turbine engine |
| 12/27/2013 | WO2013191937A1 Compressor cover for turbochargers |
| 12/27/2013 | WO2013191877A1 Airfoil including adhesively bonded shroud |
| 12/27/2013 | WO2013189470A1 Combustion engine |
| 12/26/2013 | US20130340437 Turbine engine combustor wall with non-uniform distribution of effusion apertures |
| 12/26/2013 | US20130340435 Gas turbine engine aft spool bearing arrangement and hub wall configuration |
| 12/26/2013 | US20130340403 Erosion and corrosion resistant coatings for exhaust gas recirculation based gas turbines |
| 12/25/2013 | EP2677139A2 Fuel delivery system |
| 12/25/2013 | EP2677138A2 Fuel system |
| 12/25/2013 | EP2676022A2 Fluid flow devices with vertically simple geometry and methods of making the same |
| 12/25/2013 | CN203362320U Charging automobile engine |
| 12/25/2013 | CN103470318A Method for controlling temperature of a turbine engine compressor and compressor of a turbine engine |
| 12/25/2013 | CN101021181B Double bypass turbofan |
| 12/24/2013 | US8613187 Fuel flexible combustor systems and methods |
| 12/20/2013 | DE202012103544U1 System zur Erzeugung von Heißwasser und/oder Dampf mit Hochtemperaturspeicher für den Einsatz in einem Gasturbinenkraftwerk System to generate hot water and / or steam with high temperature storage for use in a gas turbine power plant |
| 12/19/2013 | WO2013187944A2 Counter rotating low pressure compressor and turbine each having a gear system |
| 12/19/2013 | WO2013013740A3 Gas turbine centripetal annular combustion chamber and method for flow guidance |
| 12/19/2013 | US20130333393 Gas turbine control systems and methods |
| 12/19/2013 | US20130333392 Turbine compressor blade tip resistant to metal transfer |
| 12/19/2013 | US20130333391 Integration of pressure swing adsorption with a power plant for co2 capture/utilization and n2 production |
| 12/19/2013 | CA2876195A1 Integration of pressure swing adsorption with a power plant for co2 capture/utilization and n2 production |
| 12/18/2013 | EP2674688A2 Air Treatment Apparatus and System Comprised Thereof |
| 12/18/2013 | CN103452671A Gas turbine compressor inlet pressurization and flow control system |
| 12/18/2013 | CN103452670A Micro gas turbine combined circulating system based on renewable energy sources |
| 12/18/2013 | CN103452669A Fuel gas autorotation type engine |
| 12/18/2013 | CN103452668A Axial compressor and gas turbine having axial compressor |
| 12/18/2013 | CN103452667A Gas turbine compressor inlet pressurization having a torque converter system |
| 12/18/2013 | CN101457693B Method and system for controlling flowrate of recirculated exhaust gas |
| 12/17/2013 | US8607576 Single turbine driving dual compressors |
| 12/12/2013 | WO2013184619A1 Single turbine driving dual compressors |
| 12/12/2013 | WO2013184504A1 Combustor liner with reduced cooling dilution openings |
| 12/12/2013 | WO2013184502A1 Combustor liner with improved film cooling |
| 12/12/2013 | WO2013184496A1 Combustor liner with convergent cooling channel |
| 12/12/2013 | WO2013184495A2 Combustor liner with decreased liner cooling |
| 12/12/2013 | WO2013184454A1 Seal land for static structure of a gas turbine engine |
| 12/12/2013 | WO2013184330A1 Nacelle inner flow structure leading edge latching system |
| 12/12/2013 | WO2013184329A1 Compressor tip clearance management for a gas turbine engine |
| 12/12/2013 | US20130327060 Single turbine driving dual compressors |
| 12/12/2013 | US20130327050 Controlling flame stability of a gas turbine generator |
| 12/12/2013 | US20130327010 Wave disc engine apparatus |
| 12/11/2013 | EP2672089A1 Control device for gas turbine power generation plant |
| 12/11/2013 | CN203335245U Aircraft pipeline wheel gas engine |
| 12/11/2013 | CN103443403A Systems and methods for carbon dioxide capture in low emission combined turbine systems |
| 12/10/2013 | US8601820 Integrated late lean injection on a combustion liner and late lean injection sleeve assembly |
| 12/05/2013 | WO2013180917A1 Adaptive fan with cold turbine |
| 12/05/2013 | WO2013180895A1 Turbomachine containment structure |
| 12/05/2013 | WO2013180424A1 Apparatus for a fuel-air pre-mixture using a rotary injection device and a gas turbine burner mounting the same |
| 12/05/2013 | US20130319011 Geared architecture carrier torque frame assembly |
| 12/05/2013 | US20130319010 Airfoil cover system |
| 12/05/2013 | US20130319008 Turbine blade support |
| 12/05/2013 | US20130319006 Direct feed auxiliary oil system for geared turbofan engine |
| 12/05/2013 | US20130318999 Gas turbine engine with a counter rotating fan |
| 12/05/2013 | US20130318998 Geared turbofan with three turbines with high speed fan drive turbine |
| 12/05/2013 | US20130318992 Combustor with a Brief Severe Quench Zone |
| 12/05/2013 | US20130318991 Combustor With Multiple Combustion Zones With Injector Placement for Component Durability |
| 12/05/2013 | US20130318988 Aircraft engine with turbine heat exchanger bypass |
| 12/05/2013 | US20130318984 Gas Turbine Compressor Inlet Pressurization Having a Torque Converter System |
| 12/05/2013 | US20130318982 Turbine cooling apparatus |
| 12/05/2013 | US20130318981 Adaptive fan with cold turbine |
| 12/05/2013 | US20130318976 Turbomachine combustor nozzle and method of forming the same |
| 12/05/2013 | US20130318972 Gas turbine apparatus with improved exergy recovery |