| 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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| 06/12/2013 | CN202991239U Combustion gas turbine air bleeding sealing structure |
| 06/12/2013 | CN202991238U Gas compressor casing for gas turbine |
| 06/12/2013 | CN103147859A Gas turbine electricity generating apparatus |
| 06/12/2013 | CN101978150B System of counter-rotating propellers with a feathering device for propeller blades |
| 06/12/2013 | CN101939539B Engine-driven hydraulic pump |
| 06/12/2013 | CN101675226B Acoustic panel having a variable acoustic characteristic |
| 06/12/2013 | CN101631941B Coating for acoustic treatment having a hot air icing processing function |
| 06/12/2013 | CN101405184B Structure for an air inlet lip of an electric de-icing pod comprising an acoustic attenuation zone |
| 06/12/2013 | CN101368512B Turbine engine diffuser |
| 06/12/2013 | CN101230790B Control system based on forecasting model for heavy gas turbine |
| 06/12/2013 | CA2797229A1 Turning gear for gas turbine arrangements |
| 06/11/2013 | US8459936 Flexible seal for gas turbine engine system |
| 06/11/2013 | US8459934 Varying cross-sectional area guide blade |
| 06/11/2013 | US8459042 Gas turbine engine combustor and method for delivering purge gas into a combustion chamber of the combustor |
| 06/11/2013 | US8459040 Rear hub cooling for high pressure compressor |
| 06/11/2013 | US8459033 Systems and methods for modified wobbe index control with constant fuel temperature |
| 06/11/2013 | US8459001 Ammonia injection system |
| 06/11/2013 | CA2718682C Planetary gear reduction system |
| 06/11/2013 | CA2575277C Segmented effusion cooled gas turbine engine combustor |
| 06/11/2013 | CA2566789C Methods and apparatus for injecting fluids into a turbine engine |
| 06/11/2013 | CA2534213C Inboard radial dump venturi for combustion chamber of a gas turbine |
| 06/11/2013 | CA2528808C Method and apparatus for decreasing combustor acoustics |
| 06/11/2013 | CA2502813C Improved fuel injector head |
| 06/08/2013 | CA2797299A1 Dynamic load reduction system |
| 06/07/2013 | CA2776525A1 Two-stage combustor for gas turbine engine |
| 06/06/2013 | WO2013081142A1 Turbine blade |
| 06/06/2013 | WO2013080894A1 Valve control device, gas turbine, and valve control method |
| 06/06/2013 | WO2013080839A1 Support mechanism for heavy structure |
| 06/06/2013 | WO2013080828A1 Bonded component |
| 06/06/2013 | WO2013080386A1 Solar thermal combined cycle power plant |
| 06/06/2013 | WO2013079294A1 Method for operating a fixed gas turbine with a low-calorific or medium-calorific fuel as well as a fixed gas turbine therefor |
| 06/06/2013 | US20130142643 Structural joint for connecting a first component to a segmented second component |
| 06/06/2013 | US20130142630 Airfoil seal system for gas turbine engine |
| 06/06/2013 | US20130142624 Multi-layer acoustic treatment panel |
| 06/06/2013 | US20130139520 Method for monitoring a control device of a fuel metering valve of a turbojet engine |
| 06/06/2013 | US20130139516 Cooling system for gas turbine load coupling |
| 06/06/2013 | US20130139514 Combustor liner support and seal assembly |
| 06/06/2013 | US20130139513 Fuel nozzle and method of repair |
| 06/06/2013 | US20130139511 Gas turbine combustor and gas turbine |
| 06/06/2013 | US20130139510 Method for manufacturing a hot gas path component and hot gas path turbine component |
| 06/06/2013 | US20130139487 Variable initiation location system for pulse detonation combustor |
| 06/06/2013 | US20130139486 Variable initiation location system for pulse detonation combustor |
| 06/06/2013 | DE212011100145U1 Selbstanpassende Dichtung für rotierende Turbomaschine Adaptive seal for rotating turbomachinery |
| 06/06/2013 | DE102012107305A1 Verdichtergehäuse und Zwei-Stufen-Turbolader damit The compressor housing and the two-stage turbocharger so that |
| 06/06/2013 | DE102012023626A1 Hochdruck-Verdichter, insbesondere einer Gasturbine High-pressure compressor, in particular a gas turbine, |
| 06/06/2013 | DE102011119881A1 Aufladeeinrichtung für eine Brennstoffzelle, insbesondere eines Kraftwagens Charging means for a fuel cell, in particular a motor vehicle |
| 06/06/2013 | DE102011087628A1 Ladeeinrichtung Loader |
| 06/05/2013 | EP2599981A2 Systems and Methods for Changing a Speed of a Compressor Boost Stage in a Gas Turbine |
| 06/05/2013 | EP2599967A1 Cooling system for gas turbine load coupling |
| 06/05/2013 | EP2599078A2 Acoustic panel for a turbojet engine nacelle, with in-built fasteners |
| 06/05/2013 | EP2598738A1 Lateral turbojet improved in order to limit the deformation thereof |
| 06/05/2013 | EP2598723A1 Quick-start device for a turbine, and method for operating a quick-start device |
| 06/05/2013 | CN202970913U Supporting system of gas turbine |
| 06/05/2013 | CN202970912U Intercooling and heat recovering structure of aero-engine |
| 06/05/2013 | CN103140716A Acoustic damper, combustor, and gas turbine |
| 06/05/2013 | CN103140651A System for pressurising the bearing chambers of turbine engines machines using air taken from the intake duct |
| 06/05/2013 | CN103140650A Sealing device having a sleeve for the passage of a connecting rod of a system for controlling the orientation of the blower blades of a turboprop engine through a partition |
| 06/05/2013 | CN103133145A Gas turbine engine lockout reduction |
| 06/05/2013 | CN103133144A On-duty flame device |
| 06/05/2013 | CN103133143A Method for operating a combustion device during transient operation |
| 06/05/2013 | CN103133142A Cooling system for gas turbine load coupling |
| 06/05/2013 | CN103133141A Gas turbine engine |
| 06/05/2013 | CN103133138A Internal combustion wave rotor based on non-constant combustion and with pressurization function and working method thereof |
| 06/05/2013 | CN101641256B Device for de-icing the air intake of a gas turbine |
| 06/05/2013 | CN101608576B Skid mounted equipment structure for power augmentation system |
| 06/05/2013 | CN101324205B Exhaust casing for a turbomachine |
| 06/04/2013 | US8457861 Late lean injection with adjustable air splits |
| 06/04/2013 | US8453465 Device for optimizing cooling in gas turbines |
| 06/04/2013 | US8453464 Air metering device for gas turbine engine |
| 06/04/2013 | US8453463 Anti-vortex device for a gas turbine engine compressor |
| 06/04/2013 | US8453462 Method of operating a stoichiometric exhaust gas recirculation power plant |
| 06/04/2013 | US8453461 Power plant and method of operation |
| 06/04/2013 | US8453428 Modular engine units including turbine engine with combustion mediating hub |
| 06/04/2013 | CA2817609A1 Automated tuning of gas turbine combustion systems |
| 06/04/2013 | CA2586887C Ventilating air intake arrangement |
| 06/02/2013 | CA2797209A1 Cooling system for gas turbine load coupling |
| 05/30/2013 | WO2013077861A1 System and method for anomaly detection |
| 05/30/2013 | WO2013077761A1 Airfoil with cooling passages |
| 05/30/2013 | WO2013077394A1 Combustor and gas turbine |
| 05/30/2013 | WO2013075954A1 Abradable liner for a gas turbine |
| 05/30/2013 | US20130136605 Device for locking a root of a rotor blade |
| 05/30/2013 | US20130134682 Seal arrangement and a method of repairing a seal arrangement |
| 05/30/2013 | US20130133333 Shaft break detection |
| 05/30/2013 | US20130133306 Starter Control Valve Prediction System to Predict and Trend Starter Control Valve Failures in Gas Turbine Engines Using a Starter Control Valve Health Prognostic, Computer Readable Medium and Related Methods |
| 05/29/2013 | EP2597287A1 Method for operating a stationary gas turbine with a low-calorific or medium-calorific fuel and stationary gas turbine for same |
| 05/29/2013 | EP2597286A2 Machined springs for injector applications |
| 05/29/2013 | EP2597285A2 Fuel-air mixture distribution for gas turbine engine combustors |
| 05/29/2013 | EP2597284A2 Apparatus to apply a specified texture on the surface of a turbine airfoil |
| 05/29/2013 | EP2597272A2 Thermal gradient tolerant turbomachine coupling member |
| 05/29/2013 | EP2597271A1 Combined cycle power generator |
| 05/29/2013 | EP2597269A2 Support for electric machine in a turbine engine |
| 05/29/2013 | EP2596213A2 Steam turbine with an internal cooling |
| 05/29/2013 | DE102011119521A1 Method for operating combustion engine in motor vehicle, involves switching-off individual or all cylinders of combustion engine, and adjusting lubrication oil inflow to supercharger by magnetic shut-off valve of valve apparatus |
| 05/29/2013 | CN103124833A Method for mounting shielding on a turbine casing, and mounting assembly for implementing same |
| 05/29/2013 | CN101876270B Turbine engine having cooling pin |
| 05/29/2013 | CN101626953B Aircraft leading edge |
| 05/29/2013 | CN101315033B Shroud configuration having sloped seal |
| 05/28/2013 | US8452516 Variable vane scheduling based on flight conditions for inclement weather |
| 05/28/2013 | US8448450 Support assembly for transition duct in turbine system |
| 05/28/2013 | US8448449 Fuel injector mounting system |