| 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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| 01/23/2013 | CN102889133A Gas-leading sealing structure of gas turbine |
| 01/23/2013 | CN102889132A Starting device of gas turbine engine |
| 01/23/2013 | CN102889130A Gas turbine set of indirect cooling female pipe type split type air compressor |
| 01/23/2013 | CN101539057B Air intake for a turboshaft engine equipped with a controlled filtering system |
| 01/22/2013 | US8356486 APU bleed valve with integral anti-surge port |
| 01/22/2013 | US8356485 System and method for oxygen separation in an integrated gasification combined cycle system |
| 01/22/2013 | US8356484 Hybrid Wobbe control during rapid response startup |
| 01/22/2013 | US8356467 Combustion wave ignition for combustors |
| 01/22/2013 | CA2703108C Passive cooling system for auxiliary power unit installation |
| 01/22/2013 | CA2685514C Method of starting turbine engine from low engine speed |
| 01/22/2013 | CA2665353C Multi-channel fuel manifold |
| 01/22/2013 | CA2502816C Forced air cooling system |
| 01/22/2013 | CA2500963C Air intake structure for aircraft engine |
| 01/17/2013 | WO2013009177A1 Improved diverter damper |
| 01/17/2013 | WO2013007937A2 Method for manufacturing a turbine-engine fan casing having an acoustic coating |
| 01/17/2013 | WO2013007912A1 Method for starting a turbomachine that reduces the thermal imbalance |
| 01/17/2013 | WO2013007824A1 Compressor blade with nozzle |
| 01/17/2013 | WO2013007463A1 A rotor train for a turbine system |
| 01/17/2013 | US20130014515 Link between the exhaust casing and a structural ring of the fan duct of a jet engine |
| 01/17/2013 | US20130014514 Systems and methods for bulk temperature variation reduction of a gas turbine through can-to-can fuel temperature modulation |
| 01/17/2013 | US20130014512 Ceramic Matrix Composite Combustor Vane Ring Assembly |
| 01/17/2013 | DE19680223B3 Verfahren zum Schutz eines Wärmesperren-Überzuges und entsprechendes Bauteil A method for protecting a thermal barrier coating and corresponding component |
| 01/17/2013 | DE102012013048A1 Fluid-flow machine for supplying compressed air to fuel cell of fuel cell arrangement of passenger car, has compressor fluidly connected with branch line at branching point that is arranged at downstream of compressor wheel |
| 01/17/2013 | CA2839817A1 Method for starting a turbomachine that reduces the thermal imbalance |
| 01/16/2013 | EP2546575A2 Systems and methods for bulk temperature variation reduction of a gas turbine through can-to-can fuel temperature modulation |
| 01/16/2013 | EP2546494A1 Assembly method for a gas turbine fan drive gear system |
| 01/16/2013 | EP2546493A2 Contained shaft spring load |
| 01/16/2013 | EP2546466A1 Shaft seal device and rotary machine with shaft seal device |
| 01/16/2013 | EP2546459A1 A rotor train for a turbine system |
| 01/16/2013 | CN202675358U Mixing device, combustion chamber and aeroengine |
| 01/16/2013 | CN202674142U Extrusion oil film damper |
| 01/16/2013 | CN202673456U Windward differential pressure type plasma ignition burner |
| 01/16/2013 | CN202673455U Spiral-flow type plasma ignition mouth |
| 01/16/2013 | CN202673454U Inlet protective screen cover |
| 01/16/2013 | CN202673453U Power transmitting mechanism for compressor and turbine |
| 01/16/2013 | CN102883872A Seamless acoustic liner |
| 01/16/2013 | CN102877983A Multistage hydraulic jet engine for military use |
| 01/16/2013 | CN102877948A Systems and methods for bulk temperature variation reduction of a gas turbine through can-to-can fuel temperature modulation |
| 01/16/2013 | CN102877947A Rotatable power-plant case section |
| 01/16/2013 | CN102877946A Back heating type electric drive multi-compressor main pipeline combustion gas turbine |
| 01/16/2013 | CN102877945A Variable working condition analysis method for gas turbine and combined cycle thereof based on resolving method |
| 01/16/2013 | CN102203475B Fluid valve drive mechanism |
| 01/15/2013 | US8355855 Systems and methods for controlling an integrated drive train |
| 01/15/2013 | US8355819 Method, apparatus and system for igniting wide range of turbine fuels |
| 01/15/2013 | US8353306 Fuel divider system for gas turbine engine |
| 01/15/2013 | US8353166 Gas turbine combustor and fuel manifold mounting arrangement |
| 01/15/2013 | US8353163 Fuel injector sans support/stem |
| 01/15/2013 | CA2770756A1 Connection for generator in a gas turbine engine |
| 01/15/2013 | CA2703166C Passive cooling system for auxiliary power unit installation |
| 01/15/2013 | CA2532605C Tube heat shield and method of making same |
| 01/15/2013 | CA2503066C Turbine ring |
| 01/15/2013 | CA2469849C Combustion chamber having a flexible liaison between the chamber floor and chamber wall |
| 01/10/2013 | WO2013006410A2 Method and apparatus for distributed cleft and liberated tile detection achieving full coverage of the turbine combustion chamber |
| 01/10/2013 | WO2013006083A1 Gas turbine arrangement for a locomotive |
| 01/10/2013 | WO2013004964A1 Turbine engine drive shaft device |
| 01/10/2013 | WO2013004958A1 Gas turbine auxiliaries relay gearbox incorporating uncoupling means |
| 01/10/2013 | WO2013004451A1 Hydraulic bearing for a stationary gas turbine |
| 01/10/2013 | WO2012022551A3 Steam turbine comprising an internal cooling arrangement |
| 01/10/2013 | US20130008180 Method and apparatus for distributed cleft and liberated tile detection achieving full coverage of the turbine combustion chamber |
| 01/10/2013 | US20130008179 Ultra high temperature circuit coupling |
| 01/10/2013 | US20130008178 Support assembly for transition duct in turbine system |
| 01/10/2013 | US20130008177 Support assembly for transition duct in turbine system |
| 01/10/2013 | US20130008176 Gas turbine shroud arrangement |
| 01/10/2013 | US20130008174 Method and controller for detecting ice |
| 01/10/2013 | US20130008173 Power generation assembly and method |
| 01/10/2013 | US20130008172 Systems and Methods for Modified Wobbe Index Control With Constant Fuel Temperature |
| 01/10/2013 | US20130008169 Apparatus and systems relating to fuel injectors and fuel passages in gas turbine engines |
| 01/10/2013 | US20130008168 Burner for stabilizing the combustion of a gas turbine |
| 01/10/2013 | US20130008167 Gas turbine combustor |
| 01/10/2013 | DE102012106057A1 Mehrschichtiger Filter, Gasturbine mit einem mehrschichtigen Filter und Filterungsverfahren A multilayer filter, gas turbine having a multi-layer filter and filtering method |
| 01/10/2013 | DE102012013160A1 Labyrinthdichtungen Labyrinth seals |
| 01/10/2013 | DE102011106965A1 Fluggasturbinentriebwerk mit Wärmetauscher im Kerntriebwerksgehäuse Aircraft gas turbine engine with heat exchanger in the core engine housing |
| 01/10/2013 | DE102011106961A1 Flight gas turbine engine i.e. turbomachine, has flow guide element designed as radiator element, and core thruster surrounded by by-pass channel, where partial flow is conducted from channel through engine casing for cooling core thruster |
| 01/10/2013 | CA2840543A1 Gas turbine auxiliaries relay gearbox incorporating uncoupling means |
| 01/10/2013 | CA2838919A1 Turbine engine drive shaft device |
| 01/10/2013 | CA2834057A1 Gas turbine arrangement for a locomotive |
| 01/09/2013 | EP2543931A1 Apparatus and systems relating to fuel injectors and fuel passages in gas turbine engines |
| 01/09/2013 | EP2543868A2 Turbofan engine |
| 01/09/2013 | EP2543864A2 Aircraft propulsion assembly with a heat shield for thermal protection of a rear aerodynamic fairing of a pylon and a cooling method for the heat shield |
| 01/09/2013 | EP2543853A2 Systems and methods for modified wobbe index control with constant fuel temperature |
| 01/09/2013 | EP2543852A2 Method for assessing the performance of auxiliary power unit |
| 01/09/2013 | EP2543851A1 Gas turbine engine |
| 01/09/2013 | EP2543832A1 Hydraulic bearing for a stationary gas turbine |
| 01/09/2013 | EP2543829A2 Fan Stagger Angle for Dirt Rejection |
| 01/09/2013 | EP2543600A2 Sound absorber for an auxiliary engine of an aircraft |
| 01/09/2013 | EP2542471A2 Engine nacelle comprising an equipment cooling device |
| 01/09/2013 | EP2542401A2 Seamless acoustic liner |
| 01/09/2013 | CN202659351U 进口锥 Imported Cone |
| 01/09/2013 | CN202659350U Asynchronous injection compensation diffuser |
| 01/09/2013 | CN102865148A Method of controlling gas turbine |
| 01/09/2013 | CN102865146A Systems and methods for modified wobbe index control with constant fuel temperature |
| 01/09/2013 | CN102865145A Support assembly for a turbine system and corresponding turbine system |
| 01/09/2013 | CN102865144A Hinge seal |
| 01/09/2013 | CN102865143A Lubrication systems with nozzle blockage detection systems |
| 01/09/2013 | CN102865142A Multi-layer filter, gas turbine including a multi-layer filter, and process of filtering |
| 01/09/2013 | CN102865139A Runoff jet flow heat power system |
| 01/08/2013 | US8350398 Aeroengine starter/generator arrangement |
| 01/08/2013 | US8348180 Conical swirler for fuel injectors and combustor domes and methods of manufacturing the same |
| 01/08/2013 | US8347635 Locking apparatus for a radial locator for gas turbine engine mid turbine frame |
| 01/08/2013 | US8347633 Gas turbine engine with variable geometry fan exit guide vane system |