| 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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| 09/16/2010 | CA2754175A1 Device for driving a pair of counter-rotating propellers by means of an epicyclic gear train |
| 09/16/2010 | CA2754090A1 Rotor element with a fluid passage and passage-blocking member, and turbine engine including the rotor element |
| 09/15/2010 | EP2228525A1 Gas turbine controlling method, and gas turbine power generating apparatus |
| 09/15/2010 | EP2228515A2 Two-shaft gas turbine system |
| 09/15/2010 | EP2227624A2 Methods and systems for generating power from a turbine using pressurized nitrogen |
| 09/15/2010 | CN201581996U Gas turbine generator set box-packaging body |
| 09/15/2010 | CN201581995U Hot-gas turbine |
| 09/15/2010 | CN1877101B Gas turbine, method of controlling air supply and computer program product for controlling air supply |
| 09/15/2010 | CN1573018B 蒸汽涡轮机 Steam turbine |
| 09/15/2010 | CN101832183A Low heating value fuel gas blending control |
| 09/15/2010 | CN101832182A Synthesis gas humidifier and heating and humidifying method |
| 09/15/2010 | CN101832181A Novel film cooling hole with anti-whorl hole branch structure |
| 09/15/2010 | CN101832154A Method for cooling air film of turbine blade of aircraft engine |
| 09/15/2010 | CN101307721B Motor drive rotating combustion-chamber assembly outer compression double-modes runner engine |
| 09/14/2010 | US7793507 Expansion joint for gas turbines |
| 09/14/2010 | CA2464253C In-situ method and composition for repairing a thermal barrier coating |
| 09/14/2010 | CA2389531C Variable cycle propulsion device employing mechanical transmission for supersonic aircraft |
| 09/09/2010 | US20100226757 Instrumented component for combustion turbine engine |
| 09/09/2010 | US20100226755 Turbine Vane for a Gas Turbine Engine Having Serpentine Cooling Channels Within the Outer Wall |
| 09/09/2010 | US20100223931 Pattern cooled combustor liner |
| 09/09/2010 | US20100223905 Scoop of a running-gap control system of an aircraft gas turbine |
| 09/09/2010 | US20100223902 Thermoelectrically cooled components for distributed electronics control system for gas turbine engines |
| 09/09/2010 | DE102009012252A1 Abgasturbolader Exhaust gas turbocharger |
| 09/09/2010 | DE102009011635A1 Luftleitelement eines Laufspalteinstellungssystems einer Fluggasturbine Air directing a running gap adjustment system of an aircraft gas turbine |
| 09/08/2010 | EP2226473A2 Air guiding element of a system for tip clearance adjustment of an aero gas turbine |
| 09/08/2010 | EP2225156A1 Aircraft propulsion assembly comprising hot air bleed systems |
| 09/08/2010 | CN201572462U Fire prevention self-rescue device of Fire-fighting turbojet engine |
| 09/08/2010 | CN101825018A A system and method for heating a fuel using a solar heating system |
| 09/08/2010 | CN101463764B High-energy plasma igniter of gas turbine |
| 09/08/2010 | CN101280725B Side combustion type rotor internal combustion engine |
| 09/07/2010 | US7789125 Extended impingement cooling device and method |
| 09/07/2010 | US7788932 Seal structure for gas turbine combustor |
| 09/07/2010 | US7788926 Resonator device at junction of combustor and combustion chamber |
| 09/07/2010 | US7788898 Variable coupling of turbofan engine spools via open differential gear set or simple planetary gear set for improved power extraction and engine operability, with torque coupling for added flexibility |
| 09/07/2010 | CA2487604C Method for repairing coated components |
| 09/02/2010 | WO2010099535A2 Liquid-gas heat exchanger |
| 09/02/2010 | WO2010099193A2 Improved air riding seal |
| 09/02/2010 | WO2010098003A1 Thrust bearing lubrication nozzle |
| 09/02/2010 | WO2010097427A1 Device and method for controlling a turbine fitted with a plurality of burners for liquid or gaseous fuel |
| 09/02/2010 | WO2010019177A3 Transition with a linear flow path with exhaust mouths for use in a gas turbine engine |
| 09/02/2010 | US20100219638 Turbomachinery Electric Generator Arrangement |
| 09/02/2010 | US20100218509 Combustion chamber |
| 09/02/2010 | US20100218508 System for supporting and servicing a gas turbine engine |
| 09/02/2010 | US20100218507 Sustainable Carbon Capture and Sequestration System and Methods |
| 09/02/2010 | US20100218504 Annular rich-quench-lean gas turbine combustors with plunged holes |
| 09/02/2010 | US20100218503 Plunged hole arrangement for annular rich-quench-lean gas turbine combustors |
| 09/02/2010 | US20100218501 Premixed direct injection disk |
| 09/02/2010 | DE102009010310A1 Loading device, particularly turbo-supercharger for motor vehicle, has turbine housing and compressor housing, where compressor housing is formed by inner shell and outer shell |
| 09/02/2010 | DE102009010110A1 Erosionsschutz-Beschichtungssystem für Gasturbinenbauteile Erosion-resistant coating system for gas turbine components |
| 09/02/2010 | CA2692068A1 Variable drive gas turbine engine |
| 09/01/2010 | EP2224171A1 Combustion burner |
| 09/01/2010 | EP2224167A1 Gas turbine casing |
| 09/01/2010 | EP2224113A2 Isothermic delivery of a cooling fluid through a passageway |
| 09/01/2010 | EP2224100A2 Controlled fan stream flow bypass |
| 09/01/2010 | EP2222944A2 Sequential combustion firing system for a fuel system of a gas turbine engine |
| 09/01/2010 | EP2222560A1 Aircraft nacelle guidance system installation |
| 09/01/2010 | CN101821489A Method for repairing turbine rotor blade |
| 09/01/2010 | CN101821481A Turbomachine |
| 09/01/2010 | CN101818690A Gas turbine combustion system cooling arrangement |
| 09/01/2010 | CN101818689A Filter retention system |
| 09/01/2010 | CN101818661A Catenary turbine seal systems |
| 09/01/2010 | CN101372915B Single element miniature turbogenerating system |
| 09/01/2010 | CN101057104B Burner starting method |
| 08/31/2010 | US7785671 metal substrate, metal bonding layer, ceramics thermal barrier; columnar structure of stabilized zirconia, or ZrO2-HfO2 solid solution; simultaneously melting two ZrO2 deposition and Lanthanum oxide deposition materials by electron beam physical vapor deposition; low thermal conductivity; durability |
| 08/31/2010 | US7785401 Fluid separation device |
| 08/31/2010 | US7784287 Pulse detonation firing detuning and frequency modulated firing |
| 08/31/2010 | US7784286 Method and apparatus for achieving power augmentation in gas turbines using wet compression |
| 08/31/2010 | US7784262 Exhaust gas guide of a gas turbine and method for mixing the exhaust gas of the gas turbine |
| 08/27/2010 | CA2693625A1 Bearing damper with spring seal |
| 08/26/2010 | WO2010096087A1 Magnetic advanced generation jet electric turbine |
| 08/26/2010 | WO2010094878A2 Engine mounting with an adapted load/deformation curve |
| 08/26/2010 | WO2010094574A1 Device for restricting the throughflow quantity at a pump, and pump arrangement having a device of this type |
| 08/26/2010 | US20100215558 Method and apparatus for operation of co/voc oxidation catalyst to reduce no2 formation for gas turbine |
| 08/26/2010 | US20100215507 Mounting arrangement |
| 08/26/2010 | US20100215479 Gas turbine engine inlet with noise reduction features |
| 08/26/2010 | US20100215476 Gas turbine combustion system cooling arrangement |
| 08/26/2010 | US20100213290 Nozzle repair to reduce fretting |
| 08/26/2010 | US20100212326 Powerplant and a method of driving a mechanical system via said powerplant |
| 08/26/2010 | US20100212325 Combustion system |
| 08/26/2010 | US20100212324 Dual walled combustors with impingement cooled igniters |
| 08/26/2010 | US20100212322 Coaxial fuel and air premixer for a gas turbine combustor |
| 08/26/2010 | DE202010005708U1 Brennkraftmaschine mit Zylinderkopf und Turbine Internal combustion engine with cylinder head and turbine |
| 08/26/2010 | DE112008002730T5 Vorrichtung zum Unterbinden einer Ölströmung entlang einer sich drehenden Welle Apparatus for inhibiting oil flow along a rotating shaft |
| 08/26/2010 | DE112008002729T5 Turbomaschine Turbomachine |
| 08/26/2010 | DE102009010611A1 Vorrichtung und Verfahren zur Steuerung einer mit mehreren Brennern ausgestatteten Turbine für flüssige oder gasförmige Brennstoffe Apparatus and method for controlling a turbine equipped with multiple burners for liquid or gaseous fuels |
| 08/26/2010 | DE102009010311A1 Charging device i.e. exhaust turbo-supercharger, for internal-combustion engine of motor vehicle, has gap formed between inner shell and outer shell and partially and/or section-wise evacuated for reduction of thermal conduction |
| 08/26/2010 | DE102009010185A1 Gasturbinenmaschine Gas turbine engine |
| 08/25/2010 | EP2221247A2 Mounting arrangement for a nose cone of a gas turbine engine |
| 08/25/2010 | EP2219947A2 Ice protection system for a multi-segment aircraft component |
| 08/25/2010 | CN201560852U Natural gas front device of gas turbine |
| 08/25/2010 | CN101815853A A turbocharger bearing assembly and lubrication thereof |
| 08/25/2010 | CN101813028A Gas turbine ejector and method of operation |
| 08/25/2010 | CN101813027A Bump air inlet method for realizing integration of unequal-strength wave system with forebody |
| 08/25/2010 | CN101014686B Gas reforming equipment |
| 08/24/2010 | US7780401 Ice strike sheathing ring for the fan casing of an aircraft gas turbine |
| 08/24/2010 | US7779541 Method for manufacturing a stator or rotor component |
| 08/24/2010 | CA2519842C Thermal barrier coating material |
| 08/20/2010 | CA2693528A1 Nozzle repair to reduce fretting |
| 08/20/2010 | CA2693527A1 Nozzle design to reduce fretting |
| 08/20/2010 | CA2692745A1 Compressor wash nozzle integrated in an inlet case strut |