Patents
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)
10/2008
10/21/2008CA2353265C Metallic article with integral end band under compression and method for making
10/21/2008CA2336581C Mismatch proof variable stator vane
10/16/2008WO2008123418A1 Coating material, method for production thereof, coating method, rotor blade equipped with shroud
10/16/2008WO2008092845A3 A gas turbine
10/16/2008US20080253883 Casing
10/16/2008US20080250792 Apparatus and method of operating a gas turbine engine at start-up
10/16/2008US20080250791 Electric power station with CO2 sink and production of industrial chemicals
10/16/2008US20080250769 System and method for augmenting turbine power output
10/16/2008CA2629096A1 Flexible suspension
10/15/2008EP1980732A2 Power take-off system and gas turbine assembly including same
10/15/2008EP1980723A2 Out-flow margin protection for a gas turbine engine
10/15/2008EP1980717A2 Mixer for cooling and sealing air system for turbomachinery
10/15/2008EP1980535A2 Performance-based Control System
10/15/2008EP1979593A2 Gas turbine engine fuel system with fuel metering valve
10/15/2008CN101287898A Seal structure of gas turbine combustor
10/15/2008CN100425812C Element of turbomachinery with cool unit
10/14/2008US7435049 Sealing device and method for turbomachinery
10/14/2008US7435004 Methods and apparatus for assembling a bearing assembly
10/14/2008US7434670 Support apparatus and method for ceramic matrix composite turbine bucket shroud
10/14/2008US7434406 Drive for using a direct driven generator to start a counter-rotating multi-spool gas turbine engine
10/14/2008US7434404 Method for operating a gas turbine combustion chamber including a plurality of burners arranged in groups
10/14/2008US7434403 Method of operating a thermal power plant
10/14/2008US7434402 System for actively controlling compressor clearances
10/14/2008US7434401 Fuel/air premixer for gas turbine combustor
10/14/2008CA2335355C Igniter with porous sleeve
10/09/2008WO2008120648A1 Discharge surface treatment method and repairing method
10/09/2008WO2008059168A3 Acoustic lining for an aircraft, including a frost treatment system using the joule effect
10/09/2008US20080247885 West Compression Apparatus and Method
10/09/2008US20080247865 Device and Method for Axially Displacing a Turbine Rotor
10/09/2008US20080245337 System for reducing combustor dynamics
10/09/2008US20080245074 Combustor of a gas turbine engine
10/09/2008US20080245073 Gas turbine engine
10/09/2008US20080245072 Damping of Vibration of a Combustion Chamber By Resonators
10/09/2008US20080245062 Passive cooling system for auxiliary power unit installation
10/09/2008US20080245051 Means for cooling a bearing assembly
10/08/2008EP1978307A2 Combustor of a gas turbine engine
10/08/2008EP1978224A2 Fuel system
10/08/2008EP1978222A2 Particle separator and debris control system
10/08/2008EP1978221A2 Front part of a turbomachine comprising a system for deflecting foreign bodies, such as hailstones
10/08/2008EP1978209A2 Vortex spoiler for delivery of cooling airflow in a turbine engine
10/08/2008EP1629179B1 Turbofan jet engine turbine case cooling valve
10/08/2008CN101283221A Process and device for monitoring the formation of deposits of solid particles, in particular in a fuel line and in the fuel valves of a gas turbine
10/08/2008CN101280726A Power output system and gas turbine assembly including same
10/08/2008CN101280725A Side combustion type rotor internal combustion engine
10/08/2008CN101280724A Backheating type small size gas turbine
10/08/2008CN101280723A Method and device for reutilization of natural gas pipe network pressure energy in gas turbine working domain
10/08/2008CN101280694A Thermal insulation board, bearing casing and turbo casing for exhaust-gas-turbine, and exhaust-gas-turbine
10/08/2008CN100424416C Cooling structure of gas turbine tail pipe
10/07/2008US7431569 Pump health monitoring
10/07/2008US7431197 Method of fabricating a hollow mechanical part by diffusion welding and superplastic forming
10/07/2008US7430869 System for catalytic combustion
10/07/2008US7430868 Method of operating a thermal power plant
10/07/2008US7430852 Turbojet having a large bypass ratio
10/07/2008US7430851 Air and fuel venting device for fuel injector nozzle tip
10/07/2008US7430850 Bifurcated oil scavenging bearing compartment within a gas turbine engine
10/07/2008CA2430285C Device for centring a tube in a turbine shaft
10/07/2008CA2347711C Isolated oil feed pipe
10/07/2008CA2332359C Gas turbine fuel injector
10/03/2008CA2627380A1 Power take-off system and gas turbine engine assembly including same
10/02/2008WO2008118264A1 Acoustic septum cap honeycomb
10/02/2008WO2008117802A1 Heat resistant component
10/02/2008WO2008116923A1 Cleaning device
10/02/2008WO2008116922A2 Housing insulator
10/02/2008WO2008116291A1 Oil scavenge system having churning damper for gas turbine engines
10/02/2008WO2008085542A3 Aircraft engine inlet having zone of deformation
10/02/2008WO2008041964A3 Infrared suppression system
10/02/2008US20080240914 Intermediate casing for a gas turbine engine
10/02/2008US20080236170 Transition-to turbine seal apparatus and transition-to-turbine seal junction of a gas turbine engine
10/02/2008US20080236169 Combustor floating collar with louver
10/02/2008US20080236165 Dual-injector fuel injector system
10/02/2008US20080236133 Turbomachine front portion comprising a deflector system for deflecting foreign bodies, such as hailstones
10/02/2008DE102008016306A1 Einrichtung zum Erwärmen eines Fluids Means for heating a fluid
10/02/2008DE102007014667A1 Gasturbine Gas turbine
10/02/2008DE102007001024B4 Verfahren zur rechnergestützten Regelung und/oder Steuerung eines technischen Systems insbesondere einer Gasturbine Method for computer-aided regulation and / or control of a technical system, in particular a gas turbine
10/01/2008EP1975389A2 Methods and systems for output variance and facilitation of maintenance of multiple gas turbine plants
10/01/2008EP1975388A1 Gas turbine engine with fuel booster
10/01/2008EP1975379A2 Oil scavenge system having churning damper for gas turbine engines
10/01/2008EP1974139A1 Fuel ratio control in a combustion apparatus with multiple fuel supply lines
10/01/2008EP1973779A1 Dual flow turbine engine equipped with a precooler
10/01/2008EP1973778A1 Dual flow turbine engine equipped with a precooler
10/01/2008CN201125787Y Airplane engine starting and automatic oil switching apparatus
10/01/2008CN201125786Y Gas turbine water injection pump integration apparatus
10/01/2008CN101277871A Engine assembly for an aircraft comprising an engine as well as an engine mounting structure for such an engine
10/01/2008CN101275482A Apparatus for heating a fluid
10/01/2008CN101274746A Reforming system for combined cycle plant with partial CO2 capture
10/01/2008CN100423440C Method and apparatus for starting a gas turbine using a polyphase electric power generator
10/01/2008CN100422645C Multiport dome baffle
10/01/2008CN100422541C Exhaust-gas-turbine casing
10/01/2008CN100422508C Turbine airfoil trailing edge repair and methods therefor
09/2008
09/30/2008US7429403 Gas distributor for vapor coating method and container
09/30/2008US7429350 Target for vaporizing under an electron beam, a method of fabricating it, a thermal barrier and a coating obtained from a target, and a mechanical part including such a coating
09/30/2008US7429174 Clean atmosphere heat treat for coated turbine components
09/30/2008US7428819 Method for the operation of a compressor of a gas turbine with evaporative cooling of the compressor induction air
09/30/2008US7428818 System and method for augmenting power output from a gas turbine engine
09/30/2008US7428815 Method of operating a compressor near the compressor pumping limit and compressor
09/30/2008CA2626907A1 Turbine engine nose including a system for deflecting foreign bodies, such as hailstones
09/30/2008CA2498057C Gas turbine sealing air supply system
09/30/2008CA2377280C Fuel and oil system for a gas turbine
09/27/2008CA2626978A1 Support dampers for bearing assemblies and methods of manufacture
09/26/2008CA2627112A1 Vortex spoiler for delivery of cooling airflow in a turbine engine