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)
08/2002
08/20/2002US6434945 Dual fuel nozzle
08/20/2002US6434924 Ramjet engine for power generation
08/20/2002CA2263642C Seal structure for gas turbines
08/15/2002WO2002063214A1 A method and a device for supplying fuel to a combustion chamber
08/15/2002WO2002063156A1 Bulkhead for dual fuel industrial and aeroengine gas turbines
08/15/2002WO2002063153A1 Uniaxial gas turbine system
08/15/2002WO2002035072A3 Nested core gas turbine engine
08/15/2002WO2001040548A9 Chemical cleaning solution for gas turbine blades
08/15/2002US20020110454 Gas turbine blade and method for producing a gas turbine blade
08/15/2002US20020110451 Methods and apparatus for reducing seal teeth wear
08/15/2002US20020109304 Turbine rotor-stator leaf seal and related method
08/15/2002US20020108809 Engine intake silencer
08/15/2002US20020108379 Gas turbine
08/15/2002US20020108378 Liner supporting structure for annular combuster
08/15/2002US20020108376 Thermal management system for turbomachinery
08/14/2002EP1231420A2 Methods and apparatus for reducing seal teeth wear
08/14/2002EP1231369A2 Gas turbine control system compensating water content in combustion air
08/14/2002EP1231368A1 Two level pressurisation valve driven by a fuel metering device
08/14/2002EP1231010A1 Transient liquid phase bonding repair for turbine blades and vanes
08/14/2002EP1230323A1 System and method for oil fuel burning integrated combined cycle power generation
08/14/2002EP0875721B1 Spring seal unit of combustor
08/13/2002US6432487 Applying layers of thermal barrier coating on component, utilizing nozzle at first distance from component; applying outer layer of thermal barrier coating on component, with nozzle at second distance from component
08/13/2002US6432478 Ceramic heat barrier coating having low thermal conductivity, and process for the deposition of said coating
08/13/2002US6431833 Gas turbine bucket with impingement cooled platform
08/13/2002US6431824 Turbine nozzle stage having thermocouple guide tube
08/13/2002US6431820 Methods and apparatus for cooling gas turbine engine blade tips
08/13/2002US6431255 Ceramic shell mold provided with reinforcement, and related processes
08/13/2002US6430931 Gas turbine in-line intercooler
08/13/2002US6430914 Combined cycle power generation plant and method of operating such a plant
08/13/2002CA2252658C Columnar zirconium oxide abrasive coating for a gas turbine engine seal system
08/08/2002WO2002061337A1 Burner unit and method for operation thereof
08/08/2002WO2002050618A3 Microturbine/capacitor power distribution system
08/08/2002US20020106292 High pressure water pump
08/08/2002US20020106001 System and method for determining gas turbine firing and combustion reference temperatures having correction for water content in fuel
08/08/2002US20020104317 Method of operation of gas turbine engine
08/08/2002US20020104316 Ultra low emissions gas turbine cycle using variable combustion primary zone airflow control
08/08/2002US20020104308 Turbine engine control system providing electronic power turbine governor and temperature/torque limiting
08/08/2002DE10102606A1 Kühlung von Gehäusen, Rotor, Schaufeln und/oder Brennern von Turbinen Cooling of housings, rotor blades and / or turbine burners
08/07/2002EP1229146A2 Oxidation resistant coatings for niobium-based silicide composites
08/07/2002EP1228293A1 Turbine blade and method for producing a turbine blade
08/07/2002EP1227905A1 Multipiece core assembly for cast airfoil
08/07/2002EP1032791B1 Combustion chamber and method for cooling a combustion chamber with vapour
08/07/2002CN1088809C Retaining arrangement for a bearing, in particular for a high pressure compressor shaft
08/06/2002US6428683 Comprises stripping tank containing an electrolyte bath for removing a coating from workpiece (air foil), rinse tank, and distillation unit for receiving electrolyte containing dissolved metals
08/06/2002US6428270 Stage 3 bucket shank bypass holes and related method
08/06/2002US6428269 Turbine engine bearing support
08/06/2002US6427752 Casting systems and methods with auxiliary cooling onto a liquidus portion of a casting
08/06/2002US6427447 Bulkhead for dual fuel industrial and aeroengine gas turbines
08/06/2002US6427435 Retainer segment for swirler assembly
08/06/2002US6427434 Device for discharging hot air for a jet engine air inlet cowl, with a deicing circuit
08/06/2002US6427327 Method of modifying cooled turbine components
08/01/2002WO2002059474A2 Assembly and method for fan noise reduction from turbofan engines using dynamically adaptive herschel-quincke tubes
08/01/2002WO2002059469A1 Turbine engine
08/01/2002WO2002044538A3 Device for centring a tube in a turbine shaft
08/01/2002US20020102409 Attaching a foil which comprises the bond coating to the substrate surface, and then fusing the foil to the substrate surface, so that the bond coating adheres to the substrate.
08/01/2002US20020102160 Gas turbine engine nose cone
08/01/2002CA2435116A1 Turbine engine
07/2002
07/31/2002EP1227325A1 Sensor for speed and vibration
07/31/2002EP1227255A2 Bi-directional tapered roller bearing
07/31/2002EP1227222A2 Utilization of pyrometer data to detect oxidation
07/31/2002EP1227217A2 Gas turbine
07/31/2002EP1227036A2 A gas turbine engine nose cone
07/31/2002EP1084337B1 Oil supply system for a gas turbine
07/31/2002CN1361350A Cooling system and method for cooling fluid mechanical shell
07/30/2002US6425943 Centrifugally ejecting heavier-than-air particles within air precleaner; pollution control
07/30/2002US6425736 Stator assembly for a rotary machine and method for making the stator assembly
07/30/2002US6425241 Pyrometer mount for a closed-circuit thermal medium cooled gas turbine
07/30/2002CA2250169C Cooled stationary blade of gas turbine
07/30/2002CA2233821C Gas turbine cooled moving blade
07/25/2002WO2002057632A2 High pressure water pump
07/25/2002WO2001076348A3 Improved brush-seal designs for turbines and similar rotary apparatus
07/25/2002US20020098776 Method and device for treating the surface of a part
07/25/2002US20020098294 Method of providing a protective coating on a metal substrate, and related articles
07/25/2002US20020098082 Gas turbine
07/25/2002US20020096197 Methods and apparatus for washing gas turbine engines
07/25/2002US20020095940 Gas turbine having a cooling air system and a spray air system
07/25/2002US20020095937 Combustion turbine cooling media supply system and related method
07/25/2002US20020095936 Fuel divider and ecology system for a gas turbine engine
07/24/2002EP1225392A2 Combustor mixer having plasma generating nozzle
07/24/2002EP1225322A1 Apparatus to centre a tube in a turbine shaft
07/24/2002EP1225307A2 Methods and apparatus for washing gas turbine engines
07/24/2002EP1225306A1 Control system and method for gas turbine inlet-air water-saturation and supersaturation system
07/24/2002EP1224382A1 Bearing housing for a turbomachine
07/24/2002EP0931214B1 Method for thermoregulating inlet air, and thermostat needed for its application
07/24/2002CN1360660A Turbo engine with rotor sealing system, especially gas turbine
07/23/2002US6423432 High temperature corrosion-resistant and abrasion-resistant coating member, and manufacturing method thereof
07/23/2002US6422817 Cooling circuit for and method of cooling a gas turbine bucket
07/23/2002US6422811 Cooling arrangement for blades of a gas turbine
07/23/2002US6422810 Exit chimney joint and method of forming the joint for closed circuit steam cooled gas turbine nozzles
07/23/2002US6422807 Turbine inner shell heating and cooling flow circuit
07/23/2002US6422023 Turbine engine control with electronic and pneumatic governors
07/23/2002US6422022 Apparatus and methods for supplying auxiliary steam in a combined cycle system
07/23/2002US6422021 Fuel divider and ecology system for a gas turbine engine
07/23/2002US6422020 Cast heat exchanger system for gas turbine
07/23/2002US6422019 Apparatus for augmenting power produced from gas turbines
07/23/2002US6422018 Gas turbine engine modular cooling and heating apparatus
07/18/2002WO2002055754A2 Method and device for gas phase diffusion coating of metal components
07/18/2002US20020092423 Methods for filtering air for a gas turbine system
07/18/2002US20020092303 Methods and apparatus for supplying air to turbine engine combustors
07/18/2002US20020092302 Combustor mixer having plasma generating nozzle