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)
02/2001
02/13/2001US6186217 Multipiece core assembly
02/13/2001US6185924 Gas turbine with turbine blade cooling
02/08/2001WO2001009694A1 Method and system for diagnosing a technical installation
02/08/2001WO2001009553A1 Baffle cooling device
02/08/2001WO2001009497A1 Gas turbine apparatus with an aerodynamic labyrinth seal
02/08/2001WO2001009403A1 High-temperature part and method for producing the same
02/08/2001WO2000053908A8 Gas turbine engine
02/08/2001WO2000053907A8 Method of operation of a gas turbine engine power plant and a gas turbine engine power plant
02/07/2001EP1074791A2 Piping support of gas turbine steam cooled combustor
02/07/2001EP1074708A1 Gas-liquid separating apparatus
02/07/2001EP1074699A2 Turbine-generator system
02/07/2001EP1074698A2 A lubricating coating for tubes in gas turbines
02/07/2001EP1074694A2 Apparatus and methods for cooling rotary components in a turbine
02/07/2001EP1074331A1 Method for repairing superralloy castings using a metallurgically bonded tapered plug
02/07/2001EP1073832A1 Turbine engine with cooled p3 air to impeller rear cavity
02/07/2001EP1073828A1 Containment system for containing blade burst
02/07/2001CN1061734C Method for adjusting rotation speed of gas turbine when load is cut off
02/06/2001US6183388 Epicyclic face gear reduction gearbox particularly for a gas turbine engine
02/06/2001US6183194 Cooling circuits for trailing edge cavities in airfoils
02/06/2001US6183193 Cast on-board injection nozzle with adjustable flow area
02/06/2001US6182787 Rigid sandwich panel acoustic treatment
02/06/2001US6182438 Method and apparatus for starting a gas turbine engine
02/06/2001US6182437 Fuel injector heat shield
02/06/2001US6182435 Thermal and energy management method and apparatus for an aircraft
02/01/2001WO2001007767A1 Draining device for the fuel supply system of a gas turbine engine
02/01/2001WO2001007766A1 Fuel divider and ecology system for a gas turbine engine
02/01/2001WO2001007765A1 A method and apparatus for vaporizing liquid gas in a combined cycle power plant
02/01/2001DE19936170A1 Cooling air pipe for aircraft gas turbine engine consists of double-walled three-part pipe with inner tube for cooling air flow
02/01/2001DE19934927A1 Verfahren zum Kühlen von Leit- und/oder Laufschaufeln in den Turbinenstufen einer Gasturbinenanlage sowie Gasturbinenanlage zur Durchführung des Verfahrens A method for cooling control and / or blades in the turbine stages of a gas turbine plant and gas turbine system for implementing the method
02/01/2001DE19933445A1 Dichtring für nicht- hermetische Fluiddichtungen Sealing ring for non-hermetic fluid seals
02/01/2001DE19843615C2 Vorrichtung und Verfahren zur Diagnose von Verbrennungsantrieben Device and method for the diagnosis of internal combustion engines
01/2001
01/31/2001EP1072772A1 Fuel cell power generating module and method for controlling the fuel cell pressure
01/31/2001EP1072758A2 Method for cooling gas turbine blades
01/31/2001EP1071872A1 Anti-coking fuel injector purging device
01/31/2001EP1071867A1 Method of generating power using an advanced thermochemical recuperation cycle
01/31/2001EP1071831A1 Method for producing fibre reinforced metallic components
01/31/2001EP1071608A2 Biplanar scarfed nacelle inlet
01/30/2001US6180262 Thermal coating composition
01/30/2001US6179556 Turbine blade tip with offset squealer
01/30/2001US6179554 Low friction fluid bearing and turbine using same
01/30/2001US6179251 Thin inlet lip design for low drag and reduced nacelle size
01/30/2001US6178751 Liquid fuel injector system
01/30/2001US6178738 Method of operating a gas-turbine group by directing a fuel/water mixture to the combustion chamber
01/30/2001US6178736 Turbine aircraft engine starting method
01/30/2001US6178735 Combined cycle power plant
01/30/2001US6178734 Combined cycle power generation plant and operating method thereof
01/30/2001US6178733 External blower motor and starting motor for a combustion turbine system
01/25/2001WO2001006097A1 Sealing ring for non-hermetic fluid seals
01/25/2001WO2001005579A2 One-step noble metal-aluminide coatings
01/24/2001EP1071072A2 Acoustic liner and method of making an acoustic liner
01/23/2001US6177038 Method for orienting an airfoil for processing and for forming a mask for the airfoil
01/23/2001US6176677 Device for controlling air flow in a turbine blade
01/23/2001US6176075 Combustor cooling for gas turbine engines
01/18/2001WO2001004477A1 High-pressure gas-turbine plant using high-pressure piston-type compressor
01/18/2001WO2001004475A1 Gas turbine engine power boost using micro droplet liquid injection
01/18/2001WO2000060239A3 Load sharing valve and system for operating centrifugal pumps in parallel
01/17/2001EP1069377A2 Fuel purging fuel injector
01/17/2001EP1069282A2 Dual-pressure steam injection partial-regeneration-cycle gas turbine system
01/17/2001EP1068161A1 Use of high temperature insulation for ceramic matrix composites in gas turbines
01/16/2001US6174133 Coolable airfoil
01/16/2001US6174130 Movable shaft assembly
01/16/2001US6173566 Casing construction on a gas turbine jet engine
01/16/2001US6173563 Modified bottoming cycle for cooling inlet air to a gas turbine combined cycle plant
01/16/2001US6173562 Exhaust recirculation type combined plant
01/16/2001US6173561 Steam cooling method for gas turbine combustor and apparatus therefor
01/11/2001DE10031484A1 Verfahren und Vorrichtung zum Starten eines Gasturbinentriebwerks Method and apparatus for starting a gas turbine engine
01/10/2001EP1067338A2 Method and apparatus for optimizing nox emissions in a gas turbine
01/10/2001EP1067282A2 Integrated engine control system for a gas turbine engine
01/10/2001EP1066451A1 Deflector for controlling entry of cooling air leakage into the gaspath of a gas turbine engine
01/10/2001EP0765453B1 Pilot injector for gas turbine engines
01/10/2001CN1279344A Oil seals of gas turbine
01/10/2001CN1279299A Die cast nickle-based high temperature alloy products
01/09/2001US6171052 Cooling of a honeycomb seal in the part of a gas turbine to which hot gas is admitted
01/09/2001US6170831 Axial brush seal for gas turbine engines
01/09/2001US6170263 Method and apparatus for converting low grade heat to cooling load in an integrated gasification system
01/09/2001US6170252 Locator for a gearbox mount
01/09/2001US6170251 Single shaft microturbine power generating system including turbocompressor and auxiliary recuperator
01/09/2001US6170141 Shipping system for jet aircraft engine and method of installing and removing jet aircraft engine
01/04/2001WO2001001041A1 Fuel injector heat shield
01/04/2001WO2001000975A1 Supercharging system for gas turbines
01/04/2001CA2376788A1 Supercharging system for gas turbines
01/03/2001EP1065490A2 Methods and apparatus for suppressing engine test cell howl
01/03/2001EP1065392A2 Varying effective cross section shaft assembly
01/03/2001EP1065347A2 Method and apparatus for fuel gas moisturization and heating
01/03/2001EP1065345A2 Turbine engine component having enhanced heat transfer characteristics and method for forming same
01/03/2001CN1278873A Method for producing abrasive tips for gas turbine blades `
01/02/2001US6167706 Externally fired combined cycle gas turbine
01/02/2001US6167691 Gasification power generation system using preheated gasifying-agent to gasify fuel
12/2000
12/28/2000WO2000079103A1 Fuel and oil system for a gas turbine
12/28/2000WO2000078480A1 Multipiece core assembly for cast airfoil
12/28/2000DE19928293A1 Exhaust gas turbocharger for internal combustion engine has masses of equal size at equal angular intervals on turbine shaft that engage shaft at equal radial, operationally variable distance
12/27/2000EP1063402A2 Method of operation of industrial gas turbine for optimal performance
12/27/2000EP1063401A1 Apparatus and method for separating gas from liquid
12/27/2000EP1063213A1 Ceramic superalloy articles
12/27/2000EP1062718A1 Electric motor or generator
12/27/2000EP1062415A2 Methods and apparatus for water injection in a turbine engine
12/27/2000EP1062409A1 High efficiency low pollution hybrid brayton cycle combustor
12/27/2000EP0854976B1 Combined pressurizing, flow measuring and flow splitting valve
12/26/2000US6165345 Electrochemical stripping of turbine blades
12/26/2000US6164912 Hollow airfoil for a gas turbine engine