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)
05/2001
05/16/2001EP1099775A1 Platinum aluminide coating for cobalt-based superalloys
05/16/2001EP1099508A2 Turbine nozzle segment and method of repairing same
05/16/2001EP1099050A1 Device and method for actively reducing the noise emissions of jet engines and for diagnosing the same
05/16/2001EP1099045A1 Device and method for reducing the noise emissions of internal combustion engines and for diagnosing the same
05/16/2001EP1098724A1 Ceramic shell mold provided with reinforcement, and related processes
05/16/2001CN1295184A Gas turbine, gas turbomachine and coolant collecting method for blades of the same
05/15/2001US6232703 Multiple electrode igniter
05/15/2001US6231998 Thermal barrier coating
05/15/2001US6231303 Gas turbine having a turbine stage with cooling-air distribution
05/15/2001US6231287 Rotor windage nut
05/15/2001US6231006 Mission adaptive inlet
05/15/2001US6230483 Steam cooled type gas turbine
05/15/2001US6230482 Appliance for operating a gas turbine installation combustion chamber with liquid fuel
05/10/2001WO2001005579A3 One-step noble metal-aluminide coatings
05/10/2001US20010000846 Coolant recovery type gas turbine
05/09/2001EP1098140A1 Methods and apparatus for fuel nozzle staging for gas turbine engines
05/09/2001EP1098067A2 Cooling structure for gas turbine rotor blades
05/09/2001EP1097325A1 Sealing system, especially for a rotary machine
05/09/2001CN2429634Y Cooling device for inlet air of gas turbine by spray vaporization
05/09/2001CN1294770A Electric motor or generator
05/08/2001US6228510 Coating and method for minimizing consumption of base material during high temperature service
05/08/2001US6227804 Gas turbine blade
05/08/2001US6227801 Turbine engine having improved high pressure turbine cooling
05/08/2001US6227800 Bay cooled turbine casing
05/08/2001US6226978 Heat, oxidation, and corrosion resistant under- and overcoating alloy of chromium, yttrium, aluminum, nickel, and base metal
05/08/2001US6226975 Turbine power plant having a floating brush seal
05/08/2001US6226974 Method of operation of industrial gas turbine for optimal performance
05/08/2001CA2048783C Fuel circulation control system
05/03/2001WO2001031181A1 Gas turbine cooling system
05/02/2001EP1095212A1 Operating a gas turbine with supplemental compressed air
05/02/2001CN1293735A Method of generating power using advanced thermochemical recuperation cycle
05/02/2001CN1293362A Method for analysing monitering and controlling laser impact cold-forging by using instantaneous plasma spectrographic
05/01/2001US6224963 Laser segmented thick thermal barrier coatings for turbine shrouds
05/01/2001US6224941 Pulsed-vapor phase aluminide process for high temperature oxidation-resistant coating applications
05/01/2001US6224361 Tool for disposing laser blocking material in an airfoil
05/01/2001US6224329 Method of cooling a combustion turbine
05/01/2001US6224327 Steam-cooling type gas turbine
05/01/2001US6224321 Impeller containment system
05/01/2001US6223523 Method of operating a power station plant
05/01/2001US6223522 Combined cycle power plant and method using both light and heavy oils
05/01/2001US6223520 Gas turbine combined plant, method of operating the same, and steam-cooling system for gas turbine hot section
05/01/2001US6223519 Method of generating power using an advanced thermal recuperation cycle
05/01/2001CA2228350C Heat recovery type gas turbine
04/2001
04/26/2001DE19950417A1 Component for gas turbine, with base body and protective covering made of ceramic material
04/25/2001EP1094212A2 Vehicle main and auxiliary power units
04/25/2001EP1093398A2 Microcomponent assembly for efficient contacting of fluid
04/24/2001US6220829 Turbocharger rotor with low-cost ball bearing
04/24/2001US6220234 Coated compressor diffuser
04/24/2001US6220086 Method for ascertaining surge pressure ratio in compressors for turbines
04/24/2001US6220036 Cooling structure for combustor tail pipes
04/24/2001US6220035 Annular combustor tangential injection flame stabilizer
04/24/2001US6220012 Booster recirculation passageway and methods for recirculating air
04/24/2001CA2230341C Cooling steam system for steam cooled gas turbine
04/19/2001WO2001027444A1 Bearing housing for a turbomachine
04/19/2001WO2000025067A9 Fuel air mixer for a radial dome in a gas turbine engine combustor
04/19/2001DE19950425A1 Charging device for IC engine has heat exchanger located inside housing of compressor, compressor is radial one and fan is axial one, both on one axis.
04/19/2001DE19949241A1 Device for reducing sound conducted through air and solids caused by turbosuperchargers in internal combustion engines comprises tubes sliding into an outer jacket with a center flange to form a chamber
04/18/2001EP1092925A1 Film cooled combustor liner and method of making the same
04/18/2001CN1292062A Seal ring for steam turbine
04/17/2001US6217279 Device for sealing gas turbine stator blades
04/17/2001US6216443 Gas turbine, combined cycle plant and compressor
04/17/2001US6216442 Supports for connecting a flow sleeve and a liner in a gas turbine combustor
04/17/2001US6216441 Removal of inert gases from process gases prior to compression in a gas turbine or combined cycle power plant
04/17/2001US6216440 Starting device for model jet engines
04/17/2001US6216439 Gas turbine fuel system comprising fuel oil distribution control system, fuel oil purge system, purging air supply system and fuel nozzle wash system
04/11/2001EP1091095A2 Gas turbine system and combined plant comprising the same
04/11/2001EP1091020A1 A method of applying a bond coating and a thermal barrier coating on a metal substrate, and related articles
04/11/2001EP1091013A1 Method for forming a coating by use of an activated foam technique
04/11/2001EP1090711A1 Superalloy weld composition and repaired turbine engine component
04/11/2001EP1090710A1 Superalloy weld composition and repaired turbine engine component
04/11/2001EP1090222A1 Driving mechanism with counter-rotating rotors
04/11/2001EP0943069A4 An electricity generating system having an annular combustor
04/10/2001US6214475 Thermal insulating layer for a metallic component and its process of manufacture
04/10/2001US6212974 Variable stiffness positioning link for a gearbox
04/10/2001US6212873 Gas turbine combined cycle
04/10/2001US6212871 Method of operation of a gas turbine engine and a gas turbine engine
04/05/2001WO2001023724A2 Integrated bleed air and engine starting system (ibaness)
04/05/2001WO2001023255A1 Integrated engine and transmission units for rotary wing aircraft
04/05/2001US20010000091 Method of operating a combustion turbine power plant at full power at high ambient temperature or at low air density using supplemental compressed air
04/04/2001EP1088966A2 Turbine nozzle stage having thermocouple guide tube
04/04/2001EP1088965A1 A pyrometer mount for a closed-circuit thermal medium cooled gas turbine
04/04/2001EP1088963A2 Method and apparatus for purging turbine wheel cavities
04/04/2001EP1088908A2 A method for smoothing the surface of a protective coating
04/04/2001EP1088189A1 A method for starting a combustion device
04/04/2001EP0778921B1 Pumping device
04/03/2001US6210630 Process for manufacturing a hollow turbomachine blade and a multiple-action furnace press for use in said process
04/03/2001US6210104 Removal of cooling air on the suction side of a diffuser vane of a radial compressor stage of gas turbines
04/03/2001US6209679 Aircraft engine acoustic liner and method of making same
04/03/2001US6209311 Turbofan engine including fans with reduced speed
04/03/2001US6209310 Method and apparatus for monitoring the fuel and water supply of a gas turbine multiburner system
04/03/2001US6209309 Pulse width modulated fuel flow control for an engine
04/03/2001US6209307 Thermodynamic process for generating work using absorption and regeneration
04/03/2001US6209216 Methods and apparatus for measuring airfoil coordinates
04/03/2001US6209198 Method of assembling a variable stator vane assembly
03/2001
03/29/2001WO2001021847A2 Superalloys with improved weldability for high temperature applications
03/28/2001EP1087102A2 Gas turbine bucket with impingement cooled platform
03/28/2001EP1087101A2 Method for connecting air ducts in gas turbine rotors
03/28/2001EP1086303A1 Filter construction resistant to the passage of water soluble materials and filtration method
03/27/2001US6206637 Gas turbine blade
03/27/2001US6206629 Turbine brush seal protection device and method