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)
10/2002
10/24/2002WO2002084091A1 Gas turbine power generator
10/24/2002US20020155009 High thrust turbocharger rotor with ball bearings
10/24/2002US20020155000 Turbine blade or vane
10/24/2002US20020154992 Shaped part for forming a guide ring
10/24/2002US20020154990 Cooling system and method for cooling a turbo-machine housing
10/24/2002US20020152754 Advanced multi pressure mode gas turbine
10/24/2002US20020152753 Fuel mixing in a gas turbine engine
10/24/2002US20020152751 Gas turbine combustor
10/24/2002US20020152740 Gas turbine combustor having bypass passage
10/24/2002DE10207279A1 Gießverfahren und Gussteil Casting and casting
10/24/2002DE10160107A1 Reinigung eines inneren Kanals einer Gasturbinenschaufel Cleaning an interior channel of a gas turbine blade or vane
10/23/2002EP1251313A2 A gas turbine combustor
10/23/2002EP1251257A1 Jet engine air intake fairing with de-icing device
10/23/2002EP1251243A1 Turbine blade with cooling air baffle
10/23/2002EP1250555A2 Thermal shield for a component carrying hot gases, especially for structural components of gas turbines
10/23/2002EP1099050B1 Device and method for actively reducing the noise emissions of jet engines and for diagnosing the same
10/23/2002EP1099045B1 Device and method for reducing the noise emissions of internal combustion engines and for diagnosing the same
10/23/2002EP1078204B1 A device for the supply of a liquid fuel to a burner member
10/23/2002EP1007271B1 Gas turbine vane and method for producing a gas turbine vane
10/23/2002CN2517877Y Water cooling gas turbine
10/22/2002WO2002068799A1 Combustion engine, gas turbine, and polishing layer
10/22/2002US6470258 System and method for monitoring engine starting systems
10/22/2002US6468669 Article having turbulation and method of providing turbulation on an article
10/22/2002US6468073 Duct burner diffuser
10/22/2002US6468031 Nozzle cavity impingement/area reduction insert
10/22/2002US6467988 Reducing cracking adjacent shell flange connecting bolts
10/22/2002US6467725 Electrical generator an aero-engine including such a generator, and an aircraft including such a generator
10/22/2002US6467339 Method for deploying shroud segments in a turbine engine
10/22/2002US6467272 Means for wear reduction in a gas turbine combustor
10/22/2002US6467252 Nozzles for water injection in a turbine engine
10/19/2002CA2381603A1 A gas turbine combustor
10/17/2002WO2002081884A1 Gas turbine, vehicle comprising said gas turbine and method for engine-braking a gas turbine
10/17/2002WO2002081869A1 Rotor gap control module
10/17/2002WO2002081868A1 Gas turbine blade
10/17/2002WO2002081602A1 Heating of fuels
10/17/2002WO2002029225A8 Method of shutting-down a turbine engine and system for carrying out said method
10/17/2002WO2001075272A3 Turbine engine foreign object damage detection system
10/17/2002US20020150470 Gas turbine
10/17/2002US20020150469 Turbine
10/17/2002US20020150468 Turbine blade or vane and process for producing a turbine blade or vane
10/17/2002US20020150467 Steam-cooling-type turbine
10/17/2002US20020150316 Bearing assembly
10/17/2002US20020150142 Sensors and methodology for improved turbine exhaust gas temperature measurements
10/17/2002US20020148929 Air inlet cowl for a jet engine, provided with deicing means
10/17/2002US20020148233 Gas turbine
10/17/2002US20020148232 Gas turbine engine having a multi-stage multi-plane combustion system
10/17/2002US20020148231 Multi-stage multi-plane combustion method for a gas turbine engine
10/17/2002US20020148227 Multi pressure mode gas turbine
10/17/2002US20020148216 Bleed system driven in simplified manner for a turbojet or turboprop engine
10/17/2002US20020148214 Gas turbine
10/17/2002US20020148213 Re-fired gas turbine engine
10/17/2002US20020148115 Transient liquid phase bonding repair for advanced turbine blades and vanes
10/17/2002CA2442749A1 Rotor gap control module
10/16/2002EP1249618A1 Bleed system for a turbofan with simplified control
10/16/2002EP1249592A2 Steam cooled turbine
10/16/2002EP1249581A2 Gas turbine combined plant
10/16/2002EP1249578A1 Cooling of a gas turbine
10/16/2002EP1249577A1 Gas turbine with axially movable shroud elements
10/16/2002EP1248924A1 Thermally stressable wall and method for sealing a gap in a thermally stressed wall
10/16/2002EP1248897A1 Gas and steam turbine installation
10/16/2002CN1092757C Control method and device for power generating equipment of gas turbine
10/16/2002CN1092748C Gas turbine airfoil cooling system and method
10/16/2002CN1092747C Compressor impeller apparatus for turbo chargers and its mounting/dismonting apparatus and method
10/15/2002US6464461 Steam cooling system for a gas turbine
10/15/2002US6464457 Turbine leaf seal mounting with headless pins
10/15/2002US6464455 Debris trap in a turbine cooling system
10/15/2002US6464401 High load capacity bi-directional tapered roller bearing
10/15/2002US6464128 Braze repair of a gas turbine engine stationary shroud
10/15/2002US6463819 Uninterruptible oil supply system
10/15/2002US6463742 Gas turbine steam-cooled combustor with alternately counter-flowing steam passages
10/15/2002US6463740 Compressor starting torque converter
10/15/2002US6463731 Two stroke regenerative external combustion engine
10/15/2002US6463729 Combined cycle plant with gas turbine rotor clearance control
10/15/2002CA2093683C Intercooled gas turbine engine
10/15/2002CA2071448C Burner for operating an internal combustion engine, a combustion chamber of a gas turbine group or firing equipment
10/10/2002WO2002080189A1 A nuclear power plant and a method of conditioning its power generation circuit
10/10/2002WO2002079631A1 Tortuous path exhaust eductor system
10/10/2002US20020146584 Process for producing sandwich structures between metallic and nonmetallic materials
10/10/2002US20020146541 Sandwich structure between metallic and non-metallic materials
10/10/2002US20020144664 Heating of fuels
10/10/2002US20020144505 Gas turbine combined plant
10/10/2002DE10117128A1 Verfahren zur Herstellung von Verbundaufbauten zwischen metallischen und nichtmetallischen Materialien A method for producing composite structures between metallic and non-metallic materials
10/10/2002DE10117127A1 Verbundaufbau zwischen metallischen und nichtmetallischen Materialien Composite structure between metallic and non-metallic materials
10/10/2002DE10116117A1 Cooling thermally loaded structures of power generation system involves regulating partly compressed air pressure or mass flow by injecting water into compressor or induction flow
10/09/2002EP1247961A2 Steam cooled gas turbine with a sliding setpoint for the high pressure bypass
10/09/2002EP1247944A2 Gas turbine frame
10/09/2002EP1247943A1 Coolable turbine shroud member
10/09/2002EP1247942A2 Seal element for sealing a gap and combustion turbine having such a seal element
10/09/2002EP1247941A1 Gas turbine blade
10/09/2002EP1247939A1 Turbine blade and process of manufacturing such a blade
10/09/2002EP1247874A1 Composite construction with metallic and non-metallic materials
10/09/2002EP1247607A2 Connecting part manufacturing method used between metallic and non-metallic materials
10/09/2002EP1247602A1 Method for producing an airfoil
10/09/2002EP1247003A1 Turbine blade and method of repair
10/09/2002EP1071872B1 Anti-coking fuel injector purging device
10/09/2002EP0898645B1 Process and apparatus for achieving power augmentation in gas turbines via wet compression
10/09/2002CN1092289C Ramjet engine for power generation
10/08/2002US6460343 Gas turbine engine
10/08/2002US6460339 Gas turbine fuel injector with unequal fuel distribution
10/08/2002US6460326 Gas only nozzle