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)
04/2004
04/22/2004WO2004033872A1 Atmospheric pressure combustion turbine system
04/22/2004WO2004033871A2 Leak resistant vane cluster
04/22/2004WO2004033116A1 Formation of corrosion-resistant coating
04/22/2004US20040076540 Welding material, gas turbine blade or nozzle and a method of repairing a gas turbine blade or nozzle
04/22/2004US20040076520 Turbine and stationary blade for a turbine
04/22/2004US20040076512 Noise reduction conduit for static components in aircraft engines
04/22/2004US20040076511 Gas turbine
04/22/2004US20040076218 System and method for determining gas turbine firing and combustion reference temperatures having correction for water content in fuel
04/22/2004US20040074873 Process for removing aluminosilicate material from a substrate, and related compositions
04/22/2004US20040074239 Annular combustion chambers for a gas turbine and gas turbine
04/22/2004US20040074237 Methods and apparatus for regulating gas turbine engine fluid flow
04/22/2004US20040074236 Gas turbine combustor
04/22/2004US20040074223 Combustion system with shutdown fuel purge
04/22/2004DE10296563T5 Rotationsmaschine mit Dichtungsvorrichtung Rotary machine with sealing device
04/21/2004EP1411281A1 Butterfly valve
04/21/2004EP1411225A1 Acoustic liner for gas turbine engine
04/21/2004EP1411209A2 Cooled stationary blades in a gas turbine
04/21/2004EP1411136A1 Ni-BASE SINTERED ALLOY
04/21/2004EP1410872A1 Welding material, gas turbine blade or nozzle and a method of repairing a gas turbine blade or nozzle
04/21/2004EP1410853A1 Apparatus and method for cleaning airfoil internal cavities
04/21/2004EP1409926A1 Baffle cooling device
04/21/2004EP1409862A1 Gas turbine
04/21/2004CN1491317A Installation for generation of energy
04/21/2004CN1491292A Method for plasma coating turbine blade and coating device
04/21/2004CN1490497A 燃气轮机 Gas turbine
04/21/2004CN1490496A Gas turbine disc rim with air cooling duct shortened axially and declined peripherily
04/21/2004CN1146576C Proteins from mammaliam liver and their use in oncology
04/20/2004US6724099 Method and apparatus for starting up a turboset
04/20/2004US6722851 Internal core profile for a turbine bucket
04/20/2004US6722138 Vane platform trailing edge cooling
04/20/2004US6722136 Aircraft engine water misting inter-cooler
04/20/2004US6722135 Performance enhanced control of DLN gas turbines
04/20/2004US6722131 Fuel control valve
04/20/2004US6722119 Turbojet power plant with heat exchanger
04/15/2004WO2004031668A1 A reduced carbon dioxide emission system and method for providing power for refrigerant compression and electrical power for a light hydrocarbon gas liquefaction process using cooled air injection to the turbines
04/15/2004WO2004031656A1 Gas turbine
04/15/2004WO2004015257A9 Particle separator for a turbine engine
04/15/2004US20040073400 Method for managing lifespans of high temperature gas turbine components and its implementation through computer program
04/15/2004US20040072014 Method for providing turbulation on the inner surface of holes in an article, and related articles
04/15/2004US20040070211 Integrated starter/generator for a turbomachine
04/15/2004US20040069748 Electrochemical process for the simultaneous stripping of diverse coatings from a metal substrate
04/15/2004US20040069324 Cleaning fluid dispenser or probe that extends into a passageway and has a longitudinal axis and at least one nozzle that is oriented at an angle to the longitudinal axis
04/15/2004US20040068975 Kinetic energy turbine with recuperation
04/15/2004US20040068974 Fuel system
04/15/2004DE10344843A1 Integrierte Rotier-Messerkanten-Injektionsanordnung Integrated Rotier knife edge injection assembly
04/15/2004DE10296161T5 Schott für industrielle Gasturbinen mit dualem Brennstoff und Luftfahrt-Gasturbinenmaschinen Schott for industrial gas turbines with dual fuel and aviation gas turbine engines
04/15/2004CA2499575A1 A reduced carbon dioxide emission system and method for providing power for refrigerant compression and electrical power for a light hydrocarbon gas liquefaction process using cooled air injection to the turbines
04/14/2004EP1408280A2 Hybrid swirler
04/14/2004EP1408214A2 A method for managing lifespans of high temperature gas turbine components
04/14/2004EP1408199A1 Leak resistant vane cluster
04/14/2004EP1408197A1 Method for forming abrasion-resistant layer for moving blade, abrasion-resistant layer and method for regeneration thereof, and gas turbine
04/14/2004EP1408134A1 Method for repairing ni base alloy component
04/14/2004EP1407852A2 Process for machining axial blade slots in turbine disks for jet engines
04/14/2004EP1407194A1 A method of combustor cycle airflow adjustment
04/14/2004EP1407193A1 Coolable segment for a turbomachinery and combustion turbine
04/14/2004EP1407158A2 Enhanced capacity bearing
04/14/2004EP1407126A1 Means for wear reduction in a gas turbine combustor
04/14/2004EP1407120A1 Method for operating a burner of a gas turbine and a power plant
04/14/2004EP1327006B1 Austenitic nickel/chrome/cobalt/molybdenum/tungsten alloy and use thereof
04/14/2004CN1489041A Life managment method for high-temperature gas turbine part and computer programme for realizing same
04/14/2004CN1145786C Optical high temperature meter for gas turbine
04/14/2004CN1145758C Shaping method and apparatus for stairs-like heating side of hurner back lining
04/13/2004US6720685 Turbogenerator cooling method
04/13/2004US6719529 Gas turbine blade and method for producing a gas turbine blade
04/13/2004US6719296 Seal for a rotating member
04/13/2004US6719295 Supplemental seal for the chordal hinge seals in a gas turbine
04/13/2004US6718794 Compression, expansion, combustion, separation cycles
04/13/2004US6718773 Method for igniting a thermal turbomachine
04/13/2004US6718771 Gas turbine operative at high ambient temperatures
04/13/2004US6718750 Gas turbine installation with regenerator and water injection
04/11/2004CA2432746A1 A method for managing lifespans of high temperature gas turbine components and its implementation through computer program
04/09/2004CA2444177A1 The electrical process for the simultaneous stripping of diverse coatings from a metal substrate
04/08/2004WO2004029433A1 A system for catalytic combustion
04/08/2004US20040067131 Leak resistant vane cluster
04/08/2004US20040066177 Method and apparatus for monitoring turbine parameters of turbine/alternator on common shaft
04/08/2004US20040066176 Method and apparatus for controlling output current of turbine/alternator on common shaft
04/08/2004US20040066175 Method and apparatus for turbine/alternator on common shaft during start-up
04/08/2004US20040065775 Tooling for molding with keys particularly for the production of air intakes without clips
04/08/2004US20040065092 Turbofan engine internal anti-ice device
04/08/2004US20040065091 Off loading clutch for gas turbine engine starting
04/08/2004US20040065090 Hybrid swirler
04/08/2004US20040065087 Variable geometry inlet design for scram jet engine
04/08/2004US20040065074 Gas turbine installation
04/08/2004US20040064944 Process for machining axial blade slots in turbine disks for jet engines
04/07/2004EP1406026A1 Oil-film damped roller bearing
04/07/2004EP1406019A1 Drum rotor for a turbomachine
04/07/2004EP1405986A2 Turbofan engine internal anti-ice device
04/07/2004EP1088189B1 A method for starting a combustion device
04/07/2004CN1488036A 高压水泵 High pressure pumps
04/07/2004CN1487174A Combined circular generator with gas and hydrocarbon oil gas turbine and steam turbine
04/07/2004CN1487173A Running controlling apparatus and running controlling method for single-shaft combine equipment with clutch
04/07/2004CN1487172A Cooling In Low-pressure turbine casing
04/07/2004CN1144964C Hair brush type seal
04/07/2004CN1144940C Exhaust reheating combined cycle electric generating complete sets of equipment
04/06/2004US6717420 Play measuring sensor by multiple depth abrasion
04/06/2004US6717418 Method and apparatus for measuring turbine blade tip clearance
04/06/2004US6715993 Methods and apparatus for manufacturing rotor shafts
04/06/2004US6715988 Turbine airfoil for gas turbine engine
04/06/2004US6715983 Method and apparatus for reducing distortion losses induced to gas turbine engine airflow
04/06/2004US6715916 System and method for determining gas turbine firing and combustion reference temperatures having correction for water content in fuel