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)
02/2003
02/12/2003EP1023526B1 Gas and steam turbine installation and method for operating an installation of this type
02/12/2003CN1396993A Improved brush-seal designs for turbines and smilar rotary apparatus
02/11/2003US6517341 Injecting effective amount of elemental silicon and/or silicon-containing compound into combustion gas environment to prevent or reduce volatilization of silica film located on silicon-containing ceramic or ceramic composite
02/11/2003US6517241 Sensors and methodology for improved turbine exhaust gas temperature measurements
02/11/2003US6516618 Gas-turbine engine with a bearing chamber
02/11/2003US6516603 Gas turbine engine system with water injection
02/06/2003WO2003010425A1 Gas turbine
02/06/2003WO2002039045A3 Annular recuperator
02/06/2003WO2002029225A9 Method of shutting-down a turbine engine and system for carrying out said method
02/06/2003US20030027093 Hybrid film cooled combustor liner
02/06/2003US20030027013 Thermal barrier coating
02/06/2003US20030026665 Component for holding down measuring leads
02/06/2003US20030025033 Device for the attachment of an engine to an aircraft
02/06/2003US20030024696 Counterflow plate-fin heat exchanger with extended header fin
02/06/2003US20030024430 Applying a slurry which comprises braze material also containing a volatile component to the substrate, drying and fusing
02/06/2003US20030024233 Particle separator for a turbine engine
02/06/2003US20030024232 Particle separator
02/05/2003EP1281922A2 Microcomponent chemical process sheet architecture
02/05/2003EP1281921A2 Counterflow plate-fin heat exchanger with extended header fin
02/05/2003EP1281916A2 Hybrid film cooled combustor liner
02/05/2003EP1281788A1 Sprayed ZrO2 thermal barrier coating with vertical cracks
02/05/2003EP1281615A1 Device for locking an engine on an aircraft
02/05/2003EP1280981A1 Method and device for cooling the inflow area of the shaft of a steam turbine
02/05/2003EP1237641A4 Engine with upstream and rotationally attached guard
02/05/2003EP1115906B1 Method for processing the interior of a hollow part
02/05/2003CN1395667A Thermal shield for component carrying hot gases, especially for structural components of gas turbines
02/05/2003CN1395649A Device for centring tube in turbine shaft
02/05/2003CN1395030A Dimethyl ether fuel and method for producing power in dry low NO2 fuel system
02/04/2003US6516263 Adaptive flame-out prevention
02/04/2003US6514038 Turbine rotor, cooling method of turbine blades of the rotor and gas turbine with the rotor
02/04/2003US6513335 Device for supplying seal air to bearing boxes of a gas turbine engine
02/04/2003US6513331 Preferential multihole combustor liner
02/04/2003US6513318 Low emissions gas turbine engine with inlet air heating
02/03/2003WO2002042031A1 Layered heat-resistant alloy plate and method of producing the same
01/2003
01/30/2003WO2003008822A2 Enhanced capacity bearing
01/30/2003WO2003008768A1 Method for operating a burner of a gas turbine and a power plant
01/30/2003WO2001071176A9 Method and system for generating power
01/30/2003US20030021678 Foreign material exclusion device
01/30/2003US20030021675 Thermal shield for a component carrying hot gases, especially for structural components of gas turbines
01/30/2003US20030020496 Play measuring sensor by multiple depth abrasion
01/30/2003US20030019229 Heat and electric power supply system and operation method thereof
01/30/2003US20030019215 Method for igniting a thermal turbomachine
01/30/2003US20030019214 Gas turbine installation
01/30/2003US20030019202 Gas turbine
01/29/2003EP1279796A2 Selective step turbine nozzle
01/29/2003EP1278947A1 Oxygen separation method integrated with gas turbine
01/29/2003CN1394263A Thermally stressable wall and method for sealing gap in thermally stressed wall
01/28/2003US6511284 Methods and apparatus for minimizing gas turbine engine thermal stress
01/28/2003US6510889 Directional solidification method and apparatus
01/28/2003US6510684 Gas turbine engine
01/23/2003WO2003006884A1 A method of combustor cycle airflow adjustment
01/23/2003WO2003006883A1 Coolable segment for a turbomachinery and combustion turbine
01/23/2003WO2003006800A1 Sole plate for turbine and power generating plant equipment
01/23/2003US20030017045 Turbine no-load speed limiter
01/23/2003US20030014978 Gas turbine
01/23/2003US20030014964 Joint arrangement
01/23/2003US20030014958 Gas turbine
01/22/2003EP1277920A1 Procedure for operating a combuster of a gas-turbine and power plant
01/22/2003EP1277919A1 Joint arrangement
01/22/2003EP1276572A2 Methods and apparatus for retrofitting compressible flanges
01/22/2003EP1171691A4 Frangible cover for turbofan engine blade removal and access
01/22/2003EP1009915B1 Gas turbine combustor transition
01/22/2003CN1392917A Steam-type gas turbine subassembly and method for enhancing turbine performance
01/22/2003CN1392809A Device and method for producing blade for turbine and blade produced according to this method
01/21/2003US6508865 Method and apparatus for compressing atmospheric air, and corresponding air distillation and gas turbine installations
01/21/2003US6508061 Diffuser combustor
01/21/2003US6508052 Air intakes of turbines comprising engine housing having air cleaners and gas flow passageways in axial layouts; filters
01/21/2003US6508000 Transient liquid phase bonding repair for advanced turbine blades and vanes
01/16/2003WO2003004834A1 Securing system for the rotor blades of axial flow turbo engines
01/16/2003US20030012939 Fiber reinforced composite article, fiber member, and method for making
01/16/2003US20030012651 Bladed rotor disc side-plate and corresponding arrangement
01/16/2003US20030010866 Aircraft engine mounting
01/16/2003US20030010469 Device and method for casting a workpiece and workpiece
01/16/2003US20030010038 Heat shield arrangement for a component carrying hot gas, in particular for structural parts of gas turbines
01/16/2003US20030010036 Method of combustor cycle airflow adjustment
01/15/2003EP1275855A1 Member for holding down measurement leads
01/15/2003CN1099003C Spring seal unit of combustor
01/14/2003US6506021 Cooling system for a gas turbine
01/14/2003US6506014 Foreign material exclusion device
01/14/2003US6505834 Pressure actuated brush seal
01/09/2003WO2003002913A1 Gas turbine combustor
01/09/2003WO2003002861A1 Method for preparing clean intake air for gas turbine
01/09/2003US20030008167 Comprises barrier layer, hot gas corrosion protection layer, heat barrier layer, and smoothing layer for turbine blades (stator or rotor blade) of an aircraft engine
01/09/2003US20030007870 Methods and apparatus for extending gas turbine engine airfoils useful life
01/09/2003US20030007864 System and method for airfoil film cooling
01/09/2003US20030005704 Apparatus for decreasing combustor emissions
01/09/2003US20030005703 Engine stall and distortion suppression system
01/09/2003US20030005702 Operation method for combined plant
01/09/2003US20030005698 LNG regassification process and system
01/09/2003US20030005669 Turbine air filter media
01/08/2003EP1273768A1 Operation method for combined plant
01/08/2003EP1273767A1 Turbocharger support
01/08/2003EP1273765A1 Turbocharger shaft dual phase seal
01/08/2003EP1273761A1 Turbine inlet duct
01/08/2003EP1273759A1 Method and apparatus for extending gas turbine engine airfoils useful life
01/08/2003EP1273758A2 System and method for airfoil film cooling
01/08/2003EP1272736A2 Turbine engine foreign object damage detection system
01/08/2003EP0975862B1 Improved integrated environmental and secondary power system
01/08/2003EP0932748B1 Closed loop steam cooled steam turbine
01/08/2003CN1390279A Method and device for increasing the pressure of a gas