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)
06/2004
06/08/2004US6745558 Gas-turbine engine control system
06/08/2004US6745557 Hydraulic valve arrangement
06/03/2004WO2004046560A1 Method of repairing turbine blade
06/03/2004WO2004004953A3 Diffusion bond mixture for healing single crystal alloys
06/03/2004US20040106486 Gas turbine arrangement
06/03/2004US20040106360 Method and apparatus for cleaning combustor liners
06/03/2004US20040106359 Method and apparatus for removing a predetermined amount of material from a bottom portion of a dovetail slot in gas turbine engine disk
06/03/2004US20040106000 Cobalt-based alloy for the coating of organs subject to erosion by liquid
06/03/2004US20040105755 Fogging device for gas turbines
06/03/2004US20040104017 Device for coolant cooling in a gas turbine and gas and steam turbine with said device
06/03/2004US20040103669 Integrated turbine power generation system with catalytic reactor
06/03/2004US20040103667 Intake silencer for gas turbines
06/03/2004US20040103666 Method and arrangement for proving a gas turbine, and engine-braking therefore
06/03/2004US20040103663 Gas turbine engine combustor can with trapped vortex cavity
06/03/2004US20040103662 Cooling of liquid fuel components to eliminate coking
06/03/2004US20040103637 Power system and method
06/03/2004DE10329849A1 Anlage mit kombiniertem Zyklus vom 1-Achsen-Typ Combined cycle plant from the 1-axis type
06/03/2004DE10254859A1 Turbolader Turbocharger
06/03/2004DE10254825A1 Wassersprühvorrichtung für Gasturbinen Fogging for gas turbines
06/03/2004DE10254721A1 Liquid injection system for air intake of gas turbine engine has radial struts between intake lip and central body each with row of nozzles connected to ring main
06/03/2004DE10253579A1 Lufteinlauf für Triebwerke und dessen Herstellung Air inlet for engines and its production
06/02/2004EP1424525A2 Method and apparatus for cleaning combustor liners
06/02/2004EP1424467A2 Row of long and short chord length turbine airfoils
06/02/2004EP1424465A1 HYBRID ROTOR, METHOD OF MANUFACTURING THE HYBRID ROTOR, AND GAS TURBINE
06/02/2004EP1424158A1 A method for fabricating, modifying or repairing of single crystal or directionally solidified articles
06/02/2004EP1423647A1 Combustion chamber arrangement
06/02/2004EP1423595A1 Combustion turbine fuel inlet temperature management for maximum power output
06/02/2004EP1423230A1 A method for manufacturing a hollow blade for a stator or rotor component
06/02/2004EP1204776B1 High-temperature part and method for producing the same
06/02/2004EP1156962B1 Tangentially directed acoustic jet controlling boundary layers
06/02/2004EP1095212A4 Operating a gas turbine with supplemental compressed air
06/02/2004EP0975435A4 Modular coating fixture
06/02/2004CN1500979A Composite bifuel turbine device and its operating method thereof
06/02/2004CN1500972A Uniaxial combined circulation power-plant
06/02/2004CN1500969A Method and apparatus for reducing flow across compressor airfoil tips
06/02/2004CN1500917A The electrical process for the simultaneous stripping of diverse coatings from a metal substrate
06/01/2004US6743350 Apparatus and method for rejuvenating cooling passages within a turbine airfoil
06/01/2004US6742698 Refractory metal backing material for weld repair
06/01/2004US6742339 Methods and apparatus for exhausting gases from gas turbine engines
06/01/2004US6742324 Methods and apparatus for supporting variable bypass valve systems
06/01/2004CA2148059C Steam cooling of gas turbine with backup air cooling
05/2004
05/27/2004US20040101433 Austenitic nickel/chrome/cobalt/molybdenum/tungsten alloy and use thereof
05/27/2004US20040101405 Row of long and short chord length and high and low temperature capability turbine airfoils
05/27/2004US20040100101 Integrated turbine power generation system with catalytic reactor
05/27/2004US20040100035 Active seal assembly
05/27/2004US20040099832 Valve having pressure balancing piston and method involving same
05/27/2004US20040098988 Uniaxial gas turbine system
05/27/2004DE10353039A1 Oil or gas, dual power, turbine power station has an analysis unit with intermediate pressure turbine pressure sensor and an analysis unit for estimating the low pressure turbine power output
05/27/2004DE10232291B4 Vorrichtung und Verfahren zur aktiven Schallbekämpfung sowie Triebwerk für Flugzeuge Apparatus and method for active noise reduction and engine for aircraft
05/26/2004EP1422479A1 Chamber for the combustion of a fluid combustible mixture
05/26/2004EP1422403A1 Fogging device for gas turbines
05/26/2004EP1422402A1 Method of closing working hole in gas turbine blade top
05/26/2004EP1422401A2 Secondary air charger
05/26/2004EP1422381A2 Method of repairing a turbine nozzle segment, and turbine nozzle segment
05/26/2004EP1421258A1 Blade for a turbine engine and method for production of said blade
05/26/2004CN1500187A Rotary machine with seal
05/26/2004CN1499044A Flow passage sealing of turbine and streamline structure thereof
05/26/2004CN1499043A Continuous radial loader for steam turbine reaction blade and its method
05/26/2004CN1499042A 涡轮机 Turbines
05/26/2004CA2449149A1 Method and apparatus for cleaning combustor liners
05/25/2004US6740292 Improved castability and resistance to oxidation, especially at high temperatures; large gas turbine single crystal components
05/25/2004US6740177 Castable and weldable nickel-base alloys exhibiting desirable properties suitable for gas turbine engine applications
05/25/2004US6739845 Compact turbocharger
05/25/2004US6739381 Method of producing a turbine blade
05/25/2004US6739119 Combustion engine improvement
05/25/2004US6739118 Safety device for a washing system for liquid fuel burners in gas turbines
05/21/2004WO2004007927A3 Method for influencing and controlling the oxide layer on metallic components of a hot co2/h2o circulating system
05/21/2004CA2552091A1 Outlet silencer structures for turbine
05/20/2004US20040098142 Arbitrage control system for two or more available power sources
05/20/2004US20040097170 Method for smoothing the surface of a gas turbine blade
05/20/2004US20040096375 Device for producing a plasma, ionisation method, use of said method and production processes using said device
05/20/2004US20040096323 Turbine nozzle segment and method of repairing same
05/20/2004US20040096322 Fabricated repair of cast nozzle
05/20/2004US20040096319 Rotary machine with seal
05/20/2004US20040096318 Combustion engine, gas turbine, and polishing layer
05/20/2004US20040096314 Selected binder method, article and system
05/20/2004US20040094359 Aircraft engine pod with acoustic attenuation
05/20/2004US20040094118 Method and a device for supplying fuel to a combustion chamber
05/20/2004US20040093872 Internally coolable screw
05/20/2004US20040093850 Gas Turbine
05/19/2004EP1420318A2 System and method for displaying real-time turbine corrected output and heat rate
05/19/2004EP1420234A1 Method for selecting a binder for a thermal indicator in a gas turbine system
05/19/2004EP1420075A1 Nickel-base superalloy
05/19/2004EP1419849A1 Fabricated repair of cast nozzle
05/19/2004EP1269097B1 A heat exchanger
05/19/2004EP1047896B1 Direct control fuel valve for fuel flow injecting circuit
05/19/2004DE10350627A1 Fortlaufende radiale Vorspannvorrichtung für Dampfturbinenschaufeln der Reaktionsbauart und zugehöriges Verfahren Continuous radial biasing device for steam turbine blades of reaction type and associated method
05/19/2004DE10350626A1 Strompfaddichtung und Stromlinienkonfigurierung für eine Turbine Current path seal and Stromlinienkonfigurierung for a turbine
05/19/2004DE10250302A1 Drallerzeugungseinrichtung für einen Verdichter Swirler for a compressor
05/19/2004CN1497218A Annular combustion chamber of gas trubine and gas turbine
05/19/2004CN1497216A Mixing swirler
05/19/2004CN1497148A Method and device for controlling fluid flow of gas turbine engine
05/19/2004CN1497133A Internal anti-icing device of fanjet
05/19/2004CN1497132A Turbine, especially gas turbine and moving vane
05/19/2004CN1497050A Cobalt-base alloy for coating element corroded by fluid
05/18/2004US6736597 Axis seal mechanism and turbine
05/18/2004US6735957 Coolant recovery type gas turbine
05/18/2004US6735956 High pressure turbine blade cooling scoop
05/18/2004US6735955 Control system for positioning compressor inlet guide vanes
05/18/2004US6735954 Offset drive for gas turbine engine