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)
05/2005
05/24/2005US6896487 Microcircuit airfoil mainbody
05/24/2005US6896485 Combustion engine, gas turbine, and polishing layer
05/24/2005US6896475 Fluidic actuation for improved diffuser performance
05/24/2005US6896099 Aircraft engine pod with acoustic attenuation
05/24/2005US6896038 Stator ring ventilation assembly
05/24/2005US6896036 Method of making turbine blades having cooling channels
05/24/2005US6895756 Compact swirl augmented afterburners for gas turbine engines
05/24/2005US6895741 Differential geared turbine engine with torque modulation capability
05/24/2005CA2364125C Steam cooling apparatus for gas turbine
05/24/2005CA2334071C Gas turbine moving blade
05/19/2005WO2005045215A1 Hybrid engine accessory power system
05/19/2005WO2005045213A1 Method for operating an atomiser in a gas turbine group
05/19/2005US20050107942 Gas turbine control apparatus, gas turbine system and gas turbine control method
05/19/2005US20050107941 Method and system for incorporating an emission sensor into a gas turbine controller
05/19/2005US20050106316 High pressure turbine blades; nickel substrate overcoated with ceramic heat barrier; diffusion bonding using aluminum intermetallics
05/19/2005US20050106315 Method for repairing components using environmental bond coatings and resultant repaired components
05/19/2005US20050106021 Hot gas path component with mesh and dimpled cooling
05/19/2005US20050106012 Welded rotor for a thermal machine, and process for producing a rotor of this type
05/19/2005US20050106007 Spanwisely variable density pedestal array
05/19/2005US20050106002 Fan blade with embrittled tip
05/19/2005US20050103931 Hybrid engine accessory power system
05/19/2005US20050103032 Packaged chilling systems for building air conditioning and process cooling
05/19/2005US20050103019 Macrolaminate radial injector
05/19/2005US20050103017 Turbine power plant, installation process and removal process of the turbine power plant
05/19/2005US20050102994 Provision of sealing for the cabin-air bleed cavity of a jet engine using a brush seal
05/19/2005US20050102835 Method for repairing gas turbine rotor blades
05/19/2005DE10348424A1 Geschweisster Rotor für eine thermische Maschine sowie Verfahren zur Herstellung eines solchen Rotors Welded rotor of a thermal machine and method for producing such a rotor
05/19/2005CA2481351A1 Spanwisely variable density pedestal array
05/18/2005EP1531243A2 Method and system for incorporating an emission sensor into a gas turbine controller
05/18/2005EP1531232A2 Method for repairing a high pressure turbine blade
05/18/2005EP1531019A1 Refractory metal core wall thickness control
05/18/2005EP1530670A1 Recirculation structure for a turbocompressor
05/18/2005EP1125087B1 Burner assembly
05/18/2005CN1617951A High-temperature protection layer
05/18/2005CN1616805A Cooling system for nozzle segment platform edges
05/18/2005CN1616798A Method and apparatus for distributing fluid into a turbomachine
05/17/2005US6893750 Thermal barrier coating protected by alumina and method for preparing same
05/17/2005US6893225 Metallic article with integral end band under compression
05/17/2005US6893222 Turbine balancing
05/17/2005US6893214 Shroud segment and assembly with surface recessed seal bridging adjacent members
05/17/2005US6893209 Connecting system for a transition duct in a gas turbine
05/17/2005US6893208 Drainage system for gas turbine supporting bearings
05/17/2005US6892931 Methods for replacing portions of turbine shroud supports
05/17/2005US6892544 Flow divider & purge air system for a gas turbine engine
05/17/2005US6892542 Gas compression system and method for microturbine application
05/17/2005US6892526 Cowl structure for a gas turbine engine
05/17/2005US6892523 Cooling-air cooler for a gas-turbine plant and use of such a cooling-air cooler
05/17/2005US6892455 Stationary roller shaft formed of a material having a low inclusion content and high hardness
05/14/2005CA2487503A1 Method for repairing gas turbine rotor blades
05/12/2005WO2005042948A2 Air turbine starter with unitary inlet and stator
05/12/2005WO2005042947A1 Method for operating a power plant
05/12/2005WO2005042929A1 Power plant
05/12/2005WO2005042928A2 Heat shield for gas turbine engine
05/12/2005WO2005028843A3 Rotary injector
05/12/2005WO2005005888A8 Cooling structure of gas turbine tail pipe
05/12/2005US20050100438 Method and apparatus for distributing fluid into a turbomachine
05/12/2005US20050100437 Cooling system for nozzle segment platform edges
05/12/2005US20050100258 Arrangement for mounting two coaxial shaftlines
05/12/2005US20050099075 Hermetic motor and gas booster
05/12/2005US20050098608 Process for manufacturing or repairing a monobloc bladed disc
05/12/2005US20050097986 Mixing and heating two alloy powders with different melting points; high temperature parts in gas turbines and jet engines
05/12/2005US20050097898 Gas turbine unit and its cooling method
05/12/2005US20050097896 Dual mode power unit having a combustor bypass system
05/12/2005US20050097895 Method and apparatus for actuating fuel trim valves in a gas turbine
05/12/2005US20050097894 Combustion chamber for combusting a combustible fluid mixture
05/12/2005US20050097893 Method and apparatus for increasing a durability of a body
05/12/2005US20050097892 Method and apparatus for arresting a crack within a body
05/12/2005US20050097890 Gas turbine combustor
05/12/2005US20050097881 Gas turbine installation
05/12/2005US20050097880 Water cooled liquid fuel valve
05/12/2005DE19619836B4 Einrichtung zur Speisewasser-Vorsteuerung eines Kühllufttemperaturreglers für einen Kühlluftkühler Means for feed water pre-control a cooling air temperature controller for a cooling air cooler
05/12/2005CA2544458A1 Hybrid vane island diffuser
05/11/2005EP1529950A1 Method and apparatus for arresting a crack within an exhaust nozzle flap seal body
05/11/2005EP1529949A1 Method and apparatus for increasing a durability of an exhaust nozzle flap seal
05/11/2005EP1529927A2 Method and apparatus for distributing fluid into a turbomachine
05/11/2005EP1529926A2 Spring and damper system for turbine shrouds
05/11/2005EP1529925A2 Method and apparatus for arresting a crack within a ceramic matrix composite body
05/11/2005EP1529181A1 Gas turbine combustion chamber
05/11/2005EP1303684B1 Method for operating a gas and steam turbine installation and corresponding installation
05/11/2005EP1268981B1 Turbine installation
05/11/2005CN2698988Y Minisize turbojet engine
05/11/2005CN1614199A Spring mass damper system for turbine shrouds
05/11/2005CN1201073C Method and device for increasing pressure of gas
05/11/2005CN1200979C Anti-oxidation coat, its correlated product and method
05/10/2005US6892127 Methods and apparatus for assessing gas turbine engine damage
05/10/2005US6891282 Method and apparatus for monitoring turbine parameters of turbine/alternator on common shaft
05/10/2005US6890248 Apparatus and method for consistently retaining a gas turbine engine blade in a predetermined position and orientation
05/10/2005US6890154 Microcircuit cooling for a turbine blade
05/10/2005US6890150 Center-located cutter teeth on shrouded turbine blades
05/10/2005US6890147 Easy-fit heat screening device for connecting a cooling pipe and a through-hole formed in a nozzle support ring of a gas turbine
05/10/2005US6889506 Gas and steam turbine installation
05/07/2005CA2486014A1 Method and apparatus for increasing a durability of a body
05/06/2005WO2005040581A1 Power station unit
05/06/2005WO2005040580A2 Fluid-cooled mechanical face seal rotor
05/06/2005WO2005039978A2 Aircraft protection method and system
05/05/2005US20050096832 Apparatus and method for determining date of gas turbine washing
05/05/2005US20050095136 Retaining arrangement
05/05/2005US20050095134 Methods and apparatus for cooling gas turbine rotor blades
05/05/2005US20050095129 Methods and apparatus for assembling gas turbine engine rotor assemblies
05/05/2005US20050095128 Methods and apparatus for cooling gas turbine engine rotor assemblies