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