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)
11/2005
11/24/2005US20050260034 Fastener assembly for attaching a non-metal component to a metal component
11/24/2005US20050260033 Fastener assembly for attaching a non-metal component to a metal component
11/24/2005US20050257863 Cold-forming a predetermined, pretreated Ti alloy into a cold-formed shape; subjecting the cold-formed shape to a post-forming annealing cycle comprising: heating the cold-formed shape, holding, cooling the cold-formed shape to room temperature
11/24/2005US20050257529 Divergent flap for a gas turbine engine
11/24/2005DE102005020470A1 Cooling insert and nozzle assembly for use by gas turbine, has cooling insert having flexible edge portion which is inserted between adjacent ribs of nozzle
11/24/2005DE102005019652A1 Turbulator auf der Unterseite einer Turbinenschaufelspitzenumleitbiegung und zugehöriges Verfahren Turbulator on the underside of a Turbinenschaufelspitzenumleitbiegung and associated method
11/24/2005DE102004016462A1 Coolable wall structure for especially gas turbine has cooling medium passing through passages formed in core and parallel to one another and parallel to inner and outer shells
11/23/2005EP1598566A1 A fastener assembly for attaching a non-metal component to a metal component
11/23/2005EP1598562A1 A fastener assembly for attaching a non-metal component to a metal component
11/23/2005EP1598537A1 Steam turbine body and method of cooling a steam turbine
11/23/2005EP1598525A1 Turbocharger support structure
11/23/2005EP1598523A1 Wall structure for hollow gas turbine blades to increase the heat transfer
11/23/2005EP1598522A1 Steam turbine components, method for cooling a steam turbine and their use.
11/23/2005EP1598439A2 HVOF bi-layer coating with controlled porosity for use in thermal barrier coatings
11/23/2005EP1598438A1 TI 6-2-4-2 sheet with enhanced cold-formability
11/23/2005EP1597465A1 Compressed air energy storage system and method of operation
11/23/2005EP1597463A1 Method for producing gas turbines and gas turbine assembly
11/23/2005EP1480770B1 Method and device for producing precision investment-cast ne metal alloy members
11/23/2005CN1701168A Method for conditioning a compressor airflow and device therefor
11/23/2005CN1699615A Method for plasma coating a turbine blade and coating device
11/23/2005CN1699614A Ti6-2-4-2 sheet with enhanced cold-formability
11/23/2005CN1699292A Method for forming cove on the metal parts surface and related procedure and parts
11/23/2005CN1228541C Gas turbine, integrated circulating device and droplet injector of gas turbine
11/22/2005US6966753 Sole plate for turbine and power generating plant equipment
11/22/2005US6966745 Method for intermediate cooling and gas turbine system with intermediate cooling
11/22/2005US6966191 Device for supplying secondary air in a gas turbine engine
11/22/2005US6966189 System for sealing the secondary flow at the inlet to a nozzle of a turbomachine having a post-combustion chamber
11/22/2005US6966188 Plate-like body connecting method, connected body, tail pipe for gas turbine combustor, and gas turbine combustor
11/22/2005US6966173 Heat transfer apparatus
11/22/2005US6966172 Gas turbine exhaust passage and damper system for same
11/22/2005US6966171 Combined cycle gas turbine system
11/22/2005CA2207834C Aerodynamic system for injecting an air-fuel mix
11/20/2005CA2500677A1 A fastener assembly for attaching a non-metal component to a metal component
11/20/2005CA2500439A1 A fastener assembly for attaching a non-metal component to a metal component
11/20/2005CA2500430A1 Divergent flap for a gas turbine engine
11/17/2005WO2005108758A1 Air compression heat accumulating power plant with an underground heat accumulator formed in the aquifer (gaes)
11/17/2005WO2005107382A2 Method and device for reducing engine noise
11/17/2005US20050255648 Silicon based substrate hafnium oxide top environmental/thermal top barrier layer and method for preparing
11/17/2005US20050254955 Friction stir welded hollow airfoils and method therefor
11/17/2005US20050254950 Drum, in particular a drum forming a turbomachine rotor, a compressor, and a turboshaft engine including such a drum
11/17/2005US20050254945 Bearing support
11/17/2005US20050253379 Threaded joint for gas turbine components
11/17/2005US20050252375 Air recharge system dryer and methods therefor
11/17/2005US20050252231 Method for operating a compressor
11/17/2005US20050252195 Noise reduction assembly for aircraft turbojet
11/17/2005US20050252194 Methods and apparatus for assembling gas turbine engines
11/17/2005DE102004019970A1 System for injecting of fluid into working medium of gas turbine has dual nozzle for two media connected to water pipe and combustion gas pipe and opening into intake section for working medium before or at compressor
11/17/2005CA2547846A1 Method and device for reducing engine noise
11/16/2005EP1596038A2 Gas turbine engine bearing support
11/16/2005EP1596036A1 Friction stir welded hollow airfoils and method therefor
11/16/2005EP1595859A2 Article comprising a substrate comprising silicon and a top barrier layer comprising hafnium oxide
11/16/2005EP1595058A1 Sealing arrangement, particularly for the blade segments of gas turbines
11/16/2005EP1264091B1 Method and arrangement for cleaning the intake air of a gas turbine
11/16/2005EP1259348B1 Casting system and method for forming highly pure and fine grain metal castings
11/16/2005CN1696482A Original surface heat regenerator suitable to mini type gas turbine
11/16/2005CN1227454C Method and appts. for reducing heat stress in gas turbine
11/15/2005US6964791 High-temperature articles and method for making
11/15/2005US6964169 Hollow tapered body flattened in the transverse direction, wall being divided transversely into four adjacent parts, trapezoidal wall, made of refractory fibers embedded in another refractory matrics; vapor deposit refractory matrics; durability
11/15/2005US6964155 Turbofan engine comprising an spicyclic transmission having bearing journals
11/15/2005CA2292370C Improved coating and method for minimizing consumption of base material during high temperature service
11/15/2005CA2195833C Bearing device for vertical rotating machine
11/13/2005CA2504264A1 Silicon based substrate hafnium oxide top environmental/thermal top barrier layer and method for preparing
11/10/2005WO2005106225A2 Fuel controls on apu’s
11/10/2005WO2005106224A1 Improved process for producing electrical power
11/10/2005US20050249977 Comprising zirconia-containing hafnia stabilized by silica, and rare-earth oxides, wherein silica content gradually decreases toward surface of coating material and zirconia content gradually increases toward surface of coating material; erosion protection for non-oxide ceramic-coated gas turbines
11/10/2005US20050249888 Physical vapor deposition is augmented by chemical vapor deposition from one or more organometallic compounds, preferably refractory metal carbonyls, to deposit coatings and repair material on superalloy turbine engine parts
11/10/2005US20050249602 Integrated ceramic/metallic components and methods of making same
11/10/2005US20050249593 Cooling air evacuation slots of turbine blades
11/10/2005US20050249590 Turbomachine, for example a turbojet for an airplane
11/10/2005US20050249583 Cooled turbine airfoil
11/10/2005US20050249580 System for protecting a main shaft of an engine having a fusible bearing
11/10/2005US20050249443 Installation layout for two coaxial shaft lines
11/10/2005US20050248100 Stationary ring assembly for a gas turbine
11/10/2005US20050247526 Device for lubricating a component in an assembly of parts
11/10/2005US20050247062 Gas turbine
11/10/2005US20050247044 High efficiency rotor for the second phase of a gas turbine
11/10/2005US20050246895 Method of manufacturing a hollow blade for a turbomachine
11/10/2005US20050246894 Method for manufacturing a stator or rotor component
11/10/2005US20050246889 Device for assembling annular flanges together, in particular in a turbomachine
11/10/2005DE102005017150A1 Flexible Dichtungsanordnung zwischen Gasturbinenkomponenten und Verfahren zur Installierung Flexible sealing arrangement between gas turbine components and method of installing
11/10/2005DE102005017148A1 Drehdichtungsanordnung für Kühlkreisläufe von Turbinenschaufeln Rotary seal assembly for cooling circuits of turbine blades
11/10/2005CA2555937A1 Fuel controls on apu's
11/09/2005EP1593913A1 Gas turbine annular combustion chamber with improved inner support flange
11/09/2005EP1593817A1 Turbomachine provided with a protection system for the main engine shaft with frangible bearing
11/09/2005EP1593816A1 Turbomachine provided with a blocking system for the main engine shaft with frangible bearing
11/09/2005EP1593814A1 Feather seal configuration for a gas turbine shroud
11/09/2005EP1593812A2 Cooled turbine airfoil
11/09/2005EP1593757A1 Integrated ceramic/metallic components and methods of making same
11/09/2005EP1593752A2 Multi-component coating deposition
11/09/2005EP1593596A1 Aircraft engine with means for mounting it on the aircraft structure
11/09/2005EP1592870A1 Method for operating a gas turbine group
11/09/2005EP1185764B1 Device for controlling air flow in a turbine blade
11/09/2005CN1695002A A system for catalytic combustion
11/09/2005CN1693748A Device for lubricating component in assembly composed by multi-part
11/09/2005CN1693687A Nozzle with build-in rib part and assemble of cooling insertion part
11/09/2005CN1693686A Heat and electric power supply system and operation method thereof
11/09/2005CN1693534A Multi-component coating deposition
11/08/2005US6962482 Turbine shroud segment
11/08/2005US6962057 Gas turbine power generation system
11/08/2005US6962054 Method for operating a heat exchanger in a power plant