Patents
Patents for F01D 25 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups (22,148)
01/2003
01/21/2003CA2218457C Process for manufacturing a hollow turbine engine blade
01/16/2003WO2003004834A1 Securing system for the rotor blades of axial flow turbo engines
01/16/2003WO2003004711A1 Sintered tin-containing cobalt-based and nickel-based alloys
01/16/2003US20030014219 Method for remote monitoring of gas turbine
01/16/2003US20030010038 Heat shield arrangement for a component carrying hot gas, in particular for structural parts of gas turbines
01/15/2003EP1275855A1 Member for holding down measurement leads
01/15/2003EP1275818A1 Base material with cooling hole
01/15/2003CN1391030A Transfer frame for assembling steam turbine and assembling method and transferring method thereby
01/14/2003US6506018 Casing design for rotating machinery and method for manufacture thereof
01/14/2003US6506015 Centrifugal compressor and centrifugal turbine
01/14/2003US6506013 Film cooling for a closed loop cooled airfoil
01/14/2003US6505706 Exhaust flow guide for jet noise reduction
01/09/2003WO2003002851A1 Modular gas turbine
01/09/2003US20030008166 Bondcoat is formed by thermally co-spraying distinct alloy powders on the engine component forming an oxidation-resistant region, and spraying another alloy forming a bonding region
01/09/2003US20030007870 Methods and apparatus for extending gas turbine engine airfoils useful life
01/09/2003US20030007705 Bearing arrangement for turbo-machines
01/09/2003US20030005705 Industrial gas turbine multi-axial thermal isolator
01/09/2003US20030005694 Apparatus for fastening an exhaust gas turbocharger on an exhaust chamber of a combustion engine
01/08/2003EP1273767A1 Turbocharger support
01/08/2003EP1273766A1 Turbocharger with thermal isolation connection
01/08/2003EP1273765A1 Turbocharger shaft dual phase seal
01/08/2003EP1273764A1 Turbomachine
01/08/2003EP1273762A1 Apparatus for controling the inlet stage of a steam turbine and steam turbine
01/08/2003EP1273760A1 Turbocharger with nozzle ring coupling
01/08/2003EP1273759A1 Method and apparatus for extending gas turbine engine airfoils useful life
01/08/2003EP0932748B1 Closed loop steam cooled steam turbine
01/08/2003CN2530042Y Direct air cooling turbine steam exhauster for power station
01/07/2003US6505143 Machine protection system for rotating equipment and method
01/07/2003US6503334 Forced mist cleaning of combustion turbines
01/07/2003US6503056 Heating device and method for deployable ram air turbine
01/07/2003US6503052 Integrated regulating bleed device for a steam turbine
01/07/2003US6502403 Steam-injection type gas turbine
01/07/2003US6502401 High pressure bypass sliding setpoint for steam-cooled turbine
01/07/2003US6502383 Stub airfoil exhaust nozzle
01/07/2003US6502303 Method of repairing a turbine blade tip
01/03/2003WO2003001036A1 Segmented turbine vane support structure
01/02/2003US20030002980 Apparatus for choking the control stage of a steam turbine and steam turbine
01/02/2003EP1270891A2 Device for fixing a turbocharger to an exhaust manifold of an internal combustion engine
01/02/2003EP1270876A2 Spring-backed abradable seal for turbomachinery
01/02/2003EP1270141A2 Method for repairing cracks in a turbine blade root trailing edge
01/02/2003EP1270129A2 Selective removal of brazing compound from joined assemblies
01/02/2003EP1269047A2 Improved brush-seal designs for turbines and similar rotary apparatus
01/02/2003EP1268982A1 Gas turbine engine stator case
01/02/2003EP1268981A1 Turbine installation
01/01/2003CN1388306A Combustion gas turbine nited equipment
12/2002
12/31/2002US6502085 Methods and systems for estimating engine faults
12/31/2002US6500269 Subjecting portion of component having deposit of crust-like debris to sufficient laser shock peening to cause deposited debris on the surface thereof to be loosened therefrom so that loosened debris can be removed from the component
12/31/2002US6500058 Clogging-free drain system installed in a cutting apparatus
12/31/2002US6499950 Cooling circuit for a gas turbine bucket and tip shroud
12/31/2002US6499945 Wheelspace windage cover plate for turbine
12/31/2002US6499943 Friction-susceptible component of a thermal turbo machine
12/31/2002US6499938 Method for enhancing part life in a gas stream
12/31/2002US6499884 Bearing/seal member/assembly and mounting
12/31/2002CA2261531C Seal active clearance control system for gas turbine stationary blade
12/27/2002WO2002103188A1 Exhaust flow guide for jet noise reduction
12/26/2002US20020197157 Tandem guide vanes
12/26/2002US20020197153 Segmented turbine vane support structure
12/26/2002US20020197150 Device for compensating for an axial thrust in a turbo engine
12/26/2002US20020197147 Turbine frame, turbine assembling method and turbine assembling and transporting method
12/26/2002US20020194733 Method for repairing cracks in a turbine blade root trailing edge
12/25/2002CN1097151C Gas turbine power generation equipment and air humidifying apparatus
12/24/2002US6497137 Annular after reactor with sound attenuator for use in a jet engine test cell and test stand
12/19/2002US20020193933 Apparatus for monitoring gas turbine engine operation
12/19/2002US20020192491 Oxidation resistant coatings for niobium-based silicide composites
12/19/2002US20020192074 Spring-backed abradable seal for turbomachinery
12/19/2002US20020190029 Adding an oxime to an appropriate injection point of an electric generating power plant powered by a steam turbine
12/19/2002US20020189995 Centrifugal separator for separating off water
12/19/2002US20020189896 Exhaust flow guide for jet noise reduction
12/19/2002US20020189262 Method for operating a steam turbine , and a turbine system provided with a steam turbine that functions according to said method
12/19/2002US20020189261 Method of operating a gas-turbine power plant, and gas-turbine power plant
12/18/2002EP1267310A2 Method and apparatus for managing maintenance operations
12/18/2002EP0906494B1 Turbine shaft and process for cooling it
12/18/2002EP0722534B1 Pressurized ball bearing assemblies
12/18/2002CN1385271A Selectively removing braze composition from conneted assembly
12/17/2002US6494682 Ceiling fan assembly and method for assembling same
12/17/2002US6494152 Stamped blower housing with 4″ transition
12/17/2002US6494044 Aerodynamic devices for enhancing sidepanel cooling on an impingement cooled transition duct and related method
12/17/2002US6494032 Ducted fan gas turbine engine with frangible connection
12/12/2002US20020188494 Method and apparatus for managing an operation
12/12/2002CA2390341A1 Method and apparatus for managing maintenance operations
12/11/2002EP1264966A1 Steam turbine and power generating equipment
12/11/2002EP1264965A2 Bearing housing of a turbocharger for an internal combustion engine
12/11/2002EP1264081A1 Ball bearing assembly for turbocharger rotor
12/11/2002EP1264080A1 Integral bearing assembly for a turbocharger rotor
12/11/2002EP1264079A1 Distributor for an exhaust gas turbine with an axial flow
12/11/2002CN1384273A Sealing method and device for bearing box of steam turbine
12/10/2002US6492034 Heat shield
12/10/2002US6491497 Method and apparatus for supporting rotor assemblies during unbalances
12/10/2002US6491093 Cooled heat shield
12/10/2002US6491048 Manifold for use in cleaning combustion turbines
12/10/2002US6491044 Thorough air induction, fuel injection and decarbonization cleaning machine and process that requires no disassembly of the engine or its components which uses compressed air at its source of power
12/10/2002US6490791 Method for repairing cracks in a turbine blade root trailing edge
12/05/2002US20020182069 Turbo machines
12/05/2002US20020182067 Gas turbine blade and gas turbine
12/05/2002US20020182065 Vane for a stator of a variable-geometry turbine, in particular for aeronautical engines
12/05/2002US20020182061 Air inlet and outlet silencer structures for turbine
12/05/2002US20020182059 Centripetal air-bleed system
12/05/2002US20020182058 Methods and apparatus for minimizing gas turbine engine thermal stress
12/05/2002US20020182057 Integral nozzle and shroud
12/05/2002US20020178727 Methods and apparatus for injecting fuel into gas turbine engines