Patents
Patents for F01D 25 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups (22,148)
02/2006
02/23/2006DE102004039477A1 Turbine body for turbo-charger, has spiral housing whose one part welded with contour bushing and/or outlet connection forms spiral shaped contour of canal and other part welded at bearing casing is flat base plate
02/22/2006EP1628076A1 Cooling Channel, Combustor and Gas Turbine
02/22/2006EP1627993A1 Exhaust turbine cleaning device
02/22/2006EP1627132A1 Bearing for axially mounting a rotor of a gas turbine, and gas turbine
02/22/2006CN1738682A Method and injection nozzle for interspersing a gas flow with liquid droplets
02/21/2006US7002273 Magnetic bearing
02/21/2006US7001151 Gas turbine bucket tip cap
02/21/2006US7001146 Electric fan cooling of hydraulic pump
02/21/2006US7001075 Bearing hub
02/21/2006US7000895 Valve having pressure balancing piston and method involving same
02/21/2006US7000404 Heat exchanger on a turbine cooling circuit
02/21/2006CA2243844C A method and manufacture of an axial tensioned bolt
02/18/2006CA2513036A1 Airfoil cooling passage trailing edge flow restriction
02/16/2006WO2006015613A1 Turbocharger
02/16/2006WO2006004655A3 Multi-thickness film layer bearing cartridge and housing
02/16/2006US20060032237 Assembly comprising a gas turbine combustion chamber integrated with a high pressure turbine nozzle
02/15/2006EP1626188A2 Bearing assembly for a gas turbine engine with resilient support
02/15/2006EP1626163A2 Clip member for a stator assembly
02/15/2006EP1626160A2 Degassing pipe for low pressure turbine shaft
02/15/2006EP1132594B1 Gas turbine power generation equipment and air humidifying apparatus
02/15/2006CN1735449A Filtration vessel and method for rotary gas compressor system
02/15/2006CN1734066A Internal combustion engine and lubrication system thereof
02/15/2006CN1242162C Oxygen separation method integrated with gas turbine
02/14/2006US6998756 Rotor shaft
02/14/2006US6997673 Gas turbine high temperature turbine blade outer air seal assembly
02/14/2006US6996992 Gas collection pipe carrying hot gas
02/14/2006US6996968 Bifurcated oil scavenge system for a gas turbine engine
02/09/2006US20060030748 Rotary pump with hydrodynamically suspended impeller
02/09/2006US20060026963 Approach to extending life of gas turbine engine
02/09/2006US20060026833 Method of fabricating a casing for a turbine stator
02/08/2006EP1624159A1 Gas turbine engine with shroud clearance control
02/08/2006EP1624156A1 Gas or steam turbine with a stress-resistant component
02/08/2006EP1623097A1 Steam/gas turbine pressure stage with universal shroud
02/08/2006CN1730914A Mixed ceramic ball bearing turbine supercharger
02/08/2006CN1240932C Casing design for rotating machinery and method for manufacture thereof
02/07/2006US6995979 Heat-dissipating fan module of electronic apparatus
02/07/2006US6994920 welding two alloys; one alloy being free of an element that can form a continuous layer of a brittle intermetallic; repairing turbine engine blades
02/02/2006WO2006011465A1 Wheel chamber casing and gas turbine
02/01/2006EP1621730A1 Cooled turbomachinery element and casting method thereof
02/01/2006EP1299621B1 Drainage system for gas turbine supporting bearings
01/2006
01/31/2006US6991432 Labyrinth seal for fan assembly
01/31/2006US6991427 Casing section
01/31/2006US6990815 Gas turbine and gas turbine high temperature section cooling method
01/31/2006CA2481810C Shaft structure and bearing structure for tail end of rotor of gas turbine
01/31/2006CA2381659C Gas turbine combined plant
01/26/2006US20060018757 Gas turbine engine structure
01/26/2006US20060016527 performing recovery, solution and aging heat treatments of the nickel based alloy component; hot isostatic pressing; improved creep life, ductility or toughness
01/26/2006US20060016190 Methods and apparatus for cooling turbine engine combustor ignition devices
01/26/2006US20060016173 Securing arrangement
01/26/2006DE19524218B4 Kombianlage KombiAnlage
01/26/2006CA2796895A1 Turbine exhaust case and method of making
01/26/2006CA2573342A1 Turbine exhaust case and method of making
01/25/2006EP1619369A2 Methods and apparatus for cooling turbine engine combustor ignition devices
01/25/2006EP1619356A1 Thrust bearing for a turbocharger
01/25/2006EP1619355A1 Bearing and seal arrangement in a steam turbine
01/25/2006EP1619353A1 Wall cooling circuit
01/25/2006EP1618290A1 Turbine nozzle segment
01/25/2006EP1618289A1 Method and installation for maintenance of gas turbines
01/25/2006EP1334286B1 Rotary machine with axial stop incorporating a current generator
01/25/2006CN1724851A Method and system for operating rotary machines
01/25/2006CN1724116A Oxygen separator and oxygen separation method
01/24/2006US6990432 Apparatus and method for performing gas turbine adjustment
01/24/2006US6988870 Casing for a centrifugal pump
01/24/2006US6988869 Turbine installation, especially steam turbine installation
01/24/2006US6988356 Fuel metering unit with a compensated regulator valve in a turbomachine
01/24/2006CA2254885C Turbomachine rotor cooling
01/24/2006CA2206638C Centrifugal compressor hub containment assembly
01/20/2006CA2507190A1 Methods and apparatus for cooling turbine engine combustor ignition devices
01/19/2006WO2006005659A1 Vane wheel of a turbine comprising a vane and at least one cooling channel
01/19/2006WO2006005355A1 Turbocharger housing, turbocharger and a multiturbocharger system
01/19/2006US20060013683 Spacer arrangement
01/19/2006US20060011708 Friction plug welding method, for a hole in a metal part, use of a metal bar and of a bearing supporting part for implementing the method
01/19/2006DE102004030798A1 Abgasturbolader für eine Brennkraftmaschine mit variabler Turbinengeometrie Exhaust gas turbocharger for an internal combustion engine with variable turbine geometry
01/19/2006CA2509788A1 Foreign object damage tolerant nacelle anti-icing system
01/18/2006EP1617046A1 Shaft and bearing assembly
01/18/2006EP1617043A1 Method for cooling a wall within a gas turbine engine
01/18/2006EP1327094B1 Actuator for a valve, in particular a turbine valve
01/18/2006CN1721706A Fluid machinery especially exhaust-gas turbocharger
01/18/2006CN1721670A Improvement of cooling aft end of a combustion liner
01/18/2006CN1721660A Turbine airfoil trailing edge repair and methods therefor
01/18/2006CN1237262C Device for fixing turbo charger to base
01/17/2006US6986951 Cobalt-based alloy for the coating of organs subject to erosion by liquid
01/12/2006WO2006004655A2 Multi-thickness film layer bearing cartridge and housing
01/12/2006WO2006004654A1 Rotational anx axial retention of ball bearing cartridge in the housing of a turbomachine
01/12/2006WO2006003071A1 Exhaust gas diffuser wall contouring
01/12/2006WO2006002523A1 A method of increasing the efficiency of a fuel gas turbine by cooling combustion air
01/12/2006US20060009950 Methods and apparatus for assessing gas turbine engine damage
01/12/2006US20060005545 Localized arc filament plasma actuators for noise mitigation and mixing enhancement
01/12/2006DE10011440B4 Abgasturbolader mit verstellbaren Düsenflügeln Turbocharger with variable nozzle vanes
01/11/2006EP1614879A1 Gas turbine cooling system and method
01/11/2006EP1614865A1 Stiffener for the low pressure compressor of an aeroengine
01/11/2006EP1614862A1 Gas turbine and gas turbine cooling and sealing method
01/11/2006EP1614861A1 Turbine wheel comprising turbine blades having turbulators on the platform radially inner surface.
01/11/2006EP1614858A1 Method and apparatus for monitoring the cooling system of a turbine
01/11/2006CN1720352A Aqueous composition for the chemical removal of metallic surfacing present on turbine blades, and its use
01/11/2006CN1718362A Device for demounting of a turbine or compressor blade
01/10/2006US6984112 Methods and apparatus for cooling gas turbine rotor blades
01/10/2006US6983608 Methods and apparatus for assembling gas turbine engines
01/10/2006US6983607 Turbine compartment ventilation control system and method using variable speed fan
01/05/2006WO2006001825A2 Gas turbine cooled shroud assembly with hot gas ingestion suppression