Patents
Patents for F01D 25 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups (22,148)
01/2006
01/05/2006US20060000077 A method of manufacturing a stator component
01/05/2006DE102004029696A1 Plattformkühlanordnung für den Leitschaufelkranz einer Gasturbine Platform cooling arrangement for a gas turbine vane ring
01/05/2006DE102004028133A1 Turbo-machine e.g. turbocharger, has flexible fixation provided with fitting bolt that comprises waisted shank and fitting pin, where pin is guided in flange part and/or hole of insert piece and spiral casing for receiving force
01/05/2006CA2551016A1 Gas turbine cooled shroud assembly with hot gas ingestion suppression
01/04/2006EP1612375A2 Cooling in a humid air turbine power plant
01/04/2006EP1612374A1 Turbine guide vane with improved cooling properties
01/04/2006EP1611989A1 A method of welding onto thin components
01/04/2006EP1611315A1 Turbomachine
01/04/2006CN1715625A Passive high-temperature amplifier for amplifying spark signals detected in igniter in gas turbine engine
01/04/2006CN1715618A Improved cooling stationary turbine blade
01/04/2006CN1714989A Homogeneous welding via pre-heating for high strength superalloy joining and material deposition
01/04/2006CN1234963C Gas turbine and gas turbine generator
01/04/2006CN1234961C Method for transporting steam turbine and appts. for helping such transportation of steam turbine
01/03/2006US6983199 Vibration measurement and recording system and method
01/03/2006US6981841 Triple circuit turbine cooling
01/03/2006US6981836 Apparatus and methods for removing and installing an upper diaphragm half relative to an upper shell of a turbine
01/03/2006CA2401945C Joint structure of coolant passage, tube seal and gas turbine
01/01/2006CA2508037A1 Balance assembly for rotary turbine component and method for installing and/or adjusting balance weight
12/2005
12/30/2005CA2473033A1 A method of increasing the efficiency of a fuel gas turbine by cooling combustion air
12/29/2005WO2005046021A3 Rotor and bearing system for a turbomachine
12/29/2005US20050288907 Signal processing method and apparatus
12/29/2005US20050287018 Retention of ball bearing cartridge for turbomachinery
12/29/2005US20050287001 Shroud and vane segments having edge notches
12/29/2005US20050286999 Exhaust-gas turbocharger for an internal combustion engine with a variable turbine geometry
12/29/2005US20050286823 Methods and apparatus for assembling a bearing assembly
12/29/2005US20050286819 Multi-thickness film layer bearing cartridge and housing
12/29/2005US20050284299 Centrifugal gas/liquid separators
12/29/2005US20050284214 Electric engine start system with inspection mode
12/29/2005DE102005026318A1 Verfahren und Vorrichtung zur Herstellung von Gasturbinentriebwerken Method and apparatus for the production of gas turbine engines
12/29/2005CA2510670A1 Venting tube for low-pressure shaft of a turbine engine
12/28/2005EP1610606A1 Hingeless flapper valve for flow control
12/28/2005EP1610012A1 A bearing arrangement
12/28/2005EP1609957A2 Gas turbine engine start system with inspection mode
12/28/2005EP1609956A2 Centrifugal gas/liquid separators for a gas turbine engine
12/28/2005EP1609955A1 Methods and apparatus for monitoring a bearing assembly
12/28/2005EP1609954A1 Securing arrangement
12/28/2005EP1608846A1 A method of manufacturing a stator component
12/27/2005US6979183 Arrangement for an exhaust gas turbo charger with a carrier housing
12/27/2005US6978680 Dynamic pressure probe holder and method of obtaining a dynamic pressure signal
12/27/2005US6978623 Gas turbine, driving method thereof and gas turbine combined electric power generation plant
12/27/2005US6978622 Turbomachine
12/24/2005CA2831868A1 Methods and apparatus for assembling a bearing assembly
12/24/2005CA2504173A1 Methods and apparatus for assembling a bearing assembly
12/22/2005WO2005121509A1 System and devices for collecting and treating waste water from engine washing
12/22/2005WO2005120953A1 System for washing an aero gas turbine engine
12/22/2005US20050281685 Rotary pump with exclusively hydrodynamically suspended impeller
12/22/2005US20050281663 Double impingement vane platform cooling
12/22/2005US20050279959 Valve having pressure balancing piston and method involving same
12/22/2005US20050279103 Hingeless flapper valve for flow control
12/22/2005US20050279100 High area-ratio inter-turbine duct with inlet blowing
12/22/2005US20050279061 Vents for fluid systems
12/22/2005DE102004026365A1 Turbine engine e.g. aircraft engine, outer cover band compensating device, has plate-shaped section including U-shaped area, where device is made of a plastically deformed wire-shaped unit whose cross section has round form
12/22/2005CA2714809A1 System for washing an aero gas turbine engine
12/22/2005CA2570243A1 System for washing an aero gas turbine engine
12/21/2005EP1607585A1 Fatigue failure diagnostic method of turbocharger and fatigue failure diagnostic apparatus for turbocharger
12/21/2005EP1607583A1 Method and system for operating rotary machines
12/21/2005EP1607582A1 Mounting of a gas turbine combustor with integrated turbine inlet guide conduit
12/21/2005EP1607581A1 Method and apparatus for fabricating a turbine nozzle assembly
12/21/2005EP1607580A2 Platform cooling of vanes in a gas turbine
12/21/2005EP1607579A1 Locking means for gas turbine engines
12/21/2005EP1607574A1 High area-ratio inter-turbine duct with boundary layer blowing
12/21/2005EP1607158A1 Process for preparing a turbine stator casing
12/21/2005CN2747360Y Cavitation proof diffuser for oil feeder
12/21/2005CN1711409A Shroud cooling assembly for a gas trubine
12/21/2005CN1232761C Heat shielding device for hot fuel gas guide piece, particularly gas turbine structure piece
12/20/2005US6977015 Method comprising providing an article that comprises at least one internal channel. The at least one internal channel comprises at least one inlet port and at least one outlet port. The method further comprises providing a cleaning
12/20/2005US6976827 Rotor balancing device and method
12/20/2005US6976361 Ventilation channels in an afterburner chamber confluence sheet
12/20/2005CA2357595C Combined cycle gas turbine system
12/18/2005CA2509863A1 Double impingement vane platform cooling
12/18/2005CA2509744A1 High area-ratio inter-turbine duct with inlet blowing
12/15/2005WO2005119032A1 Engine, vehicle provided with such an engine, and a connecting element between a first and a second element of an engine
12/15/2005WO2005119030A1 Turbine hub cooling system for exhaust-gas turbines
12/15/2005WO2005119028A1 Gas turbine compression system and compressor structure
12/15/2005WO2005119013A1 Vibration surpressor
12/15/2005WO2005097412A3 Seal removal tool for a seal having a grooved inner peripheral surface
12/15/2005US20050278108 Methods and apparatus for predicting and/or for avoiding lean blow-outs
12/15/2005US20050276687 Methods and apparatus for fabricating gas turbine engines
12/15/2005US20050276683 Turbomachine with means for axial retention of the rotor
12/15/2005US20050274701 Homogeneous welding via pre-heating for high strength superalloy joining and material deposition
12/15/2005US20050274114 Ventilation channels in an afterburner chamber confluence sheet
12/15/2005US20050274112 Fatigue failure diagnostic method of turbocharger and fatigue failure diagnostic apparatus for turbocharger
12/15/2005US20050274010 Method of replacing damaged aerofoil
12/15/2005DE102005022155A1 System und Verfahren zur Regelung einer Dampfturbine System and method for controlling a steam turbine
12/15/2005DE102004025049A1 Abgasturbolader Exhaust gas turbocharger
12/15/2005DE102004023284A1 Exhaust gas turbocharger for an I.C. engine of a vehicle comprises a spring element which fixes a guide blade support by pressing it against a bearing housing
12/14/2005EP1605205A2 Method and apparatus for predicting and/or avoiding lean blow-outs in a gas turbine engine
12/14/2005EP1605139A1 Turbomachine with axial retention means for the rotor
12/14/2005EP1605134A2 Device for balancing a gas turbine rotor and gas turbine engine comprising such a device
12/14/2005EP1605074A1 Thermal recovery treatment for a service-degraded component of a gas turbine
12/14/2005EP1605068A2 Homogeneous welding via pre-heating for high strength superalloy joining and material deposition
12/14/2005EP1604770A2 Method of replacing damaged aerofoil
12/14/2005CN1707076A Fatigue failure diagnostic method of turbocharger and fatigue failure diagnostic apparatus for turbocharger
12/14/2005CN1707070A Turboreactor with fan mounted on a drive shaft supported by a first and a second bearing
12/14/2005CA2763088A1 System and devices for collecting and treating waste water from engine washing
12/13/2005US6974508 Nickel base superalloy turbine disk
12/13/2005US6973771 Diffuser for terrestrial or aviation gas turbine
12/10/2005CA2509385A1 Homogeneous welding via pre-heating for high strength superalloy joining and material deposition
12/08/2005WO2005116407A2 Gas turbine engine including a low pressure sump seal buffer source and thermally isolated sump
12/08/2005WO2005116405A1 A support structure in a turbine or compressor device and a method for assembling the structure