Patents
Patents for F01D 25 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups (22,148)
07/2002
07/25/2002US20020097935 Ball bearing and bearing assembly
07/25/2002US20020097929 Turbo compressor
07/25/2002US20020097928 Self-aligning/centering rotating foil thrust bearing (air film type) utilized in a rotating compressor
07/25/2002US20020096393 Turbogenerator exhaust silencer
07/25/2002US20020096197 Methods and apparatus for washing gas turbine engines
07/25/2002US20020095937 Combustion turbine cooling media supply system and related method
07/25/2002DE10111187C1 Steam line closure valve for steam turbine plant provided by several elements cooperating for blocking steam line cross-section
07/24/2002EP1225322A1 Apparatus to centre a tube in a turbine shaft
07/24/2002EP1225309A1 Support strut for the stator ring of the high-pressure turbine of a turbomachine provided with clearance compensation
07/24/2002EP1225308A2 Split ring for gas turbine casing
07/24/2002EP1225307A2 Methods and apparatus for washing gas turbine engines
07/24/2002EP1225305A2 Gas turbine shroud segment
07/24/2002EP1224382A1 Bearing housing for a turbomachine
07/24/2002EP1224381A1 Device for compensating axial thrust in a turbomachine
07/24/2002CN1088144C Steam filter for steam turbine
07/23/2002US6422818 Lubricating system for thermal medium delivery parts in a gas turbine
07/23/2002US6422817 Cooling circuit for and method of cooling a gas turbine bucket
07/23/2002US6422810 Exit chimney joint and method of forming the joint for closed circuit steam cooled gas turbine nozzles
07/23/2002US6422809 Gas turbine arrangement
07/23/2002US6422807 Turbine inner shell heating and cooling flow circuit
07/23/2002US6422068 Test rig and particulate deposit and cleaning evaluation processes using the same
07/23/2002US6422010 Toughness, impact strength; nickel, titanium intermetallics
07/18/2002WO2002055754A2 Method and device for gas phase diffusion coating of metal components
07/18/2002US20020094268 Split ring for gas turbine casing
07/18/2002US20020092190 Trailing edge thickness measurement method and apparatus
07/18/2002DE10061816A1 System for lubricating an internal combustion engine with a turbocharger uses a first pump at a first pressure level to feed a lubricant from a lubricant sump to the turbocharger's bearings and a second pump to suck the lubricant out.
07/17/2002EP1223405A1 Method and apparatus for measuring the trailing edge thickness of a turbine airfoil
07/17/2002EP1223308A2 Cooling of a turbo machine component
07/16/2002US6419453 Steam turbine rotor shaft
07/16/2002US6419448 Flow by-pass system for use in steam turbine exhaust hoods
07/16/2002US6419445 Apparatus for impingement cooling a side wall adjacent an undercut region of a turbine nozzle segment
07/16/2002US6418722 Turbocharger bearing system
07/16/2002US6418618 Method of controlling the side wall thickness of a turbine nozzle segment for improved cooling
07/11/2002WO2002053918A1 Gas turbine engine axial stator compressor
07/11/2002WO2002053900A2 Fluid and fuel delivery system reducing pressure fluctuations
07/11/2002WO2002053876A1 Stay sector of stator shroud of the high-pressure turbine of a gas turbine engine with clearance control
07/11/2002US20020090298 Component of a flow machine, with inspection aperture
07/11/2002US20020090296 Division wall and shroud of gas turbine
07/11/2002US20020090295 Cooling structure for a gas turbine
07/11/2002US20020089298 Apparatus for robotically inspecting gas turbine combustion components
07/11/2002US20020089248 Gas turbomachinery generator
07/11/2002US20020088480 For cleaning contaminated surfaces of gas turbine structures
07/11/2002US20020088270 Water-flow testing apparatus
07/11/2002CA2433549A1 Gas turbine engine axial stator compressor
07/10/2002EP1221604A2 Water-flow testing apparatus
07/10/2002EP1221555A1 Axial compressor stator for a gas turbine
07/10/2002EP1221543A2 Misted air cleaning system and related method
07/10/2002EP1221539A2 Sealing for shrouds of a gas turbine
07/10/2002EP1221536A2 Cooling structure for a gas turbine
07/10/2002EP1221029A1 Measuring twist due to torque in a rotating shaft
07/10/2002CN1087389C Working vane assembly method and equipment
07/09/2002US6416281 Method and arrangement for cooling the flow in radial gaps formed between rotors and stators of turbomachines
07/09/2002US6416277 Individually replaceable and reversible insertable steam turbine nozzle
07/09/2002US6416276 Heat shield device in gas turbines
07/09/2002US6415846 Turbochargers
07/09/2002US6415610 Apparatus and method for replacement of combustor basket swirlers
07/09/2002US6415595 Integrated thermal management and coolant system for an aircraft
07/04/2002WO2002052128A1 Method for steam turbine halfshell alignment
07/04/2002US20020085932 Exhaust gas turbocharger for an internal combustion engine
07/04/2002US20020085925 System and method for protecting turbine and compressor during shutdown
07/04/2002US20020085911 Coolant recovery type gas turbine
07/04/2002US20020085910 Apparatus and methods for localized cooling of gas turbine nozzle walls
07/04/2002US20020084382 Aircraft deicer
07/04/2002US20020083987 Fluid and fuel delivery systems reducing pressure fluctuations and engines including such systems
07/04/2002DE10064269A1 Komponente einer Strömungsmaschine mit Inspektionsöffnung Component of a turbomachine with inspection hole
07/03/2002EP1219789A2 System and method for the cooling of a turbomachine casing
07/03/2002EP1219787A1 Gas turbine blade and gas turbine
07/03/2002EP1219786A2 Vane installation tool
07/03/2002EP1219784A2 Apparatus and method for localized cooling of gas turbine nozzle walls
07/03/2002EP1219783A2 Stator vane for an axial flow turbine
07/03/2002EP1219779A2 Turbo machine component with inspection hole
07/03/2002EP1219777A2 Methods and apparatus for controlling bearing loads
07/02/2002US6414458 Apparatus for robotically inspecting gas turbine combustion components
07/02/2002US6413046 Method and apparatus for centering rotor assembly damper bearings
07/02/2002US6413044 Blade cooling in gas turbine
07/02/2002US6413040 Support pedestals for interconnecting a cover and nozzle band wall in a gas turbine nozzle segment
07/02/2002US6412820 Secured coupling assembly and method of preventing loosening
07/02/2002US6412284 Methods and apparatus for supplying air to gas turbine engines
07/02/2002US6412270 Apparatus and methods for flowing a cooling or purge medium in a turbine downstream of a turbine seal
07/02/2002US6412269 Method for operating an engine system including a gas turbine engine, an inverted Brayton cycle apparatus having blow-in doors and blow-out doors for engine protection
07/02/2002US6412268 Cooling air recycling for gas turbine transition duct end frame and related method
07/02/2002US6412149 C-clip for shroud assembly
06/2002
06/27/2002US20020083372 Method and system for diagnosing a technical installation
06/27/2002US20020082726 Method for steam turbine halfshell alignment
06/27/2002US20020081190 Methods and apparatus for controlling bearing loads within bearing assemblies
06/27/2002US20020078677 Gas turbine installation
06/27/2002US20020078563 Pneumatic press vane lift installation tool
06/27/2002DE10064895A1 Cooling system for a turbine housing, comprises air blower and unit for adjusting air inlet temperature
06/27/2002CA2559618A1 Pneumatic press vane lift installation tool
06/27/2002CA2366184A1 Gas turbine blade/vane and gas turbine
06/26/2002EP1216797A1 Methods for robotically inspecting gas turbine combustion components
06/26/2002EP1216796A1 Apparatus for robotically inspecting gas turbine combustion components
06/26/2002EP0979347B1 Heat insulation device for a steam turbine
06/26/2002EP0891471B1 Thrust-compensating process and device for turbomachines
06/26/2002CN2497046Y High-pressure drainage sealing device
06/26/2002CN1086770C Axial-flow turbine of waste gas turbine booster
06/25/2002US6409472 Stator assembly for a rotary machine and clip member for a stator assembly
06/25/2002US6409469 Fan-stator interaction tone reduction
06/25/2002US6409464 Methods and apparatus for supplying oil to bearing assemblies
06/25/2002CA2278034C Gas turbine installation