Patents
Patents for F01D 25 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups (22,148)
06/2002
06/25/2002CA2257162C Gas turbine cooled moving blade
06/20/2002WO2002048527A1 Combustor turbine successive dual cooling
06/20/2002WO2002048525A2 System to feed cooling air into a gas turbine rotor
06/20/2002US20020076124 Squeeze film damping type bearing
06/20/2002US20020074965 Apparatus for robotically inspecting gas turbine combustion components
06/20/2002US20020074017 Cleaning of oxides and dirt from internal cooling air passages of airfoils by immersion in an inorganic hydroxide stripping solution for a short time
06/20/2002US20020073788 Methods for robotically inspecting gas turbine combustion components
06/20/2002US20020073714 Gas turbine engine with offset shroud
06/20/2002DE10150527A1 Support foot for turbosupercharger has at least two plates running transversely to longitudinal expansion of turbosupercharger and spaced out from bed
06/20/2002DE10131370A1 Cooled gas turbine blade has cover strip containing cooling system sealed by radially-oriented cover plate, facing edges of plate and strip having corresponding slope and space between them being filled with low ductility welding material
06/20/2002DE10131073A1 Cooling system for cover strip of gas turbine blade comprises cooling channels which open on one side, perforated baffle plate fitted over these being pressed against them by gas-permeable spring and cover plate being fitted above spring
06/19/2002EP1215364A2 Cooling of a blade shroud in a gas turbine
06/19/2002EP1215363A2 Cooled gas turbine blade
06/19/2002EP1215118A1 Test bench for thrust reverser
06/19/2002EP1215005A2 Electrochemical machining process for forming surface roughness elements on a gas turbine shroud
06/19/2002CN2495812Y Means for supporting gear box for steam engine
06/19/2002CN1086332C Device and method for deassembling and assembling combustion turbine
06/19/2002CA2364593A1 Cleaning of internal passages of airfoils
06/18/2002US6407475 Bearing load control
06/18/2002US6406256 Device and method for the controlled setting of the gap between the stator arrangement and rotor arrangement of a turbomachine
06/18/2002US6406253 Turbocharger
06/18/2002US6406252 Steam turbine having an exhaust-steam casing
06/13/2002WO2002046350A1 Engine cleaner composition
06/13/2002US20020070075 Silencing apparatus, notably for a turbo engine
06/13/2002US20020069644 Combustor turbine successive dual cooling
06/13/2002DE10061846A1 Exhaust gas turbocharger for internal combustion engines has turbine housing comprising two individual sheet metal parts spaced from each other with interspace formed between inner and outer shells
06/13/2002DE10022052C2 Turbinengehäuse für Abgasturbolader Turbine housings for turbocharger
06/13/2002CA2431198A1 Engine cleaner composition
06/12/2002EP1213538A2 Exhaust gas system with Helmholtz resonator
06/12/2002EP1213444A2 Shroud segment for a turbine
06/12/2002EP1213370A2 Method and composition for cleaning a turbine engine component
06/12/2002EP1128933B1 System for the precision machining of rotationally symmetrical components
06/11/2002US6402470 Method and apparatus for cooling a wall within a gas turbine engine
06/11/2002US6402468 Method and apparatus for axially aligning inner and outer turbine shell components
06/11/2002US6402466 Leaf seal for gas turbine stator shrouds and a nozzle band
06/11/2002US6402464 Enhanced heat transfer surface for cast-in-bump-covered cooling surfaces and methods of enhancing heat transfer
06/11/2002US6402458 Clock turbine airfoil cooling
06/06/2002WO2002044538A2 Device for centring a tube in a turbine shaft
06/06/2002US20020067870 Method and apparatus for supporting rotor assembly bearings
06/06/2002US20020066275 Process and device for preheating suction air by waste heat in power engines
06/05/2002EP1211406A1 Methods and apparatus for sealing gas turbine engine variable nozzles
06/05/2002EP1211387A1 Internal stator shroud
06/05/2002EP1211382A2 Turbomachine rotor with blades of different frequency
06/05/2002EP0886721B1 Protective coating for tubing blades
06/05/2002EP0800892B1 Exchanging device for combustor
06/05/2002CA2363613A1 Method and composition for cleaning a turbine engine component
06/04/2002US6398503 High temperature component, gas turbine high temperature component and manufacturing method thereof
06/04/2002US6398488 Interstage seal cooling
06/04/2002US6398486 Steam exit flow design for aft cavities of an airfoil
06/04/2002US6398485 Device for positioning of nozzles of a stator stage and for cooling of rotor discs in gas turbines
06/04/2002US6397604 Cooling supply system for stage 3 bucket of a gas turbine
06/04/2002US6397576 Gas turbine engine with exhaust compressor having outlet tap control
05/2002
05/30/2002WO2002042665A1 Enclosure for oil lubricated, rotating elements
05/30/2002WO2002042623A2 Fan-stator interaction tone reduction
05/30/2002WO2002042610A2 Metallic honeycomb cellular seal-structure for a turbomachine
05/30/2002WO2002042150A1 Aircraft deicer
05/30/2002WO2002029292A3 Apparatus and methods for determining natural frequencies of brush seals
05/30/2002US20020064458 Frequency-mistuned light-weight turbomachinery blade rows for increased flutter stability
05/30/2002US20020064455 Methods and apparatus for sealing gas turbine engine variable nozzles
05/29/2002EP1209348A1 Silencing device, particularly for turbocharged engine
05/29/2002EP1208810A2 Ball bearing and ball bearing unit
05/29/2002EP1208809A2 Medical or dental hand-piece having at least one rotary part
05/29/2002DE10055882A1 Energy generator has turbine and generator mounted in skin vulcanized into tire and driven by air flow resulting from change of wheel profile volume when coming in contact with road
05/28/2002US6394755 Enhanced coating system for turbine airfoil applications
05/28/2002US6394750 Method and detail for processing a stator vane
05/28/2002US6394749 Apparatus and methods for relieving thermally induced stresses in inner and outer bands of thermally cooled turbine nozzle stages
05/28/2002US6394746 Gas turbine engine blade containment assembly
05/28/2002US6394108 Insertion flexible hose with nozzle; high pressure hot water containing detergents
05/28/2002US6393829 Coolant recovery type gas turbine
05/28/2002US6393827 Gas turbine fuel system comprising fuel oil distribution control system, fuel oil purge system, purging air supply system and fuel nozzle wash system
05/28/2002US6393825 System for pressure modulation of turbine sidewall cavities
05/28/2002CA2070440C Heat shield mechanism for turbine engines
05/28/2002CA2061939C Cooled shroud support
05/23/2002WO2002040884A1 Rotary machine with axial stop incorporating a current generator
05/23/2002DE10057861A1 Ball bearing for high speed devices has at least one device to produce RPM-dependent clamping force for bracing of bearing and comprises at least a part of balls of bearing
05/22/2002EP1207273A2 Aerodynamic devices for enhancing sidepanel cooling on an impingement cooled transition duct and related method
05/22/2002EP1207272A2 Replaceable variable stator vane for gas turbines
05/22/2002EP1206627A1 Turbine and method for discharging leakage fluid
05/22/2002EP1206626A1 Pressure-assisted electromagnetic thrust bearing
05/22/2002CN1350110A 涡轮机 Turbines
05/21/2002US6392313 Microturbomachinery
05/21/2002US6391115 Underplatform coating tool
05/21/2002US6390774 Gas turbine bucket cooling circuit and related process
05/21/2002US6390769 Closed circuit steam cooled turbine shroud and method for steam cooling turbine shroud
05/21/2002US6390418 Tangentially directed acoustic jet controlling boundary layer
05/21/2002US6389813 Passive mounted lining system
05/21/2002US6389797 Gas turbine combined cycle system
05/21/2002US6389795 Gas turbine fuel system comprising fuel oil distribution control system, fuel oil purge system, purging air supply system and fuel nozzle wash system
05/21/2002US6389793 Combustion turbine cooling media supply system and related method
05/16/2002WO2002038938A1 Bypass gas turbine engine and cooling method for working fluid
05/16/2002WO2001070424A3 Methods and apparatus for retrofitting compressible flanges
05/16/2002DE10052023C1 Austenitische Nickel-Chrom-Cobalt-Molybdän-Wolfram-Legierung und deren Verwendung Austenitic nickel-chromium-cobalt-molybdenum-tungsten alloy and the use thereof
05/15/2002EP1205641A2 Combined cycle gas turbine system
05/15/2002EP1205640A2 Combined system for cooling by water injection and washing of a gas turbine compressor
05/15/2002EP1205637A1 Cooling device for stator ring
05/15/2002EP1205635A2 Gas injector system and its fabrication
05/15/2002EP1092099B1 Thread and screwed assembly used at high temperatures
05/15/2002CN1349057A Hydraulic axial bearing having floating disc
05/15/2002CN1084823C Steam turbine with blades and use thereof
05/14/2002US6386827 Nozzle airfoil having movable nozzle ribs