Patents
Patents for F01D 25 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups (22,148)
09/2002
09/17/2002US6449957 Gas turbine generator plant with equipment support
09/17/2002US6449952 Removable cowl for gas turbine combustor
09/17/2002US6449950 Rotor and bearing system for electrically assisted turbocharger
09/12/2002WO2002070867A1 Methods and apparatus for cooling gas turbine engine blade tips
09/12/2002WO2002053900A3 Fluid and fuel delivery system reducing pressure fluctuations
09/12/2002US20020127112 Enhanced coating system for turbine airfoil applications
09/12/2002US20020127103 Cooled gas turbine blade
09/12/2002US20020127102 Method and apparatus for centering rotor assembly damper bearings
09/12/2002US20020127101 Stator vane for an axial flow turbine
09/12/2002US20020127100 Low-pressure steam turbine with multi-channel diffuser
09/12/2002US20020124874 Cleaner for high pressure hot water comprising an insert and flexible hose with radial nozzles; cleans from the back forward giving a different blast angle with higher pressure water for improved turbine power and fuel efficiency
09/12/2002DE10125250C1 Axial turbine for exhaust gas turboloader, has exhaust gas diffuser whose outer wall is in two radial sections with annular support wall between them
09/12/2002DE10110804A1 Production of a metallic layer on the inner side of a turbine housing of an internal combustion engine comprises directly applying the layer as a single corrosion protection layer on the surface
09/11/2002EP1239121A2 An air-cooled gas turbine exhaust casing
09/10/2002US6447248 Bearing support fuse
09/10/2002US6447247 Steam turbine
09/05/2002US20020123827 System and method for performing electronic triage of a turbine part
09/05/2002US20020122726 Tip treatment bar components
09/05/2002US20020122721 Tip treatment assembly for a gas turbine engine
09/05/2002US20020122719 Tip treatment bar with a damping material
09/05/2002US20020122718 Tip treatment bars for gas turbine engines
09/05/2002US20020122717 Low drag ducted ram air turbine generator and cooling system
09/05/2002US20020122716 Methods and apparatus for cooling gas turbine engine blade tips
09/05/2002US20020122458 Utilization of pyrometer data to detect oxidation
09/05/2002US20020121082 Air-cooled gas turbine exhaust casing
09/04/2002EP1236864A2 System and method for perfoming electronic triage of a turbine part and for carrying out a turbine part repair
09/04/2002EP0968355B1 Cooling supply manifold assembly for cooling combustion turbine components
09/04/2002EP0870136B1 Circumferential seal with ceramic rotor
09/03/2002US6445995 Vibration sensing in gas turbine engine
09/03/2002US6443698 Method and apparatus for centering rotor assembly damper bearings
09/03/2002US6443695 Steam turbine
09/03/2002US6443694 Rotor machine device
09/03/2002US6442946 Three degrees of freedom aft mounting system for gas turbine transition duct
09/03/2002US6442944 Bleed air heat exchanger integral to a jet engine
08/2002
08/29/2002WO2002042150B1 Aircraft deicer
08/29/2002WO2002018674A3 Thermal barrier coating system for turbine components
08/28/2002EP1235010A2 Repositionable brush seal for turbomachinery
08/28/2002EP1060345B1 Method for operating a gas and steam turbine installation and the gas and steam turbine installation
08/28/2002CN2507999Y Independent lubricating device for turbocharger
08/28/2002CN1366144A 涡轮压缩机 Turbo Compressor
08/28/2002CA2372353A1 Torque pin
08/27/2002US6440521 Method for transferring heat in an aircraft engine thrust reverser
08/27/2002US6439842 Gas turbine engine stator case
08/27/2002US6439841 Turbine frame assembly
08/27/2002US6439836 Cryogenic turbo-expander
08/27/2002US6439772 Method and apparatus for supporting rotor assembly bearings
08/27/2002US6439616 Anti-rotation retainer for a conduit
08/27/2002US6439023 Methods and apparatus for retrofitting compressible flanges
08/27/2002US6438962 System and method for starting an engine
08/27/2002US6438938 Bearing compartment self cooling vent system
08/27/2002US6438838 Method for repairing and producing integrally bladed rotors for a turbine or turbo engine
08/22/2002US20020114700 Airfoil configured for moisture removal from steam turbine flow path
08/22/2002US20020114696 Gas turbine nozzle vane insert and methods of installation
08/22/2002US20020112535 Test bed for a thrust reverser
08/21/2002EP1233147A2 Gas turbine with cooling arrangement
08/21/2002EP1233146A2 Gas turbine nozzle vane insert and methods of installation
08/21/2002CN1365422A Component and method for guiding a hot pressured medium
08/21/2002CN1089408C Axial turbine of turbocharger
08/20/2002US6435831 Gas-turbine rotor
08/20/2002US6435820 Shroud assembly having C-clip retainer
08/20/2002US6435819 Turbo machines
08/20/2002US6435816 Gas injector system and its fabrication
08/20/2002US6435814 Film cooling air pocket in a closed loop cooled airfoil
08/20/2002US6435813 Impigement cooled airfoil
08/20/2002US6435011 Method and apparatus for determining if brush seals are defective
08/15/2002WO2001040548A9 Chemical cleaning solution for gas turbine blades
08/15/2002US20020110450 Air bearing articulated shaft and floating module configuration for a small rotary compressor
08/15/2002US20020109249 Method for removing volatile components from a gel-cast ceramic article
08/15/2002US20020108810 Exhaust gas system with helmholtz resonator
08/15/2002US20020108379 Gas turbine
08/14/2002CN1089136C Exhaust duct for steam turbine
08/13/2002US6431833 Gas turbine bucket with impingement cooled platform
08/13/2002US6431820 Methods and apparatus for cooling gas turbine engine blade tips
08/13/2002US6431756 Bearing damper
08/13/2002US6430917 Single rotor turbine engine
08/08/2002US20020107161 A single phase engine cleaner solution comprising a polar solvent, non-polar solvent, immiscible with polar solvent, and a fugitive cosolvent having a higher evaporation rate than the polar solvent and the non-polar solvent;
08/08/2002DE10102606A1 Kühlung von Gehäusen, Rotor, Schaufeln und/oder Brennern von Turbinen Cooling of housings, rotor blades and / or turbine burners
08/07/2002EP1229146A2 Oxidation resistant coatings for niobium-based silicide composites
08/07/2002CN1088809C Retaining arrangement for a bearing, in particular for a high pressure compressor shaft
08/06/2002US6428269 Turbine engine bearing support
08/06/2002US6427448 Gas turbine and method of cooling a turbine stage
08/06/2002CA2273058C Adjustable compressor bundle insertion and removal system
08/01/2002WO2002059490A1 Hydrodynamic axial slide bearing for a generator
08/01/2002WO2002044538A3 Device for centring a tube in a turbine shaft
08/01/2002WO2002036999A3 High-stability valve arrangement for a governor valve
08/01/2002US20020103093 Method and composition for cleaning a turbine engine component
08/01/2002US20020102158 Impeller of axial-flow blower
08/01/2002US20020100492 Method of cleaning turbine component using laser shock peening
08/01/2002DE10037837C2 Aufhängung Suspension
07/2002
07/31/2002EP1227325A1 Sensor for speed and vibration
07/31/2002EP1227255A2 Bi-directional tapered roller bearing
07/31/2002EP1227254A1 Thrust bearing for a generator
07/31/2002EP1227222A2 Utilization of pyrometer data to detect oxidation
07/31/2002EP1227220A1 Coupling structure for expansion unit output shaft and driven-side transmission shaft
07/31/2002EP1227217A2 Gas turbine
07/31/2002CN1361350A Cooling system and method for cooling fluid mechanical shell
07/30/2002US6425736 Stator assembly for a rotary machine and method for making the stator assembly
07/25/2002WO2001076348A3 Improved brush-seal designs for turbines and similar rotary apparatus
07/25/2002US20020098082 Gas turbine
07/25/2002US20020098079 Gas turbine split ring