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