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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04/29/2009 | EP2053213A1 Electric supercharger |
04/29/2009 | EP2053206A2 Gas turbine oil scavenging system |
04/29/2009 | EP2053205A1 Gas turbine engine systems involving integrated fluid conduits |
04/29/2009 | EP2053200A1 Control of the blade tip clearance of the high-pressure turbine of a turbomachine |
04/29/2009 | EP2053145A1 Method for removing a metal layer using FIC in an intermediate stage |
04/29/2009 | EP2052792A2 Drain valve, washing system and sensing of rinse and wash completion |
04/29/2009 | EP2051829A1 Method of producing or repairing turbine or engine components, and a component, namely a turbine or engine component |
04/29/2009 | CN201228564Y Supercharging turbine intermediate casing with quality durable tracing structure |
04/29/2009 | CN101418705A 300-400MW supercritical two-cylinder two-exhaust condensing turbine |
04/29/2009 | CN100482960C Hydrodynamic axial slide bearing for a generator |
04/29/2009 | CN100482864C Highly oxidation resistant component |
04/28/2009 | US7524167 Combustor spring clip seal system |
04/28/2009 | US7524166 Compressor cleaning system |
04/28/2009 | US7524164 Arrangement for the automatic running gap control on a two or multi-stage turbine |
04/28/2009 | US7524163 Nozzle guide vanes |
04/28/2009 | US7524161 Gas turbine engine blade containment assembly |
04/28/2009 | US7524112 Bearing support with double stiffener |
04/26/2009 | CA2639028A1 Gas turbine engine blade containment using wire wrapping |
04/23/2009 | WO2009051031A1 Method of repair |
04/23/2009 | WO2009049637A1 Fic installation and method for operating a fic installation in the pressure range above atmospheric pressure |
04/23/2009 | US20090104035 Advanced turbulator arrangements for microcircuits |
04/23/2009 | US20090104030 Assembly |
04/23/2009 | US20090104029 Flow Machine |
04/23/2009 | US20090104028 Method and apparatus for distributing fluid into a turbomachine |
04/23/2009 | US20090104026 Control of clearance at blade tips in a high-pressure turbine of a turbine engine |
04/23/2009 | US20090101787 Gas Turbine Engine Systems Involving Rotatable Annular Supports |
04/23/2009 | DE102007050124A1 Gehäuse für ein Laufrad Housing for a wheel |
04/23/2009 | CA2639025A1 Gas turbine oil scavenging system |
04/22/2009 | EP2050968A1 Pressure container with a cover |
04/22/2009 | EP2050942A2 Turbocharger mounting system |
04/22/2009 | EP2050932A2 A shaft bearing arrangement in a gas turbine engine and a method for operating this bearing arrangement |
04/22/2009 | EP2050929A1 Compressor blade, especially for the fan on plane engines |
04/22/2009 | EP2050928A2 Method and apparatus for hole crack removal |
04/22/2009 | EP2050925A2 A shaft bearing arrangement and corresponding method of operating this arrangement |
04/22/2009 | EP1444491B1 Vibration monitoring system for gas turbine engines |
04/22/2009 | CN101415961A Rolling bearing and supercharger using the same |
04/22/2009 | CN101415907A Steam turbine installation and associated operating method |
04/22/2009 | CA2642059A1 Wall of combustion chamber with optimal dilution and cooling, combustion chamber and turbine engine so equipped |
04/22/2009 | CA2641963A1 Blade tip clearance control for a turbine engine high-pressure turbine |
04/21/2009 | US7520721 System and method for aligning and sealing a turbine shell assembly |
04/21/2009 | US7520369 Soundproofing panel with beads, and a method of manufacture |
04/16/2009 | WO2009048455A1 A gas turbine engine |
04/16/2009 | WO2009047543A1 Device for inhibiting the flow of oil along a rotating shaft |
04/16/2009 | WO2009047538A1 Turbomachine |
04/16/2009 | WO2008139095A3 Method for assembling end to end two parts having different thermal expansion coefficients and assembly thus obtained |
04/16/2009 | US20090097978 Fan blade assembly |
04/16/2009 | US20090097968 Apparatus and method for clearance control of turbine blade tip |
04/16/2009 | US20090097962 Compressor inlet guide vane flow based anti-ice formation control system and method |
04/16/2009 | US20090095875 Turbocharger mounting system |
04/16/2009 | CA2640279A1 Substantially cylindrical composite articles and fan casings |
04/16/2009 | CA2638661A1 Exhaust duct with bypass channel |
04/15/2009 | EP2048423A1 Casing for a turbomachine and corresponding turbomachine |
04/15/2009 | EP2048367A1 Casing with cooling device for a process gas turbo compressor |
04/15/2009 | EP2048330A2 Systems and methods involving multiple torque paths for gas turbine engines |
04/15/2009 | EP2047070A1 Particle vibration damper |
04/15/2009 | CN101408114A Apparatus and method for clearance control of turbine blade tip |
04/15/2009 | CN100478121C Device for demounting of a turbine or compressor blade |
04/15/2009 | CN100478088C Nozzle and method for washing gas turbine compressors |
04/14/2009 | US7517189 Cooling circuit for gas turbine fixed ring |
04/14/2009 | US7517187 High-speed rotor assembly for an overhung centrifugal compressor |
04/14/2009 | US7517184 Low deflection fan case cotainment fabric |
04/14/2009 | CA2412906C Drainage system for gas turbine supporting bearings |
04/14/2009 | CA2407954C Device for controlling the cooling flows of gas turbines |
04/14/2009 | CA2282006C Brush seal and rotary machine including such brush seal |
04/11/2009 | CA2640788A1 Turbine stator for aircraft turbine engine including a vibration damping device |
04/09/2009 | WO2009043809A1 Hydrodynamic axial bearing |
04/09/2009 | WO2009043659A2 A turbomachine |
04/09/2009 | WO2009019153A3 Turbocharger comprising a cooling device and an oil supply pipe |
04/09/2009 | WO2008097276A3 Adjustable turbine exhaust flow guide and bearing cone assemblies |
04/09/2009 | US20090092499 Air Inlet Cover |
04/09/2009 | US20090092492 Balancing group for the rotor of a fluid rotary machine |
04/09/2009 | US20090092489 Expansion turbine |
04/09/2009 | US20090092477 Economizer for air conditioning system or the like |
04/09/2009 | DE102007045300A1 Gas turbine rotor manufacturing method, involves determining circumferential position of blades such that resultant unbalance is smaller than predetermined threshold value, and realizing determination of position by evolutionary algorithm |
04/09/2009 | DE102004009412B4 Abgasturbolader Exhaust gas turbocharger |
04/09/2009 | CA2699711A1 Hydrodynamic axial bearing |
04/08/2009 | EP2045472A1 Method for assembling large turbo machines and device for implementation of the same |
04/08/2009 | EP2045448A1 Low-noise exhaust gas facility |
04/08/2009 | EP2045447A1 Turbofan engine intermediate casing and corresponding turbofan engine |
04/08/2009 | EP2045445A2 Shroud segment, corresponding casting core and method for cooling this segment |
04/08/2009 | EP2045442A1 Assembly with a heat source, heat sink and a shaft |
04/08/2009 | EP2044296A2 A gas turbine arrangement |
04/08/2009 | EP2044295A2 Power system |
04/08/2009 | EP2044292A1 Turbine housing for a turbocharger |
04/08/2009 | EP2000684A9 Rolling bearing and supercharger using the same |
04/08/2009 | CN201218112Y Air-cooling turbine generator bearing |
04/08/2009 | CN101405579A Flowmeter for determining a flow direction |
04/08/2009 | CN101405480A High-speed rotating shaft for supercharger |
04/08/2009 | CN101405422A Thermal insulation layer system |
04/08/2009 | CN101403320A Assembly type nozzle diaphragm |
04/07/2009 | US7513755 Submerged motor and pump assembly |
04/07/2009 | US7513740 Turbine ring |
04/07/2009 | US7513736 Equipment for the aeration of a rotor hub of a wind energy plant |
04/07/2009 | US7513040 Manufacturable and inspectable cooling microcircuits for blade-outer-air-seals |
04/07/2009 | CA2422000C A lead-in structure and a fixing flange for a turbo generator |
04/04/2009 | CA2640208A1 Turbojet intermediate housing and turbojet |
04/02/2009 | WO2009042069A2 Improved ring segment coolant seal configuration |
04/02/2009 | WO2009041436A1 Gas turbine combustor |
04/02/2009 | WO2009041435A1 Cooling structure for gas-turbine combustor |
04/02/2009 | WO2009039835A1 Flow structure for a turbocompressor |