| 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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| 04/06/2010 | US7690885 Methods and system for shielding cooling air to facilitate cooling integral turbine nozzle and shroud assemblies |
| 04/01/2010 | WO2010036533A2 Turbocharger and blade bearing ring therefor |
| 04/01/2010 | WO2010036532A2 Turbocharger and subassembly for bypass control in the turbine casing therefor |
| 04/01/2010 | WO2010034412A1 Method for repairing a housing of an aircraft engine |
| 04/01/2010 | US20100080698 Method and apparatus for matching the thermal mass and stiffness of bolted split rings |
| 04/01/2010 | US20100080691 Magnetic adjustment of turbomachinery components |
| 04/01/2010 | US20100080689 Gas turbine engine rotor and balance weight therefor |
| 04/01/2010 | US20100080688 Hot gas component of a turbomachine including an embedded channel |
| 04/01/2010 | US20100077721 Composite fan case with integral containment zone |
| 04/01/2010 | DE102009044089A1 Verfahren und Vorrichtung zur Anpassung der thermisch wirksamen Masse und Steifigkeit von verschraubten Teilringen Method and apparatus for adjusting the thermal mass and stiffness of bolted partial rings |
| 03/31/2010 | EP2169186A2 Sealing arrangement for the compressor side of a turbocharger of a combustion engine and corresponding method for sealing of this compressor side |
| 03/31/2010 | EP2169185A1 Steam turbine |
| 03/31/2010 | EP2169184A2 Apparatus and method for removing gas turbine compressor stator vane segments with rotor in place |
| 03/31/2010 | EP2167792A1 Turbocharger having a turbocharger housing |
| 03/31/2010 | EP2167256A1 A method for producing an annular wall structure |
| 03/31/2010 | CN201433795Y Special scale eliminator for turbine |
| 03/31/2010 | CN101688448A Turbine arrangement and method of cooling a shroud located at the tip of a turbine blade |
| 03/30/2010 | US7688585 Fan mounting apparatus for heat dissipation |
| 03/30/2010 | US7688579 Portable electronic device incorporating thermal module |
| 03/30/2010 | US7687021 forming cavity of shape corresponding to shape of shroud of casing, securing soluble cores to mold, filling cavity with a metal alloy powder, sintering said powder by hot isostatic pressing, eliminating the cores and the inserts by dissolving them and extracting shroud |
| 03/30/2010 | US7686577 Stacked laminate fiber wrapped segment |
| 03/30/2010 | US7686576 Method and apparatus for assembling gas turbine engines |
| 03/30/2010 | US7686575 Inner ring with independent thermal expansion for mounting gas turbine flow path components |
| 03/30/2010 | US7685827 Gas turbine cooling systems and methods of assembly |
| 03/30/2010 | CA2447279C Fuel metering device with compensated regulator valve in a turbine engine |
| 03/30/2010 | CA2445237C Method of repairing a stationary shroud of a gas turbine engine using plasma transferred arc welding |
| 03/30/2010 | CA2406479C Weep plug |
| 03/25/2010 | WO2010033996A2 Fabricated turbine housing |
| 03/25/2010 | WO2010033414A2 Exhaust-gas turbocharger |
| 03/25/2010 | WO2010031948A1 Method and system for lubricating a turbine engine |
| 03/25/2010 | WO2010002717A3 Bearing housing body group of an exhaust-gas turbocharger |
| 03/25/2010 | US20100074739 Passive boundary layer bleed system for nacelle inlet airflow control |
| 03/25/2010 | US20100074737 Steam turbine |
| 03/25/2010 | US20100074735 Thermal Shield at Casing Joint |
| 03/25/2010 | US20100074729 Compressible Ceramic Seal |
| 03/25/2010 | US20100074726 Gas turbine airfoil |
| 03/25/2010 | DE102009003519A1 Systeme und Verfahren zum internen Kühlen eines Rades einer Dampfturbine Systems and methods for internal cooling of a wheel of a steam turbine |
| 03/25/2010 | DE102008048126A1 Exhaust gas turbocharger i.e. supercharger, for use in vehicle, has rotor provided with compressor part and turbine part, where rotor is radially and/or axially mounted only at axial ends in pivotable manner |
| 03/25/2010 | CA2738093A1 Method and system for lubricating a turbine engine |
| 03/24/2010 | EP2166196A2 Continuous supply oil tank for zero and negative G operation |
| 03/24/2010 | EP2166195A2 Fluid reservoir in a gas turbine engine |
| 03/24/2010 | EP2166194A2 Dual stage turbine shroud |
| 03/24/2010 | EP2165108A2 Composite flange, duct incorporating a flange and method of making a flange |
| 03/24/2010 | CN201428518Y Gas turbine self-cleaning air inlet screen monitor |
| 03/24/2010 | CN201428510Y Turbocharger for diesel engine |
| 03/24/2010 | CN201428481Y Packaging and lubricating device of steam turbine |
| 03/24/2010 | CN201428480Y Supporting device of high pressure cylinder and front bearing box of steam turbine |
| 03/24/2010 | CN101680309A Housing for a turbomachine |
| 03/24/2010 | CN101680306A Blade structure for turbine |
| 03/24/2010 | CN101680305A Diffuser arrangement |
| 03/24/2010 | CN101680059A Ni-based single crystal superalloy and turbine vane using the same |
| 03/24/2010 | CN101676522A Conical pin to maintain bearing system |
| 03/23/2010 | US7683497 Turbomachinery electric generator arrangement |
| 03/23/2010 | US7682130 Device and method for cooling a housing of a gas turbine or a combustion chamber |
| 03/23/2010 | US7681402 Aeroengine oil tank fire protection system |
| 03/23/2010 | CA2678988A1 Air filter mounting system and method for fabricating the same |
| 03/23/2010 | CA2451318C Method and apparatus to decrease gas turbine engine combustor emissions |
| 03/23/2010 | CA2403720C Safety device for a washing system for liquid fuel burners in gas turbines |
| 03/18/2010 | WO2010030448A1 Intershaft seal system |
| 03/18/2010 | WO2010028729A1 Improvements in or relating to engine monitoring and control |
| 03/18/2010 | US20100068051 Integrated inlet fan case |
| 03/18/2010 | US20100068043 Cooling structure for outer surface of a gas turbine case |
| 03/18/2010 | US20100068034 CMC Vane Assembly Apparatus and Method |
| 03/18/2010 | US20100065680 Device with plane jets for reducing the noise generated by a jet aircraft |
| 03/18/2010 | US20100065375 Reduced gulp fluid reservoir |
| 03/18/2010 | US20100065374 Continuous supply fluid reservoir |
| 03/18/2010 | DE102008046946A1 Axial bearing for shaft of exhaust turbocharger, has disk-shaped bearing box, which has bearing element, where bearing box is made of inner bearing flange carrying bearing element |
| 03/17/2010 | EP2163749A1 Blast furnace gas burning facility and its operation method |
| 03/17/2010 | EP2163734A2 Gas turbine vane attachment |
| 03/17/2010 | EP2163733A2 Lubricant scavenge arrangement |
| 03/17/2010 | EP2163732A2 Turbine bearing locating mechanism |
| 03/17/2010 | EP2163731A1 High performance thrust bearing pad |
| 03/17/2010 | EP2163725A2 Turbine blade damper arrangement |
| 03/17/2010 | EP2162598A2 Turbine airfoil cooling system with rotor impingement cooling |
| 03/17/2010 | CN201424967Y Backpressure steam turbine |
| 03/17/2010 | CN201424966Y Backpressure steam turbine |
| 03/17/2010 | CN101675228A Gas turbine combustor |
| 03/17/2010 | CN101675227A Cooling structure for gas-turbine combustor |
| 03/17/2010 | CN101673318A Method for designing optimal static parameter of radial static pressure gas bearing of turbine expansion engine |
| 03/17/2010 | CN101672216A High performance thrust bearing pad |
| 03/17/2010 | CN101672202A Flow inhibitor of turbomachine shroud |
| 03/17/2010 | CN101671785A High-temperature-resistant cobalt-base superalloy |
| 03/16/2010 | CA2481068C Anisotropic support damper for a gas turbine bearing |
| 03/11/2010 | WO2010026182A1 Method for making a circular revolution thermomechanical part comprising a carrier substrate containing titanium coated with steel or a superalloy, and titanium fire-resistant compressor casing for a turbine engine obtained by said method |
| 03/11/2010 | WO2010026181A1 Method for making a circular revolution thermomechanical part comprising a carrier substrate containing titanium coated with steel or a superalloy, and titanium fire-resistant compressor casing for a turbine engine obtained by said method |
| 03/11/2010 | WO2010026180A1 Compressor casing resistant to titanium fire, high pressure compressor including such a casing, and aircraft engine including such a compressor |
| 03/11/2010 | WO2010026179A1 Method for making a circular revolution thermomechanical part including a carrier substrate containing titanium coated with steel or a superalloy, and titanium fire-resistant compressor casing for a turbine engine obtained by said method |
| 03/11/2010 | WO2010026005A1 Turbine rotor blade having an adapted natural frequency by means of an insert |
| 03/11/2010 | WO2010025880A1 Horizontally and vertically adjustable bearing |
| 03/11/2010 | WO2010007220A3 Turbomachine structural casing |
| 03/11/2010 | US20100061855 System for providing continuous lubrication to engine turbocharger shaft and bearing arrangement |
| 03/11/2010 | US20100061851 Secondary Air Charger |
| 03/11/2010 | US20100061848 Flow inhibitor of turbomachine shroud |
| 03/11/2010 | US20100061845 Guiding device of a flow machine and guide vane for such a guiding device |
| 03/11/2010 | US20100059131 Noise Level Reduction of Sparger Assemblies |
| 03/11/2010 | US20100058729 Lubricant scavenge arrangement |
| 03/11/2010 | DE102008046582A1 Exhaust gas turbocharger for internal combustion engine, particularly motor vehicle, has shaft, which is pivoted in housing of exhaust gas turbocharger |
| 03/11/2010 | DE102008046347A1 Rotordrehvorrichtung für eine Dampfturbine Rotor apparatus for a steam turbine |
| 03/11/2010 | DE102008045657A1 Vorrichtung und Verfahren zur Reduzierung des Drucks auf eine Trennfuge zwischen wenigstens zwei Begrenzungsteilen Apparatus and method for reducing the pressure to a parting line between at least two limiting parts |
| 03/11/2010 | DE102008045654A1 Dampfturbine mit Magnetlagerkühlung Steam turbine with magnetic bearing cooling |