| Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915) |
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| 12/06/2007 | WO2007139694A2 Blade tip coatings using high purity powders |
| 12/06/2007 | WO2007138055A1 Method of adapting a gas turbine so that it can consume a fuel of low calorific value |
| 12/06/2007 | WO2007138018A1 Component for a thermal stress, in particular a turbine blade |
| 12/06/2007 | WO2007137924A1 Diffuser |
| 12/06/2007 | WO2007137903A1 Method for spark-erosive treatment of electrically nonconductive materials |
| 12/06/2007 | WO2007137902A1 Peening device |
| 12/06/2007 | WO2007137884A1 Welded low-pressure turbine shaft |
| 12/06/2007 | WO2007081817A3 Electric turbine bypass fan and compressor for hybrid propulsion |
| 12/06/2007 | US20070280832 Turbine airfoil with floating wall mechanism and multi-metering diffusion technique |
| 12/06/2007 | US20070280831 Rotor disk and blade arrangement |
| 12/06/2007 | US20070280830 Aerofoil stage and seal for use therein |
| 12/06/2007 | US20070280819 Gas turbine engine case and method of making |
| 12/06/2007 | US20070277527 Dual-use radial turbomachine |
| 12/06/2007 | DE102006026207A1 Bauteil für eine thermische Beanspruchung, insbesondere Turbinenschaufel Component for thermal stress, especially turbine blade |
| 12/06/2007 | DE102006025883A1 Integral bladed gas turbine rotor for gas turbine aircraft engine, has shrouding band designed as closed ring, and resting against outside sections of rotor blades in resting condition and in operation of rotor by compression stress |
| 12/06/2007 | CA2653270A1 Blade tip coatings using high purity powders |
| 12/05/2007 | EP1862655A1 Method of adapting a gas turbine so that it can consume a fuel of low calorific value |
| 12/05/2007 | EP1862643A2 Pre-coating burnishing of erosion coated parts |
| 12/05/2007 | EP1862642A2 Rotor blade of a first phase of a vapor turbine with a fork foot and covering belt |
| 12/05/2007 | EP1862641A1 Annular flow channel for axial flow turbomachine |
| 12/05/2007 | EP1862640A1 Turbine blade |
| 12/05/2007 | EP1862639A1 Device for optimizing cooling in gas turbines |
| 12/05/2007 | EP1862638A1 Method for repairing the rotor of a gas turbine and rotor of a gas turbine |
| 12/05/2007 | CN101082287A Rotor blade of a first phase of a vapor turbine with a fork foot and covering belt |
| 12/05/2007 | CN101082286A 涡轮叶片 Turbine blades |
| 12/05/2007 | CN100353032C Open-cooled component for a gas turbine, combustion chamber, and gas turbine |
| 12/05/2007 | CN100353031C 透平叶片 Turbine blades |
| 12/05/2007 | CN100353030C Mutti-assembly mixing turbine blade |
| 12/04/2007 | US7303638 Cold-forming a predetermined, pretreated Ti alloy into a cold-formed shape; subjecting the cold-formed shape to a post-forming annealing cycle comprising: heating the cold-formed shape, holding, cooling the cold-formed shape to room temperature |
| 12/04/2007 | US7303377 Apparatus and method of balancing a shaft |
| 12/04/2007 | US7303376 Turbine airfoil with outer wall cooling system and inner mid-chord hot gas receiving cavity |
| 12/04/2007 | US7303375 Refractory metal core cooling technologies for curved leading edge slots |
| 12/04/2007 | US7302990 Method of forming concavities in the surface of a metal component, and related processes and articles |
| 12/04/2007 | CA2312951C Cover plate for gas turbine rotor |
| 12/04/2007 | CA2185854C Damper disposition mounted between rotor vanes |
| 11/29/2007 | WO2007134586A1 Device for carrying out an inductive low-frequency or high-frequency pressure welding method, comprising an insulator located between the inductor and the components in the zone of the joint |
| 11/29/2007 | WO2007093851A3 Airfoil for a third stage nozzle guide vane |
| 11/29/2007 | WO2007053157A3 Turbine engine |
| 11/29/2007 | US20070275210 improve the cooling in a layer structure; used for turbine components of a turbomachine, such as a gas turbine; improved mechanical bonding of the pore walls to the substrate |
| 11/29/2007 | US20070274832 Rotor For A Turbo Machine And Method For The Manufacture Of Such A Rotor |
| 11/29/2007 | US20070274831 Holder for holding a metal component part of a turbine |
| 11/29/2007 | US20070274823 Method For Reducing The Noise Of Turbo Engines |
| 11/29/2007 | DE112004000100B4 Gekühlte Schaufeln eines Gasturbinentriebwerks -Cooled blades of a gas turbine engine |
| 11/29/2007 | DE102007011508A1 Brennkraftmaschine mit Abgasturbine und Abgasrückführung Internal combustion engine with exhaust gas turbine and exhaust gas recirculation |
| 11/29/2007 | CA2652359A1 Device for carrying out an inductive low-frequency or high-frequency pressure welding method, comprising an insulator located between the inductor and the components in the zone of the joint |
| 11/28/2007 | EP1860325A1 Diffuser |
| 11/28/2007 | EP1860280A1 Locking device of a turbine blade with a locking element |
| 11/28/2007 | EP1860279A1 Welded LP-turbine shaft |
| 11/28/2007 | EP1859897A1 Method of manufacturing a turbomachine rotor disk. |
| 11/28/2007 | EP1859889A1 A method of manufacturing a component made of two workpieces through Hot Isostatic pressure with deposition of a coating with reduced density on at least one of the workpieces |
| 11/28/2007 | EP1502008B1 Device for fixing a rotor on a shaft |
| 11/28/2007 | CN101078355A Airfoil and method for moisture removal and steam injection |
| 11/28/2007 | CN101078354A Porous metal vane coupling design method |
| 11/28/2007 | CN100351496C Continuous radial loader for steam turbine reaction blade and its method |
| 11/28/2007 | CN100351495C Turbine blade pocket shroud |
| 11/27/2007 | US7300708 shape memory alloy to decrease the rate of wear/erosion of the blade due to contact of the blade with its surrounding shroud |
| 11/27/2007 | US7300256 Damping arrangement for a blade of an axial turbine |
| 11/27/2007 | US7300255 Laminated turbomachine airfoil with jacket and method of making the airfoil |
| 11/27/2007 | US7300253 Gas turbine blade or vane and platform element for a gas turbine blade or vane ring of a gas turbine, supporting structure for securing gas turbine blades or vanes arranged in a ring, gas turbine blade or vane ring and the use of a gas turbine blade or vane ring |
| 11/27/2007 | US7300252 Gas turbine airfoil leading edge cooling construction |
| 11/27/2007 | US7300251 Turbine cooling vane of gas turbine engine |
| 11/27/2007 | US7300250 Cooled airfoil trailing edge tip exit |
| 11/24/2007 | CA2589077A1 Manufacturing process for a turbine engine rotor disk |
| 11/22/2007 | WO2007133204A1 BLADE/DISK DOVETAIL BACKCUT FOR BLADE/DISK STRESS REDUCTION (6FA+e, STAGE 2) |
| 11/22/2007 | US20070269608 Rotor repair method and rotor repair apparatus |
| 11/22/2007 | US20070269315 Rotor assembly for a rotary machine |
| 11/22/2007 | US20070269309 Method for Operating a Liquid Ring Compressor |
| 11/22/2007 | US20070266707 Boundary Layer Suction Arrangement |
| 11/22/2007 | DE102006022683A1 Flugtriebwerk-Baugruppe, nämlich Verdichter oder Turbine eines Flugtriebwerks, Flugtriebwerk-Bauteil sowie Verfahren zur Herstellung oder Instandsetzung eines Flugtriebwerk-Bauteils Aircraft engine assembly, namely the compressor or turbine aircraft engine, aircraft engine component and methods for making or repairing an aircraft engine-component |
| 11/22/2007 | CA2651931A1 Fluid energy converter |
| 11/21/2007 | EP1857636A1 Turbine blade and method for matching the platform stiffness with that of the airfoil portion |
| 11/21/2007 | EP1857635A1 Turbine blade for a gas turbine |
| 11/21/2007 | EP1857217A1 High pressure turbine airfoil recovery device and method of heat treatment |
| 11/21/2007 | EP1856306A1 Component, in particular, a gas turbine component |
| 11/21/2007 | CN100350134C Method and apparatus to facilitate sealing within turbines |
| 11/21/2007 | CN100350133C Device for fixing a blade on a rotor disc of a turbomachine, turbomachine and method to assemble and disassemble a blade on a rotor disc of a turbomachine |
| 11/21/2007 | CN100350132C 透平叶片 Turbine blades |
| 11/21/2007 | CN100350131C Wing surface of secondary turbine blade |
| 11/21/2007 | CN100350075C High-temperature protection layer |
| 11/20/2007 | US7296976 Dual counterweight balancing system |
| 11/20/2007 | US7296973 Parallel serpentine cooled blade |
| 11/20/2007 | US7296972 Turbine airfoil with counter-flow serpentine channels |
| 11/20/2007 | US7296967 Counterflow film cooled wall |
| 11/20/2007 | US7296966 Methods and apparatus for assembling gas turbine engines |
| 11/20/2007 | CA2482388C Sealing arrangement for an axial turbine wheel |
| 11/20/2007 | CA2307050C Cover for a component surface |
| 11/17/2007 | CA2587311A1 High pressure turbine airfoil recovery device and method of heat treatment |
| 11/16/2007 | CA2576620A1 Airfoil prognosis for turbine engines |
| 11/15/2007 | US20070264126 Method of Protecting a Component Against Hot Corrosion |
| 11/15/2007 | US20070264125 Lightweight Heat-Resistant Material for Generator Gas Turbine |
| 11/14/2007 | EP1855011A1 Assembly for the engine compressor of an aircraft comprising tilted-head hammer attachment vanes |
| 11/14/2007 | EP1854899A1 Alloy, protective layer and component |
| 11/14/2007 | EP1854898A1 Alloy, protective layer and component |
| 11/14/2007 | EP1853795A1 Method for manifacturing an integrally bladed rotor |
| 11/14/2007 | EP1759091B1 Turbine wheel in a waste gas turbine of a waste gas turbocharger |
| 11/14/2007 | CN100348838C Rotor blade for a centripetal turbine |
| 11/14/2007 | CN100348373C Power tool |
| 11/13/2007 | US7294413 Substrate protected by superalloy bond coat system and microcracked thermal barrier coating |
| 11/13/2007 | US7294361 Method and device for gas phase diffusion coating of metal components |
| 11/13/2007 | US7293964 Repair method for a blade of a turbomachine |