| 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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| 05/25/2006 | US20060110247 Pattern for the surface of a turbine shroud |
| 05/25/2006 | US20060110211 Infinitely adjustable engagement system and method |
| 05/24/2006 | EP1659265A1 Turbine vane segment with cooling air supplying system |
| 05/24/2006 | EP1659264A2 Airfoil with supplemental cooling channel adjacent leading edge |
| 05/24/2006 | EP1659263A2 Cooling system for a gas turbine airfoil |
| 05/24/2006 | EP1659262A1 Cooled gas turbine blade and cooling method thereof |
| 05/24/2006 | EP1658924A1 Part with a filled recess |
| 05/24/2006 | EP1658923A2 Method for making a repaired turbine engine stationary vane assembly and repaired assembly |
| 05/24/2006 | EP1204532A4 One-step noble metal-aluminide coatings |
| 05/24/2006 | DE19654471B4 Rotor einer Strömungsmaschine Rotor of a turbomachine |
| 05/24/2006 | DE102005040304A1 Verfahren und Vorrichtung zur Kühlung von Gasturbinentriebwerksläufern Method and apparatus for cooling gas turbine engine rotors |
| 05/24/2006 | CN2782936Y Equal strength vane structure for impeller of radial flow turbine |
| 05/24/2006 | CN1776199A Cooling system for an airfoil |
| 05/24/2006 | CN1776025A Hard composibe nlano ceramic film cladding for use on surface of turbine blade |
| 05/23/2006 | US7048509 Axial flow turbine |
| 05/23/2006 | US7048508 Rotor end piece |
| 05/23/2006 | US7048507 Axial-flow thermal turbomachine |
| 05/23/2006 | US7048502 Fluid coupling |
| 05/23/2006 | US7048497 Gas turbine stator |
| 05/23/2006 | CA2491476C An arrangement for sealing a steam-cooled gas turbine |
| 05/18/2006 | WO2006052278A2 Ceramic matrix composite airfoil trailing edge arrangement |
| 05/18/2006 | US20060105192 Pre-creased sheet metal coil stock |
| 05/18/2006 | US20060104819 Low-noise fan exit guide vanes |
| 05/18/2006 | US20060104818 Blade |
| 05/18/2006 | US20060104814 Heat transfer arrangement |
| 05/18/2006 | US20060104813 Cooling system for an airfoil |
| 05/18/2006 | US20060104808 Turbine blade cooling system |
| 05/18/2006 | US20060102800 Method and apparatus for modulating flow separation |
| 05/18/2006 | DE10245197B4 Verfahren zum Fräsen von tiefen Nuten zur Herstellung mehreren zueinander paralleler, hinsichtlich der Fräsbearbeitung instabiler Wänden an einem Werkstück Process for milling of deep grooves for preparing a plurality of mutually parallel, unstable with respect to the milling walls on a workpiece |
| 05/18/2006 | DE102005019937B3 Turbine for exhaust gas turbocharger, has auxiliary blades, which are dimensioned such that throughput parameter of turbine wheel blades is set to throughput parameter of auxiliary blades in certain ratio, which is greater than fifteen |
| 05/18/2006 | DE102004055199A1 Gleitschichten aus Verbundmaterial und Verfahren zu deren Herstellung Sliding layers of composite material and process for their preparation |
| 05/18/2006 | DE102004054930A1 Rotor einer Turbomaschine, insbesondere Gasturbinenrotor Rotor of a turbomachine, in particular a gas turbine rotor |
| 05/18/2006 | DE102004054752A1 Schaufel einer Strömungsarbeitsmaschine mit erweiterter Randprofiltiefe Blade of a turbomachine with extended edge tread depth |
| 05/18/2006 | DE102004053424A1 Turbine shaft for turbocharger has core made of material with higher thermal conductivity compared to that of shaft material with turbine and compressor wheel mounted on it and they are supported in bearing housing of turbocharger |
| 05/18/2006 | CA2563824A1 Ceramic matrix composite airfoil trailing edge arrangement |
| 05/17/2006 | EP1657536A1 Device comprising at least one luminescent thermal barrier coating on a substrate |
| 05/17/2006 | EP1657404A1 Turbomachine rotor, in particular gas turbine rotor |
| 05/17/2006 | EP1657403A1 Airfoil with large fillet and micro-circuit cooling |
| 05/17/2006 | EP1657402A1 Blade |
| 05/17/2006 | EP1657401A2 Turbo machine blade with an extended profile chord length in its tip and root regions |
| 05/17/2006 | EP1656493A1 Labyrinth seal in a stationary gas turbine |
| 05/17/2006 | EP1534878B1 Highly oxidation resistant component |
| 05/17/2006 | EP1513781B1 Heat-insulating layer made of complex perovskite |
| 05/17/2006 | CN1774560A Center-located cutter teeth on shrouded turbine blades |
| 05/17/2006 | CN1773080A Heat transferring cooling features for an airfoil |
| 05/17/2006 | CN1773079A High efficiency rotor for the first phase of a gas turbine |
| 05/17/2006 | CN1256464C Chemical cleaning solution for gas turbine blades |
| 05/16/2006 | US7047167 Blade shape designing method, program thereof and information medium having the program recorded thereon |
| 05/16/2006 | US7044710 Gas turbine arrangement |
| 05/11/2006 | WO2006048401A1 Optimised turbine stage for a turbine engine and layout method |
| 05/11/2006 | WO2006048379A1 Vacuum pump impeller |
| 05/11/2006 | WO2006047854A1 Aspherical dimples for heat transfer surfaces and method |
| 05/11/2006 | US20060099074 Component having a film cooling arrangement |
| 05/11/2006 | US20060099073 Aspherical dimples for heat transfer surfaces and method |
| 05/11/2006 | US20060096091 Method for manufacturing aircraft engine cases with bosses |
| 05/11/2006 | DE102004052142A1 Laser welding process especially for compressor blades for a gas turbine cleans weld region with defocused beam before welding with the same beam that is focused |
| 05/11/2006 | CA2583126A1 Aspherical dimples for heat transfer surfaces and method |
| 05/10/2006 | EP1655568A1 Method of Determining the Wall Thickness of a Hollow Element |
| 05/10/2006 | EP1655454A1 Coated wall with cooling arrangement |
| 05/10/2006 | EP1655453A1 A component having a film cooling arrangement |
| 05/10/2006 | EP1655452A2 Cooling features for an airfoil |
| 05/10/2006 | EP1655451A1 A cooling arrangement |
| 05/10/2006 | EP1655100A1 Method for machining a workpiece and workpiece |
| 05/10/2006 | EP1654089A1 Rotating blade for a gas turbine rotor and a method for producing integrated blade rotors for a gas turbine mounted by capacitor discharge welding |
| 05/10/2006 | CN1769653A Element of turbomachinery with cool unit |
| 05/10/2006 | CN1769652A Unit for sealing transition region between two parts cool passage of turbomachinery |
| 05/10/2006 | CN1769647A High efficiency stator for the second phase of a gas turbine |
| 05/10/2006 | CN1769646A Rotor blade for a first phase of a gas turbine |
| 05/10/2006 | CN1769043A Article including environmental barrier wall coating system and method for manufacturing the same |
| 05/09/2006 | US7041383 metallic substrate with ceramic coating consisting of a formula of NdxZr1-xOy with yttria and hafnia added and dissolved in; protective coatings for turbine components, (e.g. blades and vanes) to prevent the components from overheating during high temperature operation. |
| 05/09/2006 | US7040940 Rotatable lifting surface device having selected pitch distribution and camber profile |
| 05/09/2006 | US7040867 Compressor wheel joint |
| 05/09/2006 | US7040866 System for retaining an annular plate against a radial face of a disk |
| 05/09/2006 | US7040097 Gas turbine and associated cooling method |
| 05/09/2006 | CA2367711C Blade structure in a gas turbine |
| 05/04/2006 | WO2005120824A3 Durable thermal barrier coating having low thermal conductivity |
| 05/04/2006 | US20060093480 Airfoil with three-pass serpentine cooling channel and microcircuit |
| 05/04/2006 | DE19754369B4 Zentrifugalturbinenrad, insbesondere für eine Heizungs-, Belüftungs- und/oder Klimaanlage eines Kraftfahrzeugs Zentrifugalturbinenrad, in particular for a heating, ventilation and / or air conditioning system of a motor vehicle |
| 05/03/2006 | EP1653047A2 Gas turbine rotor blade |
| 05/03/2006 | EP1653046A1 Cooled turbine blade and method of adjusting the coolant flow |
| 05/03/2006 | EP1652968A1 Coating systems containing beta phase and gamma-prime phase nickel aluminide |
| 05/03/2006 | EP1652967A1 Coating system, comprising a coating containing gamma-prime nickel aluminide |
| 05/03/2006 | EP1652964A1 Superalloy article having a gammaprime nickel aluminide coating |
| 05/03/2006 | EP1652959A1 Method for depositing gamma-prime nickel aluminide coatings |
| 05/03/2006 | EP1652955A1 Method and apparatus for repairing thermal barrier coatings |
| 05/03/2006 | EP1652954A1 Method and apparatus for microplasma spray coating a portion of a compressor blade in a gas turbine engine |
| 05/03/2006 | EP1652953A1 Methods for repairing a workpiece |
| 05/03/2006 | EP1652952A1 Methods for repairing workpieces using microplasma spray coating |
| 05/03/2006 | EP1652951A1 Method and apparatus for microplasma spray coating a portion of a turbine vane in a gas turbine engine |
| 05/03/2006 | EP1652612A1 Method of repairing a brazed joint between two components of an aerospace article; Article repaired using such method |
| 05/03/2006 | EP1652603A2 Investment casting cores and methods |
| 05/03/2006 | EP1651841A1 Open-cooled component for a gas turbine, combustion chamber, and gas turbine |
| 05/03/2006 | EP1651380A1 Parametric production of cooling bores |
| 05/03/2006 | EP1481151B1 Improved vane design for use in variable geometry-turbocharger |
| 05/03/2006 | EP1478482B1 Method of removing casting defects |
| 05/03/2006 | CN2777200Y Steam turbine power system |
| 05/03/2006 | CN1766290A Turbine airfoil with stepped coolant outlet slots |
| 05/03/2006 | CN1766150A Method of repairing a ni-base alloy part |
| 05/02/2006 | US7037079 Axial-flow thermal turbomachine |
| 05/02/2006 | US7037078 Turbomachine turbines with blade inserts having resonant frequencies that are adjusted to be different, and a method of adjusting the resonant frequency of a turbine blade insert |