| 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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| 08/04/2004 | EP1442817A2 Apparatus and method for rejuvenating cooling passages within a turbine airfoil |
| 08/04/2004 | EP1441874A1 Method for removing coating material from a cooling hole of a gas turbine engine component |
| 08/04/2004 | EP1343950B1 System to feed cooling air into a gas turbine rotor |
| 08/04/2004 | EP1175517B1 Stop-off for diffusion coating |
| 08/04/2004 | CN2630501Y Gas-steam turbine impeller |
| 08/04/2004 | CN1517691A Estimating method for fatigue life of turbine blade, turbine blade creep elongation strain measurement device and turbine blade |
| 08/04/2004 | CN1517513A Turbo-blade and gas turbine |
| 08/03/2004 | US6769879 Airfoil shape for a turbine bucket |
| 08/03/2004 | US6769878 Turbine blade airfoil |
| 08/03/2004 | US6769877 Undercut leading edge for compressor blades and related method |
| 08/03/2004 | US6769875 Cooling system for a turbine blade |
| 08/03/2004 | US6769869 High efficiency blade configuration for steam turbine |
| 08/03/2004 | US6769867 Joint structure of coolant passage, tube seal, and gas turbine |
| 08/03/2004 | US6769866 Turbine blade and method for producing a turbine blade |
| 08/03/2004 | CA2190567C Process for making a composite rotor with metallic matrix |
| 07/30/2004 | CA2456403A1 An active cooling panel of thermostructural composite material and method for its manufacture |
| 07/29/2004 | WO2004063571A2 Cooling fan with reinforced blade |
| 07/29/2004 | WO2004046414A3 Method of forming a vibration damping coating on a metallic substrate |
| 07/29/2004 | US20040146741 Thermal barrier coating |
| 07/29/2004 | US20040146657 Using three plasma torches ; concurrent spraying, heating |
| 07/29/2004 | US20040146404 Turbine blade with sealing element |
| 07/29/2004 | US20040146402 Turbine moving blade and gas turbine |
| 07/29/2004 | US20040146401 Turbine blade |
| 07/29/2004 | US20040146399 Coolable segment for a turbomachinery and combustion turbine |
| 07/29/2004 | US20040145251 Damper for Stator Assembly |
| 07/29/2004 | DE10358431A1 Temperaturabtaststruktur, Verfahren zu ihrer Herstellung, Gasturbinen-Triebwerk und Temperatursteuerverfahren Temperaturabtaststruktur, to processes for their preparation, to gas turbine engine and temperature control method |
| 07/29/2004 | DE10301755A1 Fanschaufel für ein Gasturbienentriebwerk Fan blade for a Gasturbienentriebwerk |
| 07/28/2004 | EP1441108A2 Damper for gas turbine stator assembly |
| 07/28/2004 | EP1441107A2 Turbine blade |
| 07/28/2004 | EP0911489B1 Gas turbine cooling stationary blade |
| 07/28/2004 | CN1516756A Method for producing mono-crystalline structures |
| 07/27/2004 | US6767659 Ceramic matrix composite component of a gas turbine engine such as a combustion liner adapted for backside radiative cooling |
| 07/27/2004 | US6767649 Crack-free welded joint to join two rotor sections; layers joined by powder metallurgy |
| 07/27/2004 | US6767183 Methods and apparatus for sealing gas turbine engine variable vane assemblies |
| 07/22/2004 | US20040142204 alloy containing more than 3 weight percent rhenium and at least one of tungsten, tantalum, hafnium, molybdenum, niobium, or zirconium; diffusion barrier coating; aluminum-containing overlay coating |
| 07/22/2004 | US20040142112 superalloy parts exposed to high temperatures and frequent thermal cycles |
| 07/22/2004 | US20040141847 Stator blade for an axial flow compressor |
| 07/22/2004 | US20040141838 Turbine stage one shroud configuration and method for service enhancement |
| 07/22/2004 | US20040140672 Gas turbomachinery generator |
| 07/22/2004 | US20040140079 Device and method for casting a workpiece, and workpiece |
| 07/21/2004 | EP1439282A1 Device for mounting an annular flask at a radial side of a rotor |
| 07/21/2004 | EP1439281A2 Gas turbine engine blade |
| 07/21/2004 | EP1133619B1 Turbine blade to disk retention device |
| 07/21/2004 | CN1514112A Sealing of steam turbine blade shackle part leak using braided rope sealing unit |
| 07/21/2004 | CN1514111A Turbine machine matched with gas turbine |
| 07/20/2004 | US6764771 Product, especially a gas turbine component, with a ceramic heat insulating layer |
| 07/20/2004 | US6764384 System for the precision machining of rotationally symmetrical components |
| 07/20/2004 | US6764282 Blade for turbine engine |
| 07/20/2004 | US6764281 Rotor system for an expansion turbine for low-temperature applications |
| 07/20/2004 | US6764276 Guide vane assembly |
| 07/20/2004 | US6763560 Spreader for separating turbine buckets on wheel |
| 07/20/2004 | CA2300038C Gas turbine stationary blade |
| 07/15/2004 | US20040136844 Split seal plate with integral brush seal |
| 07/15/2004 | US20040136831 Weight reduced steam turbine blade |
| 07/15/2004 | US20040136828 Wheel space pressure relief device |
| 07/15/2004 | US20040136824 Trailing edge cooling |
| 07/15/2004 | US20040134897 Process of removing a ceramic coating deposit in a surface hole of a component |
| 07/14/2004 | EP1437483A1 Trailing edge cooling of a turbine airfoil |
| 07/14/2004 | EP1437425A1 Method for removing aluminide coating from metal substrate and turbine engine part so treated |
| 07/14/2004 | EP1437194A2 Process of removing a ceramic coating deposit in a surface hole of a component |
| 07/14/2004 | CN1512046A 燃气轮机 Gas turbine |
| 07/14/2004 | CN1512038A Mounting method and device for gas turbine jet nozzle |
| 07/14/2004 | CN1512037A Method and device for assembling turbine engine |
| 07/14/2004 | CN1512036A Worm wheel wing with venturi outlet |
| 07/14/2004 | CN1512035A Nonsteady matching method of impeller edge line |
| 07/13/2004 | US6761956 Ventilated thermal barrier coating |
| 07/13/2004 | US6761807 Molded tooling for use in airfoil stripping processes |
| 07/13/2004 | US6761538 Continual radial loading device for steam turbine reaction type buckets and related method |
| 07/13/2004 | US6761537 Methods and apparatus for assembling turbine engines |
| 07/13/2004 | US6761536 Turbine blade platform trailing edge undercut |
| 07/13/2004 | US6761535 Internal core profile for a turbine bucket |
| 07/13/2004 | US6761534 Cooling circuit for a gas turbine bucket and tip shroud |
| 07/13/2004 | US6761529 Cooling structure of stationary blade, and gas turbine |
| 07/13/2004 | US6761040 Cross flow fan and air conditioner fitted with the same |
| 07/13/2004 | US6761034 Structural cover for gas turbine engine bolted flanges |
| 07/13/2004 | CA2092273C Two-lug side-entry turbine blade attachment |
| 07/08/2004 | WO2004057157A1 Turbine blade |
| 07/08/2004 | WO2004056525A1 Spun metal form used to manufacture dual alloy turbine wheel |
| 07/08/2004 | WO2004042198A3 Self-regulating turbine |
| 07/08/2004 | US20040131877 Article having turbulation and method of providing turbulation on an article |
| 07/08/2004 | US20040131471 Blade arrangement for gas turbine engine |
| 07/08/2004 | US20040131470 Cooling fan with reinforced blade |
| 07/08/2004 | DE10359917A1 Verfahren und Vorrichtung zum Abstimmen der Eigenfrequenz von Turbinenlaufschaufeln Method and apparatus for tuning the natural frequency of the turbine blades |
| 07/08/2004 | DE10261262A1 Laser welded rotor discs for turbines and compressors consist of base rotating body and individually manufactured guide blades which are optimized in their strength values |
| 07/08/2004 | DE10257044A1 Gas turbine particularly to power aircraft has fixed guide vanes has curvature of guide vanes and simultaneously entry angle and/or emergence angle of vanes adjustable independent of each other |
| 07/08/2004 | DE10052176B4 Dampfturbinenrotor und Verfahren zur Herstellung desselben Steam turbine rotor and method of manufacturing the same |
| 07/07/2004 | EP1435492A2 High temperature turbine nozzle and process for manufacturing |
| 07/07/2004 | EP1435491A2 Improved high temperature splash plate |
| 07/07/2004 | EP1435490A2 High temperature centerbody and process for manufacturing |
| 07/07/2004 | EP1435489A2 High temperature combustor wall and process for manufacturing |
| 07/07/2004 | EP1435432A1 Turbine blade |
| 07/07/2004 | EP1435431A1 SEALING STRUCTURE OF SPINDLE BOLT, AND GAS TURBINE |
| 07/07/2004 | CN1509841A Component for forming fixed channels through gas turbine disc dovetail grooves |
| 07/07/2004 | CN1509840A Method and device for removing materials from bottom of gas turbine disc dovetail grooves |
| 07/06/2004 | US6760264 Apparatus and structure for rapid enablement |
| 07/06/2004 | US6758985 Method of removing a ceramic coating |
| 07/06/2004 | US6758651 Gas turbine |
| 07/06/2004 | CA2012240C Fiber reinforced ceramic matrix composite member and method for making |
| 07/01/2004 | WO2004055332A1 Manufacturing method for obtaining high-temperature components for gas turbines and components thus obtained |
| 07/01/2004 | WO2004054744A1 Manufacturing method for obtaining high-performance components for gas turbines and components thus obtained |