| 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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| 02/21/2001 | EP1077361A2 Methods and apparatus for measuring airfoil coordinates |
| 02/21/2001 | EP1077311A1 Cooled gas turbine vane |
| 02/21/2001 | EP1077310A1 Vaned stator |
| 02/21/2001 | EP1077309A1 Turbine blade with improved section |
| 02/21/2001 | EP1077308A1 Turbomachinery blade or vane with a survivable machine datum |
| 02/21/2001 | EP1077126A1 Injection formed hydrid airfoil |
| 02/20/2001 | US6190133 High stiffness airoil and method of manufacture |
| 02/20/2001 | US6190131 Non-integral balanced coverplate and coverplate centering slot for a turbine |
| 02/20/2001 | US6190130 Gas turbine moving blade platform |
| 02/20/2001 | US6190129 Tapered tip-rib turbine blade |
| 02/20/2001 | US6190128 Cooled moving blade for gas turbine |
| 02/20/2001 | US6190127 Tuning thermal mismatch between turbine rotor parts with a thermal medium |
| 02/20/2001 | US6190124 Columnar zirconium oxide abrasive coating for a gas turbine engine seal system |
| 02/20/2001 | US6190122 Intake and exhaust air damper with movable motor fan assembly |
| 02/20/2001 | US6190120 Partially turbulated trailing edge cooling passages for gas turbine nozzles |
| 02/15/2001 | WO2001011197A1 Turbine guide vane for exhaust gas turbocharger |
| 02/15/2001 | WO2001010795A1 Silicon nitride components with protective coating |
| 02/15/2001 | WO2001000964B1 Cooled airfoil |
| 02/15/2001 | DE19937577A1 Reibungsbehaftete Gasturbinenkomponente Viscous gas turbine component |
| 02/15/2001 | DE19936507A1 Turbinenleitschaufel für einen Abgas-Turbolader Turbine vane for an exhaust gas turbocharger |
| 02/14/2001 | EP1076159A2 Stator vane blank and method of forming the vane blank |
| 02/14/2001 | EP1076158A1 Gas turbine component having location-dependent protective coatings thereon |
| 02/14/2001 | EP1076157A2 Friction element for a turbomachine |
| 02/14/2001 | EP1076116A1 Components having a partial platinum coating thereon, and preparation thereof |
| 02/14/2001 | EP1076114A1 Method for removing a dense ceramic thermal barrier coating from a surface |
| 02/14/2001 | EP1076111A2 Apparatus and method for selectively coating internal and external surfaces of an airfoil |
| 02/14/2001 | EP1076107A1 Process of plugging cooling holes of a gas turbine component |
| 02/14/2001 | EP1076106A1 Process for masking cooling holes of a gas turbine component |
| 02/13/2001 | US6187453 Article having a durable ceramic coating |
| 02/13/2001 | US6187450 For closing high pressure turbine blade tip cap holes to maximize filling of holes, minimize porosity; oxidation resistance; reliability |
| 02/13/2001 | US6186741 Airfoil component having internal cooling and method of cooling |
| 02/13/2001 | US6186740 Gas turbine cooling blade |
| 02/13/2001 | US6186217 Multipiece core assembly |
| 02/13/2001 | US6185924 Gas turbine with turbine blade cooling |
| 02/08/2001 | WO2001009553A1 Baffle cooling device |
| 02/08/2001 | WO2001009488A1 Blade clearance control for turbomachinery |
| 02/08/2001 | WO2001009405A1 Drag reduction for gas turbine engine components |
| 02/08/2001 | WO2001009403A1 High-temperature part and method for producing the same |
| 02/08/2001 | DE19937146A1 Magnetic device for damping turbo machine blade oscillations has magnet(s) mounted on first vane end on first blade so end(s) of magnet(s) is opposite second vane end on second blade |
| 02/08/2001 | DE19934050A1 Gasturbine Gas turbine |
| 02/07/2001 | EP1074700A2 Rotor blade |
| 02/07/2001 | EP1074698A2 A lubricating coating for tubes in gas turbines |
| 02/07/2001 | EP1074697A2 Apparatus and method for stabilizing the core gas flow in a gas turbine engine |
| 02/07/2001 | EP1074696A2 Stator vane for a rotary machine |
| 02/07/2001 | EP1074695A2 Method for forming a cooling passage in a turbine vane |
| 02/07/2001 | EP1074694A2 Apparatus and methods for cooling rotary components in a turbine |
| 02/07/2001 | EP1074331A1 Method for repairing superralloy castings using a metallurgically bonded tapered plug |
| 02/07/2001 | EP1073827A1 Turbine blade |
| 02/06/2001 | US6183811 Method of repairing turbine airfoils |
| 02/06/2001 | US6183202 Stress relieved blade support |
| 02/06/2001 | US6183199 Cooling-air bore |
| 02/06/2001 | US6183198 Airfoil isolated leading edge cooling |
| 02/06/2001 | US6183197 Airfoil with reduced heat load |
| 02/06/2001 | US6183194 Cooling circuits for trailing edge cavities in airfoils |
| 02/06/2001 | US6183193 Cast on-board injection nozzle with adjustable flow area |
| 02/06/2001 | US6183192 Durable turbine nozzle |
| 02/06/2001 | US6182439 Using nickel-chromium-molybdenum-vanadium low alloy steel for the high and low pressure sides-integrated mono-block rotor shaft, long blades can be provided, efficiency of machine increased and it can be made compact |
| 02/01/2001 | WO2001007760A1 Hydraulic seal for rotary pumps |
| 02/01/2001 | DE19934927A1 Verfahren zum Kühlen von Leit- und/oder Laufschaufeln in den Turbinenstufen einer Gasturbinenanlage sowie Gasturbinenanlage zur Durchführung des Verfahrens A method for cooling control and / or blades in the turbine stages of a gas turbine plant and gas turbine system for implementing the method |
| 01/31/2001 | EP1072759A1 Tip insulated airfoil |
| 01/31/2001 | EP1072758A2 Method for cooling gas turbine blades |
| 01/31/2001 | EP1072757A1 Dust resistant airfoil cooling |
| 01/31/2001 | EP1072692A2 Method and assembly for assessing quality of a coating process |
| 01/31/2001 | EP1072354A2 Turbine blade and it's production method |
| 01/31/2001 | EP1071831A1 Method for producing fibre reinforced metallic components |
| 01/30/2001 | US6180262 Thermal coating composition |
| 01/30/2001 | US6179567 Turbomachinery blade or vane with a survivable machining datum |
| 01/30/2001 | US6179565 Coolable airfoil structure |
| 01/30/2001 | US6179559 Variable camber vane |
| 01/30/2001 | US6179556 Turbine blade tip with offset squealer |
| 01/30/2001 | US6179555 Sealing of T.O.B.I feed plenum |
| 01/25/2001 | WO2001006134A1 System and method for manipulating and controlling fluid flow over a surface |
| 01/25/2001 | WO2001006102A1 Efficiency enhanced turbine engine |
| 01/25/2001 | WO2001006096A1 Gas turbine blade |
| 01/25/2001 | WO2001005579A2 One-step noble metal-aluminide coatings |
| 01/25/2001 | DE19934856A1 Turbinenschaufel und Verfahren zu deren Herstellung Turbine blade and methods for their preparation |
| 01/25/2001 | DE19934418A1 Verfahren zum Beschichten einer lokal unterschiedlich beanspruchten Komponente A method for coating a locally differently stressed component |
| 01/25/2001 | DE19931035A1 Rotor mit gespaltenem Rotorblatt Rotor with a split blade |
| 01/24/2001 | EP1070829A2 Internally cooled airfoil |
| 01/24/2001 | EP1070769A1 Process for coating a locally diversely stressed component |
| 01/24/2001 | CN1061123C Blade for gas turbine, manufacturing method of same, and gas turbine including blade |
| 01/23/2001 | US6177200 Thermal barrier coating systems and materials |
| 01/23/2001 | US6177038 Method for orienting an airfoil for processing and for forming a mask for the airfoil |
| 01/23/2001 | US6176678 Apparatus and methods for turbine blade cooling |
| 01/23/2001 | US6176677 Device for controlling air flow in a turbine blade |
| 01/23/2001 | US6176676 Cooling system for a main body used in a gas stream |
| 01/17/2001 | EP1069281A2 Pre-stressed/pre-compressed gas turbine nozzle |
| 01/17/2001 | EP1069205A1 Article with tailorable high temperature coating |
| 01/17/2001 | EP1068428A1 Apparatus for cooling a gas turbine airfoil and method of making same |
| 01/17/2001 | CN1280648A Turbine components with skin bonded to substrates |
| 01/16/2001 | US6174448 Method for stripping aluminum from a diffusion coating |
| 01/16/2001 | US6174380 Method of removing hot corrosion products from a diffusion aluminide coating |
| 01/16/2001 | US6174135 Turbine blade trailing edge cooling openings and slots |
| 01/16/2001 | US6174134 Multiple impingement airfoil cooling |
| 01/16/2001 | US6174133 Coolable airfoil |
| 01/16/2001 | US6174132 A steam turbine which permits a heightened steam temperature of 610-660 degree c. by heat resistant ferritic steels and exhibits a high thermal efficiency; rotor shaft, moving blades and fixed blades are made of high strength martensitic steel |
| 01/16/2001 | US6173491 Method for replacing a turbine vane airfoil |
| 01/11/2001 | WO2001002742A2 Rotor with a split rotor blade |
| 01/11/2001 | WO2000061918A3 Airfoil leading edge vortex elimination device |
| 01/11/2001 | DE19931763A1 Two/multistage axial turbine, especially for aircraft engine, has intermediate stage sealing ring with front projection parallel to vane ring, to seal ring channel for working gas |