| 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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| 04/07/2005 | US20050074325 Cooling jets |
| 04/07/2005 | US20050071999 Method of producing a turbine rotor having a control wheel |
| 04/07/2005 | DE10342207A1 Laufschaufelbindung einer Turbomaschine Blade binding of a turbomachine |
| 04/07/2005 | DE10342097A1 Axialkompressor Axial Compressor |
| 04/07/2005 | DE10341415A1 Hochgeschwindigkeitslaufrad High-speed impeller |
| 04/06/2005 | EP1520957A1 Apparatus and method for damping vibrations between a compressor stator vane and a casing of a gas turbine engine |
| 04/06/2005 | EP1520062A1 Highly oxidation resistant component |
| 04/06/2005 | EP0934455B1 Airfoil for a turbomachine |
| 04/05/2005 | US6875953 Method using laser shock processing to provide improved residual stress profile characteristics |
| 04/05/2005 | US6875529 Stabilized zirconia ceramic coating; reduced heat conductivity |
| 04/05/2005 | US6875464 Using ceramic paste containing zirconia particles in binder; heating |
| 04/05/2005 | US6875292 Oxidation, corrosion resistant protective coatings; surface treatment; controlling temperature |
| 04/05/2005 | US6874992 Gas turbine engine aerofoil |
| 04/05/2005 | US6874988 Gas turbine blade |
| 04/05/2005 | US6874987 Cooled turbine blade |
| 04/05/2005 | US6874324 Gas turbine and gas turbine power generator |
| 03/31/2005 | WO2005028876A1 Compressor cleaning system |
| 03/31/2005 | WO2005028812A1 Labyrinth seal in a stationary gas turbine |
| 03/31/2005 | US20050069647 Applying Pt(acetylacetonate)2 onto a nonmetal, matal or alloy substrate, wrapping substrate with a metal foil; heating substrate and foil, wherein Pt(acetylacetonate)2 decomposes to deposit pure platinum on the substrate |
| 03/31/2005 | US20050069414 Flow guide component with enhanced cooling |
| 03/31/2005 | US20050069411 Turbine comprising at least four stages and use of a turbine blade with a reduced mass |
| 03/31/2005 | US20050067065 From an article with an oriented microstructure by locating and locally melting the defect, and then epitaxially solidifying the melt; cobalt or nickel super alloy for gas turbines |
| 03/31/2005 | US20050067061 containing nickel, palladium, and restricted amounts of boron and silicon; for repairing nickel-based superalloy articles, or for joining different sections of superalloy components |
| 03/31/2005 | DE10340827A1 Reparaturverfahren für eine Schaufel einer Strömungsarbeitsmaschine Repair method for a blade of a turbomachine |
| 03/31/2005 | DE10340823A1 Blade for compactor or turbine disc is connected to blade foot which in relation to rotary axis of disc is radially extended with joining surface at radially inner side to connect with disc |
| 03/31/2005 | DE10340520A1 Verfahren zur Herstellung von Gasturbinenrotoren mit integraler Beschaufelung A process for producing gas turbine rotors with integral blading |
| 03/30/2005 | EP1519008A1 Internally cooled fluid directing component and a cooling method for this component |
| 03/30/2005 | EP1519007A1 Gas turbine |
| 03/30/2005 | EP1518942A1 Platinum coating process |
| 03/30/2005 | EP1518636A2 Nickel-based braze alloy compositions, and related processes and articles |
| 03/30/2005 | EP1518619A1 Turbine blade for an aircraft engine and casting mould for its manufacture |
| 03/30/2005 | EP1517762A2 Diffusion bond mixture for healing single crystal alloys |
| 03/30/2005 | CN1602236A Method for removing coating material from a cooling hole of a gas turbine engine component |
| 03/30/2005 | CN1601056A Turbine blade of turine and its puller |
| 03/29/2005 | US6871398 Method of manufacturing an article by diffusion bonding |
| 03/24/2005 | WO2005026501A1 Turbine rotor blade |
| 03/24/2005 | US20050065712 Engine balancing system and method |
| 03/24/2005 | US20050064229 Rhenium-containing protective layer for protecting a component against corrosion and oxidation at high temperatures |
| 03/24/2005 | US20050064228 Protective coating for turbine engine component |
| 03/24/2005 | US20050064225 Thermal barrier composition, a superalloy machine part provided with a coating having such a composition, a ceramic coating, and a method of fabricating the coating |
| 03/24/2005 | US20050064213 a ceramic layer disposed on the substrate surface in a manner that provides the ceramic layer with a microstructure characterized by multiple vertical and horizontal gaps, and sintering resistance material with specific morphology disposed in gaps |
| 03/24/2005 | US20050064104 Forming thermal barrier coating by evaporating one or more ingots that in combination provide sources of yttria-stabilized zirconia, a carbon-containing material chosen from the group consisting of graphite and carbides, and an oxide so that vapors thereof deposit to form a thermal-insulating material |
| 03/24/2005 | US20050063826 Inter-vane platform with flexible securing pins and variable shear stresses for a support disk for the vanes of a turbine engine |
| 03/24/2005 | US20050063824 Hollow rotor blade for the turbine of a gas turbine engine |
| 03/24/2005 | US20050063819 Axial compressor |
| 03/24/2005 | US20050061855 Spun metal form used to manufacture dual alloy turbine wheel |
| 03/24/2005 | DE10340773A1 Rotor einer Dampf- oder Gasturbine Rotor of a steam or gas turbine |
| 03/24/2005 | DE102004041392A1 Dickenprofil eines Verdichterlaufrads mit lokalisierter Verdickung Thickness profile of a compressor rotor with localized thickening |
| 03/23/2005 | EP1517008A2 Cooling of a coated wall by a network of cooling channels |
| 03/23/2005 | EP1517004A1 Rotor wheel for a turbomachine and assembly method therefor |
| 03/23/2005 | EP1517003A2 Cooled turbomachine blade |
| 03/23/2005 | EP1516943A2 Protective coating for turbine engine component |
| 03/23/2005 | EP1516942A1 Method for coating a substrate |
| 03/23/2005 | EP1516690A1 Method of manufacturing or repairing a bladed rotor disc |
| 03/23/2005 | EP1516106A1 Variable geometry turbocharger having internal bypass exhaust gas flow |
| 03/23/2005 | EP1466079B1 Turbine comprising at least four stages and use of a turbine blade with a reduced mass |
| 03/23/2005 | EP1017510B1 Method and apparatus for gas phase coating complex internal surfaces of hollow articles |
| 03/23/2005 | CN1598248A Methods and apparatus for reducing vibrations induced to compressor airfoils |
| 03/22/2005 | US6869703 Thermal barrier coatings with improved impact and erosion resistance |
| 03/22/2005 | US6869270 Turbine blade cover cooling apparatus and method of fabrication |
| 03/22/2005 | US6869268 Combustion turbine with airfoil having enhanced leading edge diffusion holes and related methods |
| 03/22/2005 | US6869049 Method and apparatus for modulating flow separation |
| 03/19/2005 | CA2440804A1 Internal combustion engine catalytic converter |
| 03/17/2005 | WO2005024185A1 Method for the production of gas turbine rotors with integrated blading |
| 03/17/2005 | US20050058547 Bond coat process for thermal barrier coating |
| 03/17/2005 | US20050058546 Vane apparatus for a gas turbine engine |
| 03/17/2005 | US20050058545 Turbine blade platform cooling system |
| 03/17/2005 | US20050058541 Casing, a compressor, a turbine, and a combustion turbine engine including such a casing |
| 03/17/2005 | US20050058534 Network cooled coated wall |
| 03/17/2005 | US20050056965 Method for making a pin reinforced, crack resistant fiber reinforced composite airfoil |
| 03/17/2005 | US20050056013 Turbocharger compressor wheel having a counterbore treated for enhanced endurance to stress-induced fatigue and configurable to provide a compact axial length |
| 03/17/2005 | US20050056007 Internal combustion engine catalytic converter |
| 03/17/2005 | DE19615549B4 Vorrichtung zum thermischen Schutz eines Rotors eines Hochdruckverdichters Device for thermal protection of a rotor of a high-pressure compressor |
| 03/17/2005 | DE10339046A1 Vorrichtung zum Elysiersenken Apparatus for Elysiersenken |
| 03/17/2005 | DE10337868A1 Rotor für eine Gasturbine sowie Gasturbine A rotor for a gas turbine and gas turbine |
| 03/17/2005 | CA2480983A1 Network cooled coated wall |
| 03/16/2005 | EP1515040A1 Wind turbine with outer noise shell |
| 03/16/2005 | EP1515001A2 Blade to blade connection in a turbomachine |
| 03/16/2005 | EP1515000A1 Blading of a turbomachine with contoured shrouds |
| 03/16/2005 | EP1514999A2 Turbine blade platform cooling system |
| 03/16/2005 | EP1514017A2 Miniature gas turbine engine with unitary rotor shaft for power generation |
| 03/16/2005 | EP1513781A1 Heat-insulating layer made of complex perovskite |
| 03/16/2005 | CN1594841A Blade to blade connection in a turbomachine |
| 03/16/2005 | CN1594840A Wind urbine with outer noise shell |
| 03/15/2005 | US6866479 Exhaust diffuser for axial-flow turbine |
| 03/15/2005 | US6866478 Miniature gas turbine engine with unitary rotor shaft for power generation |
| 03/15/2005 | US6866477 Airfoil shape for a turbine nozzle |
| 03/15/2005 | US6866234 Method and device for altering the separation characteristics of air-flow over an aerodynamic surface via intermittent suction |
| 03/15/2005 | CA2327149C Blade with optimized vibration behaviour |
| 03/10/2005 | WO2005022065A2 Oxidation resistant coatings for ultra high temperature transition metals and transition metal alloys |
| 03/10/2005 | WO2005021205A1 Automated adaptive machining of obstructed passages |
| 03/10/2005 | US20050053799 Thermal barrier coating utilizing a dispersion strengthened metallic bond coat |
| 03/10/2005 | US20050053467 Aluminide or chromide coating of turbine engine rotor component |
| 03/10/2005 | US20050053466 Reinforced fan blade and method of making |
| 03/10/2005 | US20050053464 Methods and apparatus for cooling gas turbine engine rotor assemblies |
| 03/10/2005 | US20050053461 Impeller and cutting elements for centrifugal chopper pumps |
| 03/10/2005 | US20050053460 Gas turbine engine air baffle for a rotating cavity |
| 03/10/2005 | US20050053459 Microcircuit cooling for a turbine airfoil |
| 03/10/2005 | US20050053458 Cooling system for a turbine blade |
| 03/10/2005 | US20050050901 Part load blade tip clearance control |