| 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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| 08/01/2007 | EP1813774A2 Turbine element cooling |
| 08/01/2007 | EP1813773A2 Aerofoil assembly with improved vibration response and a method of manufacturing the aerofoil assembly |
| 08/01/2007 | EP1813772A2 Nozzle blade airfoil profile for a turbine |
| 08/01/2007 | EP1813771A2 Bladed rotor assembly |
| 08/01/2007 | EP1813770A1 Fastening system for an engine shaft with a clamping nut |
| 08/01/2007 | EP1813769A1 Assembly with reduced radial dimensions between a turbine shaft and a compressor shaft journal in a turbomachine |
| 08/01/2007 | EP1813686A1 Preparation of an article surface having a surface compressive texture |
| 08/01/2007 | EP1813374A1 Gas welding shielding dam with a flange and a fastener for automated welding of impellers and blisks |
| 08/01/2007 | EP1812769A1 Aspherical dimples for heat transfer surfaces and method |
| 08/01/2007 | EP1812688A2 Woven turbomachine impeller |
| 08/01/2007 | EP1631734B1 Rotor for a gas turbine |
| 08/01/2007 | EP1446565B1 Turbine engine with air cooled turbine |
| 08/01/2007 | CN2929194Y Small turbocharger with mixed flow turbine and water cooling bearing |
| 08/01/2007 | CN1329633C Steam penetrating flat |
| 08/01/2007 | CN1329632C Method and device for cooling gas turbine nozzle |
| 08/01/2007 | CN1329631C Second-stage turbine nozzle airfoil |
| 08/01/2007 | CN1329630C Francis turbine |
| 08/01/2007 | CN1329629C Device for fixing a rotor on a shaft |
| 08/01/2007 | CN1329551C Novel heat barrier coating material |
| 08/01/2007 | CN101010486A Non-positive-displacement machine and rotor for a non-positive-displacement machine |
| 08/01/2007 | CN101008327A Film cooling method and method of manufacturing a hole |
| 08/01/2007 | CN101008324A Surface composite coating of turbomachine rotor blade and preparation method thereof |
| 08/01/2007 | CN101008323A Gas turbine bucket with cooled platform edge and method of cooling platform leading edge |
| 08/01/2007 | CN101008322A Balancing mass and rotor disc, rotor and aircraft engine comprising such a mass |
| 08/01/2007 | CN101008105A Repair method of crystalline structures by epitaxy |
| 08/01/2007 | CN101008059A Rhenium-free nickel base single crystal high-temperature alloy material |
| 07/31/2007 | US7250225 Gamma prime phase-containing nickel aluminide coating |
| 07/31/2007 | US7250224 For damping vibration in an airfoil of a rotating component of a turbomachine, examples of which include fan and compressor blades formed of titanium-based alloys |
| 07/31/2007 | US7250222 Layer system |
| 07/31/2007 | US7250192 Sprayable noble metal coating for high temperature use directly on aircraft engine alloys |
| 07/31/2007 | US7249934 Pattern cooled turbine airfoil |
| 07/31/2007 | US7249933 Funnel fillet turbine stage |
| 07/31/2007 | US7249412 Method for repairing a damaged blade of a Blisk |
| 07/27/2007 | CA2576709A1 Manufacturing process for a turbine engine part that includes cooling air exhaust orifices |
| 07/26/2007 | WO2007084100A1 Bearing-like structure to control deflections of a rotating component |
| 07/26/2007 | WO2007083361A1 Surface treatment coating film with resistance to erosion by solid particle and rotary machine |
| 07/26/2007 | WO2007082823A1 Component for arrangement in the duct of a turbine engine and spray method for production of a coating |
| 07/26/2007 | WO2007082793A1 Component having a coating and process for producing a coating |
| 07/26/2007 | WO2007082787A1 Welding process with subsequent diffusion treatment |
| 07/26/2007 | US20070172357 Generator rotor crack propagation prediction system and operation conditions determination support system, method, and program, and operation control system |
| 07/26/2007 | US20070172355 Microcircuit cooling with an aspect ratio of unity |
| 07/26/2007 | US20070172354 Blade or vane for a turbomachine |
| 07/26/2007 | US20070172351 Repaired turbine nozzle |
| 07/26/2007 | DE202004021250U1 Turbinenrad zum Antrieb schnell rotierender Werkzeuge Turbine to drive fast rotating tools |
| 07/26/2007 | DE102006002791A1 Axial flow cylinder for pneumatic tool, has internal cylinder chamber in cylinder housing, where air flows between air passage openings of moveable wheels and fixed wheels is discharged through exhaust connection |
| 07/25/2007 | EP1811150A2 Motor-Driven supercharge |
| 07/25/2007 | EP1811129A2 Aerofoils for gas turbine engines |
| 07/25/2007 | EP1811061A2 Yttria-stabilized zirconia coating with a molten silicate resistant outer layer |
| 07/25/2007 | EP1811060A2 CMAS resistant thermal barrier coating |
| 07/25/2007 | EP1811055A1 Method for manufacturing a component with holes |
| 07/25/2007 | EP1421257B1 Double flow compressor |
| 07/25/2007 | CN2926517Y End vane of large rotating-speed steam turbine |
| 07/25/2007 | CN2926516Y End vane of high-rotating speed and rotating-speed variable industrial steam turbine |
| 07/25/2007 | CN2926515Y End vane of medium-miniature power steam turbine set |
| 07/25/2007 | CN1328480C Fastening system |
| 07/25/2007 | CN1328479C Method of confirming damaged condition of urbo engine electric-insulating surface |
| 07/25/2007 | CN1328478C Method and device for reducing the temperature of turbine leaf opex |
| 07/25/2007 | CN1328477C Nonsteady matching method of impeller edge line |
| 07/25/2007 | CN1328413C Method for removing at least one area of a layer of a component consisting of metal or a metal compound |
| 07/25/2007 | CN1327997C Method for renewing cooling path in turbine wing surface |
| 07/25/2007 | CN101004147A Microcircuit cooling for a turbine blade tip |
| 07/25/2007 | CN101004142A Cmas resistant thermal barrier coating |
| 07/25/2007 | CN101004141A Microcircuit cooling for a turbine blade tip |
| 07/25/2007 | CN101004140A Microcircuit cooling for a turbine blade tip |
| 07/25/2007 | CN101003874A High temperature alloy of nickel based monocrystalline capable of bearing high temperature |
| 07/25/2007 | CN101003849A Method for heat treating a serviced turbine part |
| 07/24/2007 | US7247958 Dynamo-electric machine |
| 07/24/2007 | US7247393 Protective coating on surfaces of components used in hostile thermal environments, including the turbine, combustor and augmentor sections of a gas turbine engine |
| 07/24/2007 | US7247348 providing an airfoil substrate having an airfoil substrate surface, and depositing a diamond-like coating (DLC) directly on the airfoil substrate surface |
| 07/24/2007 | US7247212 Orthogonal weaving for complex shape preforms |
| 07/24/2007 | US7247003 Stacked lamellate assembly |
| 07/24/2007 | US7246994 Spacing arrangement |
| 07/24/2007 | US7246993 Coolable segment for a turbomachine and combustion turbine |
| 07/24/2007 | US7246992 High efficiency fan cooling holes for turbine airfoil |
| 07/19/2007 | WO2007080744A1 Method and apparatus for balancing an electrically assisted turbocharger rotor |
| 07/19/2007 | WO2007080189A1 Turbine blade with recessed tip |
| 07/19/2007 | WO2007080060A1 Method of making a hole |
| 07/19/2007 | WO2007080058A1 Ceramic solid component, ceramic layer having a high porosity, use of said layer, and a component comprising said layer |
| 07/19/2007 | WO2007080041A1 Layer system comprising two pyrochlore phases |
| 07/19/2007 | US20070166161 Turbine airfoil with improved cooling |
| 07/19/2007 | US20070166152 Turbomachine |
| 07/19/2007 | US20070163682 Ni-based superalloy having high oxidation resistance and gas turbine part |
| 07/19/2007 | DE19944923B4 Turbinenschaufel für den Rotor einer Gasturbine Turbine blade for the rotor of a gas turbine |
| 07/19/2007 | DE19807563B4 Kühlkonstruktion zum Kühlen der Plattform einer Turbinenschaufel Cooling structure for cooling the platform of a turbine blade |
| 07/19/2007 | DE102005059438B3 Turbo-jet engine e.g. bypass engine, for e.g. commercial aircraft, has rotors arrowed in opposite directions in such a manner that rotor distance is increased with increasing radius, and rotor blades bent against each other in convex manner |
| 07/19/2007 | CA2675151A1 Turbine blade with recessed tip |
| 07/18/2007 | EP1808576A1 Turbine shaft for a flow machine |
| 07/18/2007 | EP1808575A2 Tilted turbine vane with impingement cooling |
| 07/18/2007 | EP1808574A2 Turbine engine with improved cooling |
| 07/18/2007 | EP1808573A1 Balancing mass and rotor disc, rotor and aircraft engine comprising such a mass |
| 07/18/2007 | EP1808572A1 Welding method with subsequent diffusion treatment |
| 07/18/2007 | EP1808508A1 Component located in the flow channel of a turbomachine and spraying process for generating a coating. |
| 07/18/2007 | EP1808507A1 Coated component and method of manufacturing said coating |
| 07/18/2007 | EP1808506A1 Method for treating a workpiece with a chemical |
| 07/18/2007 | EP1808266A2 Turbine platform repair using laser clad |
| 07/18/2007 | EP1808263A2 Chordwidth restoration of a trailing edge of a turbine airfoil by laser clad |
| 07/18/2007 | EP1808236A1 Process of masking cooling holes, espacially of turbine blades |
| 07/18/2007 | EP1807685A1 Arrangement provided with at least one luminescent heat-insulating layer on a carrier body |
| 07/18/2007 | EP1807674A1 Method for determining the wall thickness of a hollow component |
| 07/18/2007 | EP1807554A2 Electrolyte for deposition of an alloy and method for electrolytic deposition |