| 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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| 09/27/2007 | WO2007107602A2 Quasicrystalline compound and the use thereof as a heat insulating layer |
| 09/27/2007 | WO2007107388A2 Thermal insulation layer system |
| 09/27/2007 | WO2007107145A1 Method and device for joining by way of inductive hf pressure welding a rotor blade with a rotor support of a gas turbine with automatic supply of the rotor blade |
| 09/27/2007 | WO2007107144A1 Component and method for joining metal elements |
| 09/27/2007 | WO2007013892A3 Composite turbomachine impeller and method of manufacture |
| 09/27/2007 | US20070224048 Advanced turbulator arrangements for microcircuits |
| 09/27/2007 | US20070224047 Tip clearance centrifugal compressor impeller |
| 09/27/2007 | US20070224037 Geothermal turbine |
| 09/27/2007 | US20070224033 Fanned trailing edge teardrop array |
| 09/27/2007 | DE102006012675A1 Verfahren und Vorrichtung zum Verbinden von Bauteilen einer Gasturbine Method and apparatus for joining components of a gas turbine |
| 09/27/2007 | CA2645725A1 Method and device for joining components of a gas turbine |
| 09/27/2007 | CA2645582A1 Component and method for joining metal elements |
| 09/27/2007 | CA2641806A1 Turbine blade cascade end wall |
| 09/27/2007 | CA2576004A1 Oxidation-resistant coating and formation method thereof, thermal barrier coating, heat-resistant member, and gas turbine |
| 09/26/2007 | EP1837485A1 Component with a protective layer |
| 09/26/2007 | EP1837484A2 Quasicrystalline bond coating and its use as a thermal barrier coating |
| 09/26/2007 | EP1837483A1 Welded shaft for turbomachines |
| 09/26/2007 | EP1837104A2 Repair of HPT schrouds with sintered preforms |
| 09/26/2007 | EP1836377A1 Turbine blade for turbo-engines and method for manufacturing same |
| 09/26/2007 | CN200952408Y Special last stage blades for large air-cooled turbine |
| 09/26/2007 | CN101042056A Grooving gaseous film cooling hole |
| 09/26/2007 | CN101042055A Composite blading member and method for making |
| 09/26/2007 | CN101042054A Unshrouded turbine and its blade tip with groove |
| 09/26/2007 | CN100339563C Improvement on rotor platform of steam turbine and method for eliminating totor bending with sealing brush |
| 09/26/2007 | CN100339561C Worm wheel wing with venturi outlet |
| 09/26/2007 | CN100339560C Turbine nozzle for coolling wall |
| 09/26/2007 | CN100339559C Last stage rotor blade of steam turbine |
| 09/26/2007 | CN100339558C Internal core outline for vortex blade |
| 09/26/2007 | CN100339557C Compressor with multi-stage axial structure mode |
| 09/25/2007 | US7273353 Shroud honeycomb cutter |
| 09/25/2007 | US7273351 Component having a film cooling arrangement |
| 09/25/2007 | US7273350 Heat transfer arrangement |
| 09/25/2007 | US7273347 Blade for a gas turbine |
| 09/25/2007 | US7273188 Internal self-rotating fluid jetting nozzle |
| 09/25/2007 | CA2354121C Axial retaining ring for a disk flange |
| 09/21/2007 | CA2569902A1 Improved tip clearance centrifugal compressor impeller |
| 09/20/2007 | WO2007106065A1 Roughened coatings for gas turbine engine components |
| 09/20/2007 | WO2007105702A1 Holding structure of fan blade |
| 09/20/2007 | WO2007105701A1 Holding structure of fan blade |
| 09/20/2007 | WO2007105380A1 Blade for axial-flow fluid machine |
| 09/20/2007 | WO2007050205A3 Serpentine cooling circuit and method for cooling a gas turbine part |
| 09/20/2007 | US20070217916 Gas Turbine Vane |
| 09/20/2007 | US20070217915 Dovetail structure of fan |
| 09/20/2007 | US20070217914 Dovetail structure of fan |
| 09/20/2007 | US20070216166 Method for controlling a wind power plant and corresponding wind power plant |
| 09/20/2007 | DE102007012374A1 Turbinenschaufel mit Schwalbenschwanzstruktur Turbine blade dovetail structure |
| 09/20/2007 | DE102007008769A1 Schwalbenschwanzstruktur einer Ansaugeinrichtung Dovetail structure of a suction |
| 09/20/2007 | CA2637278A1 Holding structure of fan blade |
| 09/19/2007 | EP1835129A2 Aerofoil for a gas turbine engine |
| 09/19/2007 | EP1835128A2 Air-oil heat exchanger |
| 09/19/2007 | EP1835045A1 Process for obtaining a coated part |
| 09/19/2007 | EP1834717A2 Cores for use in precision investment casting |
| 09/19/2007 | EP1834133A1 Improved gas turbines |
| 09/19/2007 | EP1834076A1 Tip turbine engine comprising turbine blade clusters and radial attachment lock arrangement therefor |
| 09/19/2007 | EP1834071A1 Inducer for a fan blade of a tip turbine engine |
| 09/19/2007 | EP1834067A1 Tip turbine engine comprising turbine blade clusters and method of assembly |
| 09/19/2007 | EP1834066A1 Turbine blade for a gas turbine, use of a turbine blade and method for cooling a turbine blade |
| 09/19/2007 | EP1833896A2 Plastic material comprising nanoparticles and coatings prepared therefrom |
| 09/19/2007 | CN200949477Y Large-scale full speed nuclear steam turbine last stage blade |
| 09/19/2007 | CN101040101A Non-positive-displacement machine with a rotor having at least one bored rotor disk |
| 09/19/2007 | CN101037960A High pressure ratio aft fan |
| 09/19/2007 | CN101037950A Double-water internal cooling system of gas turbine of gas-steam combined cycling power station |
| 09/19/2007 | CN101037947A Damper cooled turbine blade |
| 09/19/2007 | CN101037946A Fastening arrangement of a pipe on a circumferential surface |
| 09/19/2007 | CN101036955A Enhanced bearing durability rotating member method and apparatus |
| 09/19/2007 | CN100338350C Returnable pressurzing air compressor for gas turbine |
| 09/19/2007 | CN100338337C Turbine bucket assembly and its assembling method |
| 09/18/2007 | US7270852 Aluminizing slurry compositions free of hexavalent chromium, and related methods and articles |
| 09/18/2007 | US7270764 Applying caustic solution then nitric acid; without damage to base metal from used turbine engine blade having a metal-based substrate and an aluminide coating |
| 09/18/2007 | US7270519 Methods and apparatus for reducing flow across compressor airfoil tips |
| 09/18/2007 | US7270518 Steep angle turbine cover buckets having relief grooves |
| 09/18/2007 | US7270517 Turbine blade with vibration damper |
| 09/18/2007 | US7270515 Turbine airfoil trailing edge cooling system with segmented impingement ribs |
| 09/18/2007 | US7270514 Turbine blade tip squealer and rebuild method |
| 09/18/2007 | CA2349994C Turbojet powerplant with heat exchanger |
| 09/18/2007 | CA2347329C Methods and apparatus for supplying cooling airflow in turbine engines |
| 09/18/2007 | CA2335321C Integrated fan/low pressure compressor rotor for gas turbine engine |
| 09/18/2007 | CA2327850C Swept barrel airfoil |
| 09/13/2007 | WO2007101814A1 Gas turbine |
| 09/13/2007 | WO2007101743A1 Method for producing a turbine or compressor component and turbine or compressor component thus obtained |
| 09/13/2007 | WO2007101423A1 Gas turbine component and method for machining gas turbine components during production or reconditioning of said gas turbine components |
| 09/13/2007 | WO2007081347A3 Ceramic matrix composite vane with chordwise stiffener |
| 09/13/2007 | US20070212228 Moving blade for a turbomachine, the blade having a common cooling air feed cavity |
| 09/13/2007 | DE102006010927A1 Gasturbinenbauteil sowie Verfahren zur Bearbeitung von Gasturbinenbauteilen im Rahmen der Herstellung oder Instandsetzung dieser Gasturbinenbauteile A gas turbine component and method for processing gas-turbine components, in the production or repair of gas turbine components |
| 09/13/2007 | CA2644094A1 Gas turbine component,as well as method for machining of gas turbine components in the context of production and repair of these gas turbine components |
| 09/12/2007 | EP1832717A1 Method for influencing the blade tip flow of an axial turbomachine and annular channel for the main axial flow through a turbomachine |
| 09/12/2007 | EP1832714A1 Method of fabrication of a turbine or compressor component and turbine and compressor component |
| 09/12/2007 | EP1832713A1 Gas turbine |
| 09/12/2007 | EP1832712A1 Turbomachine blade with a cooling air manifold cavity |
| 09/12/2007 | EP1832669A1 Bond coat process for thermal barrier coating. |
| 09/12/2007 | EP1832668A1 Local repair process of thermal barrier coatings in turbine engine components |
| 09/12/2007 | EP1831505A1 Static gas turbine component and method for repairing such a component |
| 09/12/2007 | EP1831504A2 Durable thermal barrier coatings |
| 09/12/2007 | EP1831428A2 Turbine engine components with non-aluminide silicon-containing and chromium-containing protective coatings and methods of forming such non-aluminide protective coatings |
| 09/12/2007 | EP1831427A1 Method of manufacturing a component part of a turbine and a component of a turbine |
| 09/12/2007 | EP1673518B1 Hollow turbine blade stiffening |
| 09/12/2007 | EP1385668A4 Method of repairing a turbin blade tip |
| 09/12/2007 | CN101035988A Compressor blade and production and use of a compressor blade |
| 09/11/2007 | US7267527 Rotor for a turbomachine |
| 09/11/2007 | US7267526 Heat-dissipating device |