Patents
Sitemap › F01 - Machines or engines in general; Engine plants in general; Steam engines › F01D - Non-positive-displacement machines or engines, e.g. steam turbines › F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
06/2012
06/28/2012US20120163993 Leading edge airfoil-to-platform fillet cooling tube
06/28/2012US20120163992 Drill to flow mini core
06/28/2012US20120163991 Axial flow fan with hub isolation slots
06/28/2012US20120163988 Gas turbine engine airfoil shaped component
06/28/2012US20120163987 High strength glass composition and fibers
06/28/2012US20120163986 Turbine airfoil components containing ceramic-based materials and processes therefor
06/28/2012US20120163985 Components containing ceramic-based materials and coatings therefor
06/28/2012US20120163983 Diffusion bonded and superplastically formed turbomachine blade
06/28/2012US20120163982 Airfoil, turbomachine and gas turbine engine
06/28/2012US20120163981 Method and coating for protecting and repairing an airfoil surface
06/28/2012US20120163980 Impeller for a pump and core arrangement and method for casting an impeller for a pump
06/28/2012US20120163978 Turbine airfoil components containing ceramic-based materials and processes therefor
06/28/2012US20120163975 Platform with cooling circuit
06/28/2012US20120163966 Radial turbine
06/28/2012US20120163960 Gas turbine engine and variable camber vane system
06/28/2012US20120161446 Global wind farm surveillance systems using fiber optic sensors
06/28/2012US20120159952 Gas turbine component having thermal barrier coating and a gas turbine using the component
06/28/2012DE102011121634A1 Turbinenschaufel Turbine blade
06/28/2012DE102011056905A1 Kühlkanalsysteme für mit Beschichtungen überzogene Hochtemperaturkomponenten und zugehörige Verfahren Cooling duct systems with coatings plated high-temperature components and associated methods
06/28/2012DE102011055612A1 Turbinenkomponenten mit Kühleinrichtungen und Verfahren zur Herstellung derselben Turbine components with cooling devices and processes for producing same
06/28/2012DE102010055775A1 Verfahren zur Instandsetzung von Gasturbinenkomponenten A method for repair of gas turbine components
06/28/2012CA2762785A1 Gas turbine engine airfoil shaped component
06/28/2012CA2762774A1 Gas turbine engine and airfoil
06/27/2012EP2469036A2 Flue gas diverter damper seal land
06/27/2012EP2469032A2 Titanium alloy turbine blade
06/27/2012EP2469031A2 Turbine airfoil components containing ceramic-based materials and processes therefor
06/27/2012EP2469030A2 Gas turbine engine with cooled blade tip and corresponding operating method
06/27/2012EP2469029A1 Impingement cooling of gas turbine blades or vanes
06/27/2012EP2469028A2 Airfoil for a turbomachine comprising a metal foam core
06/27/2012EP2469027A2 A diffusion bonded and superplastically formed turbomachine blade
06/27/2012EP2469026A2 Turbine components containing ceramic-based materials and coatings therefore
06/27/2012EP2469025A2 Method for securing a sheath to a blade
06/27/2012EP2469024A1 Gas turbine rotor and method for cooling thereof
06/27/2012EP2469023A1 Gas turbine engine with cooled rotor disks
06/27/2012EP2468919A1 Cathodic arc vapor deposition coatings for dimensional restoration of surfaces
06/27/2012EP2468596A2 A method of monitoring aircraft brake performance and apparatus for performing such a method
06/27/2012EP2468463A2 Method and device for coating path generation
06/27/2012EP2468434A1 Processes for producing components containing ceramic-based and metallic materials
06/27/2012EP2468433A2 Drill to flow mini core
06/27/2012EP2467581A2 Turbine blade with contoured platform
06/27/2012EP2467230A1 Automated repair method and system
06/27/2012EP1971705B1 Layer system comprising two pyrochlore phases
06/27/2012CN202284483U Radial-flow turbine
06/27/2012CN102518481A Compressed air energy storage power generating system
06/27/2012CN102518479A Aerodynamic generating set
06/27/2012CN102518475A Vapour Turbine
06/27/2012CN101405477B Quasicrystalline compound and the use thereof as a heat insulating layer
06/27/2012CN101148993B Methods and apparatus for fabricating turbine engines
06/27/2012CN101131092B Methods and apparatus for fabricating a rotor for a steam turbine
06/27/2012CA2762765A1 Airfoil, turbomachine and gas turbine engine
06/27/2012CA2762482A1 Components containing ceramic-based materials and coatings therefor
06/27/2012CA2762291A1 Turbine airfoil components containing ceramic-based materials and processes therefor
06/26/2012US8206122 Rotor for a compressor
06/26/2012US8206119 Turbine coverplate systems
06/26/2012US8206118 Airfoil attachment
06/26/2012US8206117 Turbine components and methods of manufacturing turbine components
06/26/2012US8206116 Method for loading and locking tangential rotor blades and blade design
06/26/2012US8206115 Scalloped surface turbine stage with trailing edge ridges
06/26/2012US8206114 Gas turbine engine systems involving turbine blade platforms with cooling holes
06/26/2012US8206113 Method and apparatus for converting marine wave energy by means of a difference in flow resistance form factors into electricity
06/26/2012US8206112 Cooling system for a wind turbine
06/26/2012US8206109 Turbine blade assemblies with thermal insulation
06/26/2012US8206108 Turbine blades and methods of manufacturing
06/26/2012US8206084 Blade wheel
06/26/2012US8206079 Temperature controlling apparatus
06/26/2012US8205458 Duplex turbine nozzle
06/26/2012CA2491666C Improvements to the device to control the play in a gas turbine
06/26/2012CA2484944C Miniature gas turbine engine with unitary rotor shaft for power generation
06/24/2012CA2762694A1 Gas turbine engine flow path member
06/23/2012CA2762486A1 Processes for producing components containing ceramic-based and metallic materials
06/23/2012CA2762382A1 Turbine airfoil components containing ceramic-based materials and processes therefor
06/21/2012WO2012080669A1 Turbine engine blade having improved stacking law
06/21/2012WO2012080053A1 Axial compressor
06/21/2012US20120156055 Apparatus and methods for cooling platform regions of turbine rotor blades
06/21/2012US20120156054 Turbine component with near-surface cooling passage and process therefor
06/21/2012US20120156049 Method and coating for protecting and repairing an airfoil surface
06/21/2012US20120156047 Aircraft engine blading
06/21/2012US20120156046 Turbine rotor for air cycle machine
06/21/2012US20120156045 Methods, systems and apparatus relating to root and platform configurations for turbine rotor blades
06/21/2012US20120156044 Bi-cast turbine rotor disks and methods of forming same
06/21/2012US20120156037 Foil, utilized such as an airfoil or hydrofoil, characterized by a duct moving relative to a mass of fluid. A constriction within the duct increases the speed of the fluid flowing within the duct and thereby produces a pressure drop inducing a mass of fluid external to the duct to accelerate into the duct. The acceleration of the fluid into the duct generates a resultant force, which can be varied and controlled to improve performance and reduce drag
06/21/2012US20120156035 Blade arrangement for a gas turbine and method for operating such a blade arrangement
06/21/2012US20120156014 Air cycle machine bearing cooling inlet plate
06/21/2012US20120154177 Method of monitoring aircraft brake performance and apparatus for performing such a method
06/21/2012DE112009004789T5 Verfahren zur Verbesserung der Korrosions- und Oxidationsbeständigkeit an dem Bereich unter der Plattform einer Gasturbinenschaufel Process for improving the corrosion and oxidation resistance at the region under the platform of a gas turbine blade or vane
06/21/2012DE102011120691A1 Gebaute Schaufelanordnung für eine Gasturbine sowie Verfahren zum Betrieb einer solchen Schaufelanordnung Built blade assembly for a gas turbine and method for operating such a blade assembly
06/21/2012DE102011056567A1 System und Verfahren zum Erkennen von Abplatzen in einer Turbine System and method for detecting flaking in a turbine
06/21/2012DE102011056488A1 Turbinenkomponente mit oberflächennahem Kühlkanal und Verfahren hierfür Turbine components with near-surface cooling channel and method therefor
06/21/2012DE102011056322A1 Verfahren, Systeme und Vorrichtungen in Bezug auf Fuß- und Plattformkonfigurationen für Turbinenlaufschaufeln Methods, systems, and devices relating to foot and platform configurations for turbine blades
06/21/2012CA2821142A1 Axial compressor
06/21/2012CA2820030A1 Turbine engine blade having improved stacking law
06/21/2012CA2762710A1 Gas turbine for aeronautic engines
06/21/2012CA2762496A1 Gas turbine bladed rotor for aeronautic engines and method for cooling said bladed rotor
06/20/2012EP2466072A2 Axial air movement fans
06/20/2012EP2466071A2 Cast, dual alloy turbine disk and methods of forming the same
06/20/2012EP2466070A2 Method of repairing a transition piece of a gas turbine engine
06/20/2012EP2466069A1 Thermal inspection and machining systems and methods of use
06/20/2012EP2465977A1 Methods for producing a high temperature oxidation resistant coating on superalloy substrates and the coated superalloy substrates thereby produced
06/20/2012EP2465957A1 Ni-BASED MONOCRYSTALLINE SUPERALLOY AND TURBINE BLADE
06/20/2012EP2465636A1 Method and device for forming a section of a component with a predefined contour
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