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)
05/2003
05/15/2003US20030091459 Superalloy for single crystal turbine vanes
05/15/2003US20030091432 Method of forming a shaped hole
05/15/2003US20030091427 Methods and apparatus for cooling gas turbine nozzles
05/15/2003US20030088980 Method for correcting defects in a workpiece
05/15/2003US20030088958 Method and apparatus for correcting airfoil twist
05/14/2003EP1310632A1 Method and apparatus for correcting airfoil twist
05/14/2003EP1309773A1 Turbine vane system
05/14/2003EP1051568B1 Method for producing a wear-endangered component of a turbo-machine
05/14/2003EP0787221B1 Platinum aluminide cvd coating method
05/14/2003CN1418284A Cooling system for turbine blade
05/14/2003CN1417462A Cooling system for gas turbine
05/14/2003CN1417452A Turbine and its manufacture
05/14/2003CN1108441C 燃气轮机 Gas turbine
05/13/2003US6564317 Method and apparatus for securing computer firmware wherein unlocking of nonvolatile memory is prohibited unless address line masking Is disabled during an initialization event
05/13/2003US6563074 Method of machining the turbine rotor shaft of a supercharger
05/13/2003US6562483 Applying an aluminum-rich mixture to substrate to form a discontinuous layer of aluminum-rich particles in a matrix of metallic bond coat alloy; turbine blades
05/13/2003US6562157 Manufacturing process of nickel-based alloy having improved high temperature sulfidation-corrosion resistance
05/13/2003US6561764 Gas turbine rotor with an internally cooled gas turbine blade and connecting configuration including an insert strip bridging adjacent blade platforms
05/13/2003US6561761 Fluted compressor flowpath
05/13/2003US6561758 Methods and systems for cooling gas turbine engine airfoils
05/13/2003US6561757 Turbine vane segment and impingement insert configuration for fail-safe impingement insert retention
05/13/2003US6561048 Water-flow testing apparatus
05/13/2003US6560870 Method for applying diffusion aluminide coating on a selective area of a turbine engine component
05/13/2003CA2084266C Method for repairing a rotor
05/09/2003CA2361977A1 Methods for manufacture and repair and resulting components with directionally solidified or single crystal materials
05/08/2003WO2003038254A1 Turbine engine with air cooled turbine
05/08/2003WO2003038240A1 Securing device for the moving blades of axial flow turbomachines
05/08/2003WO2003038239A1 Device and method for rotor blades
05/08/2003US20030087120 Zirconium or erbium oxide; wear resistance, stability, durability
05/08/2003US20030086788 Three dimensional blade
05/08/2003US20030086785 Cooling passages and methods of fabrication
05/08/2003US20030085324 Boundary layer control of aerodynamic airfoils
05/08/2003US20030085259 Method of joining material
05/08/2003US20030084568 Method for the manufacture of a welded rotor of a fluid-flow machine
05/07/2003EP1308600A1 A cooling system for a gas turbine
05/07/2003EP1308535A1 High-temperature strength member
05/07/2003EP1308236A1 Method of forming a shaped hole
05/07/2003EP1196696B1 Rotor with a split rotor blade
05/07/2003EP1140417B1 Method for linking blade parts
05/07/2003EP0945594B1 Cooled moving blade for gas turbines
05/07/2003EP0929734B1 Gas turbine airfoil cooling
05/06/2003US6559415 Single sided laser shock peening
05/06/2003US6558485 Ablative coated surface; gas turbine engine parts
05/06/2003US6558122 Second-stage turbine bucket airfoil
05/06/2003US6558121 Method and apparatus for turbine blade contoured platform
05/06/2003US6558119 Turbine airfoil with separately formed tip and method for manufacture and repair thereof
05/06/2003US6558115 Turbine guide blade
05/06/2003US6558114 Gas turbine with baffle reducing hot gas ingress into interstage disc cavity
05/02/2003EP1306591A2 Sealing system having two concentrically arranged lips
05/02/2003EP1306524A2 Turbine shroud cooling hole configuration
05/02/2003EP1306523A1 Platforms for blades in a rotating assembly
05/02/2003EP1306522A1 Locking device for axial turbomachine blades
05/02/2003EP1306521A1 Rotor blade for a gas turbine and gas turbine with a number of rotor blades
05/02/2003EP1306520A1 Method of joining high temperature, high strength material
05/02/2003EP1306458A2 12Cr alloy steel for a turbine rotor
05/02/2003EP1306454A1 Rhenium containing protective coating protecting a product against corrosion and oxidation at high temperatures
05/02/2003EP1305133A1 Method and device for hardening a metal component by plasma pulse technology
05/01/2003WO2003036140A1 Gasket with two concentric lips
05/01/2003WO2003036049A1 Blade retention
05/01/2003WO2003036048A1 High pressure turbine blade cooling scoop
05/01/2003US20030082054 Oxidation resistant and/or abrasion resistant squealer tip and method for casting same
05/01/2003US20030082053 Repair of advanced gas turbine blades
05/01/2003US20030082048 Airfoils with improved strength and manufacture and repair thereof
05/01/2003US20030082046 Turbine shroud cooling hole diffusers and related method
05/01/2003US20030079478 High pressure turbine blade cooling scoop
05/01/2003US20030079477 Turbine engine having turbine cooled with diverted air
04/2003
04/30/2003CN1415064A Cold air refrigerating system and turboexpander turbine for this system
04/30/2003CN1414216A Heat-insulating coating material and gas turbine component and gas turbine
04/30/2003CN1414129A 12 Cr alloy steel for turbin rotor, its manufacturing method and turbin rotor
04/29/2003US6554575 Ramped tip shelf blade
04/29/2003US6554572 Gas turbine engine blade
04/29/2003US6554571 Curved turbulator configuration for airfoils and method and electrode for machining the configuration
04/29/2003US6554570 Turbine blade support assembly and a turbine assembly
04/29/2003US6554569 Compressor outlet guide vane and diffuser assembly
04/29/2003US6554566 Turbine shroud cooling hole diffusers and related method
04/29/2003US6554564 Reduced noise fan exit guide vane configuration for turbofan engines
04/29/2003US6554563 Tangential flow baffle
04/29/2003US6554562 Combustor hot streak alignment for gas turbine engine
04/29/2003US6553763 Turbocharger including a disk to reduce scalloping inefficiencies
04/29/2003US6553665 Stator vane assembly for a turbine and method for forming the assembly
04/29/2003CA2409425A1 Method of joining material
04/29/2003CA2231753C Seal plate for a gas turbine moving blade
04/29/2003CA2062026C Ductility microalloyed nial intermetallic compounds
04/24/2003WO2003033880A1 Turbine blade
04/24/2003WO2003033879A1 Sealing structure of spindle bolt, and gas turbine
04/24/2003US20030077477 Article protected by thermal barrier coating having a sintering inhibitor, and its fabrication
04/24/2003US20030077176 Bucket and wheel dovetail design for turbine rotors
04/24/2003US20030077171 Method for repairing a turbine vane
04/24/2003US20030077170 Structures of turbine scroll and blades
04/24/2003CA2409328A1 Rotor blade platform
04/23/2003EP1304446A1 Method for replacing a damaged TBC ceramic layer
04/23/2003EP1304445A2 Structure of radial turbine scroll and blades
04/23/2003EP1304397A2 Article protected by thermal barrier coating having a sintering inhibitor, and its fabrication
04/23/2003EP1105243B1 Turbine rotor modernization and repair method
04/23/2003CN1413288A Steam turbine operating method, and turbine device provided with steam turbine that functions according to said method
04/23/2003CN1413270A Chemical cleaning solution for gas turbine blades
04/23/2003CN1412418A Blade for turbomachine rotor and seallow-tail joint of impeller
04/23/2003CN1412417A Turbine volute pipeline and moving blade structure
04/23/2003CN1106496C Turbine shaft and process for cooling it
04/22/2003US6551372 Nickel base powder metallurgy superalloy gas turbine engine disk for a compressor or turbine; enhanced fatigue crack growth resistance and a superior balance of mechanical properties
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