Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
09/2010
09/01/2010CN101818286A Ni-based alloy for a forged part of a steam turbine, rotor blade of a steam turbine, stator blade of a steam turbine, screw member for a steam turbine, and pipe for a steam turbine
08/2010
08/31/2010US7785671 metal substrate, metal bonding layer, ceramics thermal barrier; columnar structure of stabilized zirconia, or ZrO2-HfO2 solid solution; simultaneously melting two ZrO2 deposition and Lanthanum oxide deposition materials by electron beam physical vapor deposition; low thermal conductivity; durability
08/31/2010US7785076 Refractory component with ceramic matrix composite skeleton
08/31/2010US7785075 Optimized aerodynamic profile for a turbine blade
08/31/2010US7785071 Turbine airfoil with spiral trailing edge cooling passages
08/31/2010US7784267 Detonation engine and flying object provided therewith
08/31/2010US7784182 System for manufacturing a rotor having an MMC ring component and a unitary airfoil component
08/26/2010WO2010094540A1 Blade union of a turbo machine
08/26/2010WO2010094539A1 Rotor section for a rotor of a turbomachine, rotor blade for a turbomachine
08/26/2010WO2010094273A2 Production of a turbine blisk having an oxidation and/or corrosion protection layer
08/26/2010WO2010094256A1 Anti-erosion coating system for gas turbine components
08/26/2010WO2010094255A1 Method for the production of an integrally bladed rotor, and rotor
08/26/2010WO2009148655A3 Turbine airfoil with metered cooling cavity
08/26/2010WO2009138057A3 Shroud for rotating blades of a turbo machine
08/26/2010US20100215508 Axially Segmented Impeller
08/26/2010US20100215503 Transonic blade
08/26/2010US20100215501 Apparatus for bucket cover plate retention
08/26/2010US20100215499 Blade retaining device for turbo machine propeller
08/26/2010US20100215498 Blade for turbomachine receiving part, comprising an airfoil part including a mechanical fuse
08/26/2010US20100215495 Tapered helical auger turbine to convert hydrokinetic energy into electrical energy
08/26/2010US20100215481 Running-gap control system of an aircraft gas turbine
08/26/2010DE102009010185A1 Gasturbinenmaschine Gas turbine engine
08/26/2010CA2841296A1 Rotor section for a rotor of a turbomachine, and rotor blade for a turbomachine
08/26/2010CA2753268A1 Anti-erosion coating system for gas turbine components
08/26/2010CA2752666A1 Rotor section for a rotor of a turbomachine, and rotor blade for a turbomachine
08/25/2010EP2221454A1 Gas turbine shrouded blade
08/25/2010EP2221453A2 Airfoil insert and corresponding airfoil and assembly
08/25/2010EP2221247A2 Mounting arrangement for a nose cone of a gas turbine engine
08/25/2010EP2220342A1 Erosion protection shield for rotor blades
08/25/2010EP2219819A1 Method for the production of an integrally bladed rotor, and rotor
08/25/2010CN201560805U High efficiency mixed flow turbine
08/25/2010CN101813005A Enhanced heat transfer device in a structure with large and small interlacing fins
08/25/2010CN101813004A Method for calculating arc line in mechanical blade of impeller
08/25/2010CN101368489B Ultra-high parameter water-saving type air cooling turbine
08/24/2010US7780420 Turbine blade with a foam metal leading or trailing edge
08/24/2010US7780419 Replaceable leading edge insert for an IBR
08/24/2010US7780415 Turbine blade having a convergent cavity cooling system for a trailing edge
08/24/2010US7780414 Turbine blade with multiple metering trailing edge cooling holes
08/24/2010US7780413 Turbine airfoil with near wall inflow chambers
08/24/2010US7779541 Method for manufacturing a stator or rotor component
08/24/2010CA2519842C Thermal barrier coating material
08/19/2010WO2010091973A1 Method and device for dynamic measurement of the imbalance of the rotor of a turbo charger basic unit
08/19/2010WO2010091942A1 Method for heating a turbine shaft
08/19/2010WO2010091667A1 Coating and method for coating a workpiece
08/19/2010WO2010000229A3 Blade cascade for a flow engine and flow engine comprising said blade cascade
08/19/2010US20100209255 aerofoil structure and a method of making a rib for an aerofoil structure
08/19/2010US20100209253 Fan blade anti-fretting insert
08/19/2010US20100209252 Disk for turbine engine
08/19/2010US20100209251 Fan blade platform
08/19/2010US20100209239 Vane
08/19/2010US20100209229 Airfoil inserts, flow-directing elements and assemblies thereof
08/19/2010DE102009008887A1 Verfahren zum Herstellen einer Schaufelpanzerung auf einer Schaufel für eine Turbomaschine A method of manufacturing a blade armor on a blade for a turbomachine
08/19/2010DE102009007945A1 Gewindeelement, Vorrichtung mit Gewindeelement, System sowie Handhabungsverfahren Threaded element with threaded element, system and handling procedures
08/19/2010DE102009007468A1 Integral beschaufelte Rotorscheibe für eine Turbine The integrally bladed rotor disk for a turbine
08/18/2010EP2218947A1 Rotor for a flow machine with a shaft seal and method for repairing the rotor
08/18/2010EP2218893A2 Cooled vane for gas turbine exhaust duct
08/18/2010EP2218892A2 Cooled vane for gas turbine exhaust duct
08/18/2010EP2218875A1 Blade formation of a flow machine
08/18/2010EP2218874A2 Turbine vane airfoil with turning flow and axial/circumferential trailing edge configuration
08/18/2010EP2218873A1 Rotor section for a rotor of a turbo machine, rotor blade for a turbo machine and blocking element
08/18/2010EP2218872A1 Rotor disc
08/18/2010EP2218530A1 High Pressure Turbine Rotor and Process for its Manufacture
08/18/2010EP2217901A2 Device for dynamically measuring the imbalance of the rotor of a turbocharger
08/18/2010EP2217792A2 A wind turbine, a method for coupling a first drive train component of the drive train of a wind turbine to a second drive train component of the drive train and use of a wind turbine
08/18/2010CN101809252A 蒸气轮机设备 Steam turbine facility
08/18/2010CN101198713B Layer system for a component comprising a thermally insulating layer and a metallic anti-erosion layer, method for the production and method for the operation of a steam turbine
08/18/2010CA2693046A1 Fan blade platform
08/17/2010US7776459 High sodium containing thermal barrier coating
08/17/2010US7775772 System for manufacturing a rotor having an MMC ring component and an airfoil component having MMC airfoils
08/17/2010US7775769 Turbine airfoil fillet region cooling
08/17/2010US7775768 Turbine component with axially spaced radially flowing microcircuit cooling channels
08/17/2010US7775764 Gas turbine engine rotor ventilation arrangement
08/17/2010CA2462846C Method for removing coating material from a cooling hole of a gas turbine engine component
08/12/2010WO2010091011A1 Turbine energy generating system
08/12/2010WO2010090329A1 Process for producing sintered sialon ceramic
08/12/2010WO2010089466A1 Diffuser/rectifier assembly for a turbine engine
08/12/2010WO2010089201A1 Method for producing a closed compressor rotor
08/12/2010WO2010089183A1 Turbine component having easily removable protective layer, set of turbine components, a turbine and a method for protecting a turbine component
08/12/2010WO2010089028A1 Exhaust gas turbocharger and system having an exhaust gas turbocharger
08/12/2010WO2010088882A2 Integrally bladed rotor disk for a turbine
08/12/2010WO2010088881A1 Sealing apparatus at the blade shaft of a rotor stage of an axial turbomachine
08/12/2010WO2010088879A1 Method for producing a wear-resistant coating on a component
08/12/2010US20100202891 Low-pressure turbine rotor
08/12/2010US20100202890 Turbine of a gas turbine
08/12/2010US20100202889 Method for producing a lightweight turbine blade
08/12/2010US20100202876 Steam turbine facility
08/12/2010DE102009008510A1 Beschichtung und Verfahren zum Beschichten eines Werkstücks Coating and process for coating a workpiece
08/12/2010DE102009007666A1 Verfahren zur Herstellung einer verschleißfesten Beschichtung auf einem Bauteil A process for producing a wear resistant coating on a component
08/12/2010DE102009007664A1 Abdichtvorrichtung an dem Schaufelschaft einer Rotorstufe einer axialen Strömungsmaschine Sealing of the vane shaft of a rotor stage axial flow machine
08/12/2010DE102009007164A1 Verfahren zum Ausbilden einer Kühlluftöffnung in einer Wand einer Gasturbinenbrennkammer sowie nach dem Verfahren hergestellte Brennkammerwand A method for forming a cooling air opening in a wall of a gas turbine combustor as well as prepared by the process chamber wall
08/12/2010CA2750856A1 Diffuser/rectifier assembly for a turbine engine
08/12/2010CA2692134A1 Radial or diagonal fan wheel
08/11/2010EP2216509A1 Turbine component with easily removable protective layer, turbine component set, a turbine and method for protecting a turbine component
08/11/2010EP2216508A2 Ceramic matrix composite turbine nozzle, transition duct and turbine engine
08/11/2010EP2216507A2 Method of manufacture of retrofit turbine blade.
08/11/2010EP2216506A1 Method for heating a turbine shaft
08/11/2010EP2216505A2 Turbine coverplate systems
08/11/2010EP2215330A1 Aerodynamic performance enhancements using discharge plasma actuators
08/11/2010EP2215329A1 Production process for a rotor
08/11/2010EP1678410B1 Method for joining blades to blade roots or rotor disks when producing and/or repairing gas turbine blades or integrally bladed gas turbine rotors