Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
09/2014
09/11/2014US20140255198 Turbine disk fabrication with in situ material property variation
09/11/2014US20140255197 Rotor blades for gas turbine engines
09/11/2014US20140255196 Double split blade lock ring
09/11/2014US20140255195 Bucket Connection for a Turbine Runner
09/11/2014US20140255194 Tip shrouds of turbine rotor blades and methods of manufacture related thereto
09/11/2014US20140255192 Turbine rotor for a thermoelectric power station
09/11/2014US20140255188 Gas turbine engine airflow member having spherical end
09/11/2014US20140255187 Attachment feature of a gas turbine engine blade having a curved profile
09/11/2014US20140255174 Manufacture of full ring strut vane pack
09/11/2014US20140255170 Cmc turbine engine component
09/11/2014US20140255158 Coating process for gas turbine engine component with cooling holes
09/11/2014US20140255154 Reaction-type turbine
09/11/2014US20140250897 Tip-controlled integrally bladed rotor for gas turbine engine
09/11/2014DE102013203889A1 Reparaturverfahren für eine Schaufel von einer Gasturbine und korrespondierende Schaufel Repair method for a blade of a gas turbine blade and corresponding
09/11/2014DE102011119910B4 Verfahren zur Herstellung eines Schaufelrads mit einem mit wenigstens einer Laufschaufel verbundenen Scheibenkörper A method for producing a blade wheel with a part connected to at least one rotor blade disk body
09/11/2014DE102010047906B4 Verfahren zur elektrochemischen partiellen Beschichtung eines Bauteils sowie Vorrichtung Process for the electrochemical partial coating of a component, as well as apparatus
09/11/2014DE10059997B4 Kühlbare Schaufel für eine Gasturbinenkomponente Coolable blade for a gas turbine component
09/10/2014EP2775337A2 Photography system and photography method
09/10/2014EP2775101A1 Gas turbine blade
09/10/2014EP2775100A2 Turbine blade cooling channel formation
09/10/2014EP2775099A1 Methods for the new manufacture of a diffuser in a layer system
09/10/2014EP2775098A2 Integrated strut-vane
09/10/2014EP2775097A2 Stator vane row
09/10/2014EP2775096A2 Diffuser assembly for an exhaust housing of a steam turbine, and steam turbine with the same
09/10/2014EP2775008A1 Low energy plasma coating
09/10/2014EP2774843A1 System and method for reducing rotor blade noise
09/10/2014EP2774716A2 Method of producing a hollow airfoil
09/10/2014EP2774715A1 Method for repairing an external surface or a free-standing wall of a component
09/10/2014EP2774711A2 Supporting machine for welding rotor parts, welding machine with such supporting machine and method of supporting rotor parts during welding
09/10/2014EP2774710A1 Surface and crack repair by means of different soldering materials
09/09/2014US8827654 Compressor blade of a gas-turbine engine with a self-sharpening leading-edge structure
09/09/2014US8827651 Annulus filler
09/09/2014US8827650 Seal for a platform in the rotor of a turbine engine
09/09/2014US8827647 Turbine blade with root section cooling
09/09/2014US8827646 Gas turbine blade, manufacturing method therefor, and gas turbine using turbine blade
09/09/2014US8827643 Turbine bucket platform leading edge scalloping for performance and secondary flow and related method
09/09/2014US8827642 Flexible seal for turbine engine
09/09/2014US8827632 Integrated TBC and cooling flow metering plate in turbine vane
09/09/2014US8826668 Two stage serial impingement cooling for isogrid structures
09/09/2014US8826536 Blade preloading method
09/09/2014US8826535 Method for manufacturing an integrally bladed rotor
09/09/2014CA2726773C Windward cooled turbine nozzle
09/09/2014CA2554341C Thermally compliant turbine shroud mounting
09/09/2014CA2554137C Thermally compliant turbine shroud mounting assembly
09/09/2014CA2490337C High temperature alloys, and articles made and repaired therewith
09/08/2014CA2844369A1 Rotor blades for gas turbine engines
09/04/2014WO2014133804A1 Split airfoil cluster and method therefor
09/04/2014WO2014133721A1 Gas turbine engine thin wall composite vane airfoil
09/04/2014WO2014133706A1 Edge treatment for gas turbine engine component
09/04/2014WO2014133659A1 High pressure compressor thermal management and method of assembly and cooling
09/04/2014WO2014133613A2 Fan blades for gas turbine engines with reduced stress concentration at leading edge
09/04/2014WO2014133612A1 Gas turbine engine variable geometry flow component
09/04/2014WO2014133546A1 Composite airfoil metal leading edge assembly
09/04/2014WO2014133538A1 High temperature bond coating with increased oxidation resistance
09/04/2014US20140248157 Blade or vane of differing roughness and production process
09/04/2014US20140248155 One-block bladed disk provided with blades with adapted foot profile
09/04/2014US20140248154 Blade of a row of rotor blades or stator blades for use in a turbomachine
09/04/2014US20140248152 Plate for directing flow and film cooling of components
09/04/2014US20140248139 Turbomachine bucket having flow interrupter and related turbomachine
09/04/2014US20140245753 Gas turbine engine rotor blade
09/04/2014US20140245752 System and method for attaching a rotating blade in a turbine
09/04/2014DE102014102211A1 Turbomaschinenschaufel mit einem Strömungsunterbrecher und entsprechende Turbomaschine Turbo machine blade with a flow breaker and corresponding turbomachine
09/04/2014DE102010035393B4 Turbine und Verfahren zum Betrieb einer Turbine für ein CAES-System Turbine and method for operating a turbine for a CAES system
09/03/2014EP2772615A1 Turbomachine blade and relative production method
09/03/2014EP2772614A1 Turbomachine blade production method
09/03/2014EP2772613A1 Turbomachine blade and relative production method
09/03/2014EP2772331A1 A plug, a method for closing a hole by means of such a plug, and the manufacture of such a plug
09/03/2014EP2771547A2 Method for manufacturing a turbine nozzle guide vanes sector or a compressor guide vanes sector from composite material for a turbomachine
09/03/2014EP2771546A1 Surface having specially formed recesses and component
09/02/2014US8821127 Blade lock for compressor
09/02/2014US8821125 Turbine blade having improved flutter capability and increased turbine stage output
09/02/2014US8821124 Hybrid structure airfoil
09/02/2014US8821122 Integrally bladed rotor disk for a turbine
09/02/2014US8821119 Blade
09/02/2014US8821116 Abradable coating system
09/02/2014US8821111 Gas turbine vane with cooling channel end turn structure
09/02/2014US8821107 Method of modifying a steam turbine
09/02/2014US8820754 Turbine blade seal assembly
09/02/2014US8820092 Gas turbine engine cooling system and method
09/02/2014US8820072 Compressor diffuser plate
09/02/2014CA2612038C Cmc articles having small complex features
09/02/2014CA2552214C Blades for a gas turbine engine with integrated sealing plate and method
09/02/2014CA2551218C Counterflow film cooled wall
08/2014
08/28/2014WO2014130332A1 Gas turbine engine having a mistuned stage
08/28/2014WO2014130292A1 Hybrid turbine blade including multiple insert sections
08/28/2014WO2014130244A1 Gas turbine engine airfoil platform cooling passage and core
08/28/2014WO2014130151A1 Insulating coating to permit higher operating temperatures
08/28/2014WO2014130149A1 Disk and blade stalk bounded by motion weld and methods for motion welding
08/28/2014WO2014130134A2 Propeller
08/28/2014WO2014130131A2 Attachment of composite article
08/28/2014WO2014128169A1 Method for making an impeller from sector segments
08/28/2014WO2014105701A3 Non-integral fan blade platform
08/28/2014WO2014099082A3 Turbine blade root profile
08/28/2014WO2014092834A3 High pressure rotor disk
08/28/2014WO2014088673A3 Gas turbine engine fan spacer platform attachments
08/28/2014WO2014074199A3 Root bow geometry for airfoil shaped vane
08/28/2014US20140242411 High temperature thermal barrier coating
08/28/2014US20140241901 Impeller
08/28/2014US20140241900 Methods for repairing a turbine airfoil constructed from cmc material
08/28/2014US20140241899 Blade leading edge tip rib
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