Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
02/2015
02/24/2015US8961136 Turbine airfoil with film cooling hole
02/24/2015US8961135 Mateface gap configuration for gas turbine engine
02/24/2015US8961134 Turbine blade or vane with separate endwall
02/24/2015US8961133 Gas turbine engine and cooled airfoil
02/24/2015US8961132 Secondary flow arrangement for slotted rotor
02/24/2015US8961131 Arrangement for extracting energy from flowing liquid
02/24/2015US8961129 Method and device for joining metal elements
02/24/2015US8961118 Structural cooling fluid tube for supporting a turbine component and supplying cooling fluid
02/24/2015US8961114 Integrated variable geometry flow restrictor and heat exchanger
02/24/2015CA2778053C Steam turbine with fork-type blade attachments
02/24/2015CA2638535C Turbine blade with internal cooling structure
02/24/2015CA2636665C Ventilation air supply device for the blades of a low pressure turbine in a gas turbine engine
02/24/2015CA2610173C Hp turbine vane airfoil profile
02/19/2015WO2015023860A1 Coating pocket stress reduction for rotor disk of a gas turbine engine
02/19/2015WO2015023506A1 Repair system for turbomachinery components using additive manufacturing technology
02/19/2015WO2015023345A2 Composite airfoil metal patch
02/19/2015WO2015023342A2 Gas turbine engine with dove-tailed tobi vane
02/19/2015WO2015023338A2 Gas turbine engine component having trip strips
02/19/2015WO2015023331A2 Turbine vane with non-uniform wall thickness
02/19/2015WO2015023325A1 Non-axisymmetric fan flow path
02/19/2015WO2015023322A2 Method for detecting a compromised component
02/19/2015WO2015022463A1 Turbine engine stator blade
02/19/2015US20150050160 Rotor shaft for a turbomachine
02/19/2015US20150050159 Dual element turbine blade
02/19/2015US20150050158 Gas turbine engine component including a compliant layer
02/19/2015US20150050157 Hold and cool process for superalloy joining
02/19/2015US20150050155 Impeller for fuel pump of vehicle
02/19/2015US20150050154 Airfoil trailing edge apparatus for noise reduction
02/19/2015US20150048058 Method for automated superalloy laser cladding with 3d imaging weld path control
02/19/2015US20150047191 Method for balancing and assembling a turbine rotor
02/19/2015US20150047168 Repair chain for turbomachinery components using additive manufacturing technology
02/19/2015DE112006001614B4 Turbomaschinenschaufel Turbomachine blade
02/19/2015DE102014111151A1 Turbinenrotor- und Schaufelblattanordnung mit mehrteiligem Verriegelungsschaufelblatt Turbine rotor and blade assembly with multi-locking blade
02/19/2015DE102013216392A1 Vorrichtung und Verfahren zur Regelung der Temperatur eines Bauteils einer Strömungsmaschine Apparatus and method for controlling the temperature of a component of a turbomachine
02/19/2015DE102013213834A1 Verfahren zum Herstellen eines Isolationselements und Isolationselement für ein Gehäuse eines Flugtriebwerks A method for manufacturing an insulation element, and insulation member for a housing of an aircraft engine
02/19/2015DE10156228B4 Rotor einer Expansionsturbine für Tieftemperaturanwendungen The rotor of an expansion turbine for low-temperature applications
02/18/2015EP2837796A1 Method for manufacturing coupled turbine blades, and coupled turbine blades
02/18/2015EP2837775A1 Fixation device for turbine and method for applying fixation
02/18/2015EP2837769A1 Rotor shaft for a turbomachine
02/18/2015EP2837457A1 A technique for brazing turbomachine components
02/18/2015EP2836683A2 Tie shaft arrangement for turbomachine
02/18/2015EP2836682A2 Turbine blade damper seal
02/18/2015EP2836681A1 Coupling of shafts using variable profile splines
02/18/2015EP2836322A1 Method for producing low-pressure turbine blades from tial
02/17/2015US8956700 Method for adhering a coating to a substrate structure
02/17/2015US8956487 Rotor blade of a gas turbine engine made of composite material comprising a connecting yoke, method for manufacturing the blade
02/17/2015US8956123 Small scale high speed turbomachinery
02/17/2015US8956122 Blade fastening having safety device for turbine blades
02/17/2015US8956121 Multilayer-type fan device
02/17/2015US8956120 Non-continuous ring seal
02/17/2015US8956119 Turbine wheel provided with an axial retention device that locks blades in relation to a disk
02/17/2015US8956116 Cooling of a gas turbine component designed as a rotor disk or turbine blade
02/17/2015US8956112 CMC turbine stator blade
02/17/2015US8956105 Turbine vane for gas turbine engine
02/17/2015US8956104 Bucket assembly for turbine system
02/17/2015US8955576 Cast features for a turbine engine airfoil
02/17/2015US8955303 Pulse detonation system
02/17/2015CA2640003C Foil for turbomachine blade
02/17/2015CA2600194C Hp turbine blade airfoil profile
02/17/2015CA2543226C Protective part for the leading edge of a blade
02/12/2015WO2015021086A1 Mounting apparatus for low-ductility turbine nozzle
02/12/2015WO2015020931A2 Cover plate assembly for a gas turbine engine
02/12/2015WO2015020806A1 Airfoil trailing edge tip cooling
02/12/2015WO2015020751A1 Manufacturing method for strut shield collar of gas turbine exhaust diffuser
02/12/2015WO2015020720A2 Gas turbine engine component with rib support
02/12/2015WO2015020715A2 Gas turbine hub
02/12/2015WO2015020711A2 Gas turbine blade configuration
02/12/2015WO2015018841A1 Insert element, ring segment, gas turbine, mounting method
02/12/2015US20150044444 Method of forming thermal barrier coating, thermal barrier coating formed thereby, and article comprising same
02/12/2015US20150044382 Method of impregnating ceramic cores for the manufacture of turbomachine blades
02/12/2015US20150044059 Airfoil for a turbine system
02/12/2015US20150044056 Airfoil with leading edge reinforcement
02/12/2015US20150044054 Composite retention feature
02/12/2015US20150044053 Steam Turbine Rotor
02/12/2015US20150044052 Geared Turbofan With Fan Blades Designed To Achieve Laminar Flow
02/12/2015US20150044050 Composite blade with an integral blade tip shroud and method of forming the same
02/12/2015US20150044049 Dovetail retention system for blade tracks
02/12/2015US20150044048 Impeller assembly of fluid rotary machine and manufacturing method thereof
02/12/2015US20150044038 Blade cascade and turbomachine
02/12/2015US20150044029 Aerofoil
02/12/2015US20150044025 Turbine
02/12/2015US20150041434 Method for separating a metal part from a ceramic part
02/12/2015US20150040582 Crossover cooled airfoil trailing edge
02/12/2015US20150040570 Gas turbine engine component having foam core and composite skin with cooling slot
02/12/2015US20150040395 Method for repairing wear marks on a rotor supporting the fan of a bypass engine
02/12/2015DE102014111005A1 Schaufelblatt für ein Turbinensystem Airfoil for a turbine system
02/12/2015DE102014111004A1 Verdichterlaufschaufelbefestigungsanordnung Compressor blade mounting arrangement
02/12/2015DE102014110332A1 Schaufelblatt mit einer Hinterkantenergänzungsstruktur Airfoil with trailing edge complement structure
02/12/2015DE102014110315A1 Turbomaschinenschaufelpositionierung Turbomachine blade positioning
02/12/2015DE102013226422B3 Ein Verfahren zur Herstellung von Schaufeln A process for the preparation of blades
02/12/2015DE102013215808A1 Rotornabenanordnung, elektrischer Lüfter Rotor hub assembly, electric fan
02/12/2015DE10140742B4 Vorrichtung zur Dichtspaltreduzierung zwischen einer rotierenden und einer stationären Komponente innerhalb einer axial durchströmten Strömungsmaschine A device for sealing gap reduction between a rotating and a stationary component in an axial-flow turbomachine
02/11/2015EP2835502A2 Blade of a turbine
02/11/2015EP2835501A1 Aerofoil component and corresponding gas turbine engine
02/11/2015EP2835500A1 Insert element and gas turbine
02/11/2015EP2835499A1 Blade row and corresponding flow machine
02/11/2015EP2835498A1 Welded steam turbine rotor made of chromium alloy steel
02/11/2015EP2835497A2 Remote turbine component replacement apparatus and method of remotely replacing a turbine component
02/11/2015EP2834498A1 Cooling system for a turbine vane
02/11/2015EP2834470A1 Turbomachine rotor blade, monoblock blisk, compressor rotor, fan rotor associated therewith
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