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)
11/2010
11/18/2010US20100290897 Tip Shrouded Turbine Blade
11/18/2010US20100290891 Component Cooling Through Seals
11/18/2010DE202010012298U1 Gas.bzw. Gas.bzw. Dampfturbine Steam turbine
11/18/2010DE112008003526T5 Instabilitätschutzsystem unter Verwendung von Rotorplasmaaktuatoren Instability mitigation system using rotor plasma actuators
11/18/2010DE102010019197A1 Schaufeln mit Schwingungsdämpfungssystem Blades with vibration damping system
11/18/2010DE102010016824A1 Kupplung für Rotationskomponenten Coupling for rotational components
11/18/2010DE102010016658A1 Verfahren und Vorrichtung für Turbinenmotoren Method and apparatus for turbine engines
11/18/2010DE102008056059B4 Abgasturbolader und Verfahren zur Montage eines Abgasturboladers The exhaust gas turbocharger and method of assembling an exhaust gas turbocharger
11/18/2010DE102005033591B4 Hohlschaufel Hollow blade
11/17/2010EP2251535A2 A damping assembly
11/17/2010EP2251530A1 Gas turbine
11/17/2010EP2251529A2 Rotary machine balance weights
11/17/2010EP2251445A1 Tial-based alloy, process for production of the same, and rotor blade comprising the same
11/17/2010EP2251140A1 Method for burnishing and polishing the surface of metallic components
11/17/2010EP2251136A1 Method for reconditioning a turbine blade
11/17/2010EP2250346A2 Shrouded turbine blade design
11/17/2010EP2126287B1 Eccentric chamfer at inlet of branches in a flow channel
11/17/2010EP1656493B1 Stationary gas turbine
11/17/2010CN201635773U Turbocharger spindle
11/17/2010CN101886555A Sealing device for rotor blade of flue gas turbine expander
11/17/2010CN101886552A Coupling for rotary components
11/17/2010CN101886551A Rotor blades with vibration damping system
11/16/2010US7832988 Turbine blade
11/16/2010US7832986 Multi-alloy turbine rotors and methods of manufacturing the rotors
11/16/2010CA2604757C Steam turbine rotor blade
11/11/2010WO2010128229A1 Fan rotor for an airplane turbojet engine
11/11/2010WO2010128025A1 Housing for a stator of an aircraft turbine engine, comprising slits for the mechanical offloading of blades
11/11/2010US20100284822 Turbine Airfoil with a Compliant Outer Wall
11/11/2010US20100284820 Locking plate fast fastening ceiling fan blades
11/11/2010US20100284819 Turbine blades and methods of forming modified turbine blades and turbine rotors
11/11/2010US20100284818 Turbine blade cascade endwall
11/11/2010US20100284817 Method for producing a blisk or a bling, component produced therewith and turbine blade
11/11/2010US20100284816 Airfoil attachment
11/11/2010US20100284815 Compound variable elliptical airfoil fillet
11/11/2010US20100284814 Machine component retention
11/11/2010US20100284811 Turbine shroud ring with rotation proofing recess
11/11/2010US20100284810 Process for inhibiting delamination in a bend of a continuous fiber-reinforced composite article
11/11/2010US20100284807 Blade cooling
11/11/2010US20100284801 Turbo machine blade
11/11/2010US20100284799 Method and apparatus for turbine engines
11/11/2010US20100284798 Turbine Airfoil With Dual Wall Formed from Inner and Outer Layers Separated by a Compliant Structure
11/11/2010US20100284794 Low pressure turbine rotor disk
11/11/2010US20100283251 Turbine assembly
11/11/2010US20100281690 Method of manufacturing a blade
11/11/2010DE102009020592A1 Charging device i.e. exhaust gas turbocharger, for motor vehicle, has flow channel lying between rotatably supported guide vanes, where one guide vane is flow-permeable and forms another flow channel
11/11/2010DE102009020591A1 Charging device i.e. exhaust gas turbocharger, for internal combustion engine of motor vehicle, has guide vanes arranged in inflow zone for gases, and recess formed between head end and foot end of guide vanes
11/11/2010CA2760667A1 Housing for a stator of an aircraft turbine engine, comprising slits for the mechanical offloading of blades
11/11/2010CA2760470A1 Fan rotor for an airplane turbojet engine
11/10/2010EP2249045A2 Compressor or pump with fluid extraction
11/10/2010EP2249044A2 Compressor or pump with fluid extraction
11/10/2010EP2249043A2 Compressor or pump with fluid extraction
11/10/2010EP2248997A2 System and method for improved film cooling
11/10/2010EP2248996A1 Gas turbine
11/10/2010EP2248929A1 Method of electrical discharge surface repair of a variable vane trunnion
11/10/2010EP2248923A1 Nickel base y/ý superalloy with multiple reactive elements and use of said superalloy in complex material systems
11/10/2010EP2247935A1 Method for testing the coating of a vane base
11/10/2010CN1840857B Axial turbine
11/10/2010CN101883922A Wind turbine blade with submerged boundary layer control means comprisin crossing sub-channels
11/10/2010CN101881185A Method and apparatus for turbine engines
11/10/2010CN101300374B Two-layer thermal barrier coating system containing a pyrochlore phase
11/09/2010US7828526 Metallic blade having a composite inlay
11/09/2010US7828521 Turbine module for a gas-turbine engine
11/09/2010US7828515 Multiple piece turbine airfoil
11/09/2010US7828514 Rotor for an engine
11/09/2010US7827686 Method for the maintenance of gas turbines
11/09/2010CA2525845C Method for reaction control coating
11/09/2010CA2449263C Row of long and short chord length and high and low temperature capability turbine airfoils
11/09/2010CA2435360C Aircraft gas turbine engine with control vanes for counter rotating low pressure turbines
11/04/2010WO2010125089A1 Strengthened fan-blade block
11/04/2010WO2010124923A1 NICKEL BASE γ/ γ' SUPERALLOY WITH MULTIPLE REACTIVE ELEMENTS AND USE OF SAID SUPERALLOY IN COMPLEX MATERIAL SYSTEMS
11/04/2010WO2010071703A8 Durable thermal barrier coating compositions, coated articles, and coating methods
11/04/2010US20100278652 Tangential entry dovetail cantilever load sharing
11/04/2010US20100278651 Guide device
11/04/2010US20100278642 Bypass lip seal
11/04/2010DE112008003453T5 Rotormontagesystem und -verfahren Rotor assembly system and method
11/04/2010DE102009018924A1 Bidirektional anströmbare Turbine Bidirectional anströmbare turbine
11/04/2010CA2760290A1 Strengthened fan-blade block
11/03/2010EP2246575A1 Rotor blade assembly for an axial compressor
11/03/2010EP2246527A2 Gas turbine bucket dovetail
11/03/2010EP2246526A1 Turbine disc and gas turbine
11/03/2010EP2246525A1 Gas turbin and disc and method for forming radial passage of disc
11/03/2010EP2246449A1 Ni-base superalloy with excellent segregation properties
11/03/2010EP2246133A1 RMC-defined tip blowing slots for turbine blades
11/03/2010EP2245275A1 Guide vane for a variable turbine geometry
11/03/2010EP2245274A1 Device and method for the partial coating of components
11/03/2010EP2245273A1 Turbine vane for a stationary gas turbine
11/03/2010EP2245272A1 Multi-component bladed rotor for a turbomachine
11/03/2010EP1292760B1 Configuration of a coolable turbine blade
11/03/2010CN201620917U Last-stage moving blade of large stream turbine
11/03/2010CN1942656B Gas turbine with a compressor housing which is protected against cooling down and method for operating a gas turbine
11/03/2010CN1854465B Finger dovetail attachment between a turbine rotor wheel and bucket for stress reduction
11/03/2010CN101878317A Alloy material having high-temperature corrosion resistance, heat-shielding coating material, turbine member, and gas turbine
11/03/2010CN101220756B Axial rotor section for a rotor of a turbine
11/03/2010CN101128649B Component comprising an embedded channel, in particular a hot gas component of a turbomachine
11/02/2010US7825348 Method of repairing a blade of a one-piece bladed disc of a turbomachine and test piece for implementing the method
11/02/2010US7824159 Compressor, titanium-made rotor blade, jet engine and titanium-made rotor blade producing method
11/02/2010US7824158 Bimaterial turbine blade damper
11/02/2010US7824157 System for retaining blades in a rotor
11/02/2010US7824156 Cooled component of a fluid-flow machine, method of casting a cooled component, and a gas turbine
11/02/2010US7824150 Multiple piece turbine airfoil
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