Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
06/2012
06/05/2012US8192163 Wiper for wind turbine blades
06/05/2012US8192162 Field installable and removable helicopter rotor blade vibration and blade tracking device
06/05/2012US8192151 Turbine engine having cooling gland
06/05/2012US8192149 Turbine or compressor stage for a turbojet
06/05/2012US8192145 Turbine nozzle sector
06/05/2012US8192142 Steam turbine
06/05/2012US8191374 Two-shaft gas turbine
06/05/2012CA2541209C Method for masking a workpiece
05/2012
05/31/2012WO2012071166A2 Integrated variable geometry flow restrictor and heat exchanger
05/31/2012WO2012070984A1 Orthogonal turbine
05/31/2012WO2012069770A1 Fanwheel attachment using expansion-tolerant conically tapered rings
05/31/2012WO2012069744A1 Turbomachine rotor blade and associated turbomachine
05/31/2012WO2012069306A1 METALLIC BONDCOAT OR ALLOY WITH A HIGH γ/γ' TRANSITION TEMPERATURE AND A COMPONENT
05/31/2012WO2012069305A1 METALLIC BONDCOAT OR ALLOY WITH A HIGH γ/γ' TRANSITION TEMPERATURE AND A COMPONENT
05/31/2012WO2012069273A1 Turbine nozzle segment and corresponding gas turbine engine
05/31/2012US20120134845 Blade for a gas turbine, method for manufacturing a turbine blade, and gas turbine with a blade
05/31/2012US20120134834 Asymmetrical rotor blade slot attachment
05/31/2012US20120134822 Hub for a propeller having variable pitch blades
05/31/2012US20120134786 Compressor blade with flexible tip elements and process therefor
05/31/2012US20120134781 Axial flow gas turbine
05/31/2012US20120134780 Axial flow gas turbine
05/31/2012US20120134779 Gas turbine of the axial flow type
05/31/2012US20120134778 Axial flow gas turbine
05/31/2012DE102011117755A1 Blade arrangement, particularly guide vane arrangement, for rotating turbo-engine, particularly turbine, has blade root, which has upstream blade root front edge and downstream blade root rear edge
05/31/2012DE102010052965A1 Dämpfungsmittel zum Dämpfen einer Schaufelbewegung einer Turbomaschine Damping means for damping movement of a blade of a turbomachine
05/31/2012CA2818093A1 Turbomachine rotor blade and associated turbomachine
05/31/2012CA2817526A1 Integrated variable geometry flow restrictor and heat exchanger
05/30/2012EP2458156A2 Turbine engine stator e.g. a compressor stator
05/30/2012EP2458155A2 Gas turbine of the axial flow type
05/30/2012EP2458154A1 Rotor disk with asymmetrical rotor blade slot, corresponding blade and manufacturing method
05/30/2012EP2458153A2 Impact tolerant composite airfoil for a turbine engine
05/30/2012EP2458152A2 Gas turbine of the axial flow type
05/30/2012EP2458151A2 Blade for a gas turbine, method for manufacturing said blade and gas turbine with such a blade
05/30/2012EP2458150A1 Method for damping mechanical vibrations occurring during operation in a turbomachine blade, turbomachine blade for carrying out the method and piezoelectric damping element to be installed in such a turbomachine blade
05/30/2012EP2458149A1 Aircraft engine blades
05/30/2012EP2458148A1 Turbo-machine component with a surface for cooling
05/30/2012EP2458147A2 Gas turbine of the axial flow type
05/30/2012EP2458146A1 Nose cone assembly
05/30/2012EP2456957A1 Method for coating a turbine blade
05/30/2012EP2456665A2 Blade retention system for turboprop
05/30/2012EP2255074B1 Droplet impact protection layer for a blade
05/30/2012CN202250250U Structure for locking moving blade and wheel disc
05/30/2012CN202250249U 1300mm final stage moving blade for full rotary speed steam turbine
05/30/2012CN202250248U 906-type high or low pressure blade of million-kilowatt (KW)-level nuclear steam turbine
05/30/2012CN102483325A 用于型槽的检验设备、检验仪和检验方法 Groove for testing equipment, testing instruments and testing methods
05/30/2012CN102483072A Compressor blade for an axial compressor
05/30/2012CN102482945A A mounting apparatus
05/30/2012CN102482944A Cooling of a gas turbine component shaped as a rotor disc or as a blade
05/30/2012CN102481668A Automated repair method and system
05/30/2012CN102481660A Turbine rotor for a turbocharger, turbocharger and method for producing a turbine rotor
05/30/2012CN102477959A Method and device for utilizing fluid to drive rotor
05/30/2012CN102477873A Gas turbine of the axial flow type
05/30/2012CN102477872A Axial flow gas turbine
05/30/2012CN102477871A Axial flow gas turbine
05/30/2012CN101761364B Method for generating electricity by using low-pressure saturated steam
05/30/2012CN101617102B Turbine wheel
05/30/2012CN101473107B Platform cooling structure of gas turbine rotor blade
05/30/2012CN101438029B Lamina/disk coattail back shear for reducing lamina/disk stress
05/30/2012CN101092012B Part-holding device
05/29/2012US8186965 Recovery tip turbine blade
05/29/2012US8186963 Airfoil shape for compressor inlet guide vane
05/29/2012US8186959 Turbine moving blade assembly and turbine having the same
05/29/2012US8186953 Multiple piece turbine blade
05/29/2012US8186952 Blade arrangement
05/29/2012US8186940 Ventilation arrangement
05/29/2012CA2681866C Coating material and method of manufacturing same, coating method, and moving blade with shroud
05/24/2012WO2012067743A1 Thermal integration of thermoelectric device
05/24/2012WO2012066158A1 Improved centre rest for rotary seat of wind-turbine blades
05/24/2012WO2012065599A1 Securing means for axially securing a blade root of a turbomachine blade
05/24/2012WO2012065595A1 Rotor blade arrangement for a turbo machine
05/24/2012US20120128504 Rotor section for a rotor of a turbomachine, and rotor blade for a turbomachine
05/24/2012US20120128502 Erosion resistant machine component, method for forming surface layer of machine component, and method for manufacturing steam turbine
05/24/2012US20120128501 Fan blade tips
05/24/2012US20120128500 Turbines
05/24/2012US20120128498 Bladed disk assembly
05/24/2012US20120128497 Turbine engine compressor stator
05/24/2012US20120128486 Centrifugal fan and impeller thereof
05/24/2012US20120128473 Rotating machine
05/24/2012US20120128467 Integrated variable geometry flow restrictor and heat exchanger
05/24/2012US20120126665 Method for influencing, damping, or suppressing mechanical vibrations occurring during operation in a turbomachine blade, a turbomachine blade useful for carrying out the method, and a piezoelectric damping element
05/24/2012US20120124994 Composite Centrifugal Compressor Wheel
05/24/2012DE102011118158A1 Gasturbinenmotor und Schaufel für einen Gasturbinenmotor Gas turbine engine and blade for a gas turbine engine
05/24/2012DE102011055375A1 Turbomaschinenleitschaufel und Verfahren zur Kühlung einer Turbomaschinenleitschaufel Turbomaschinenleitschaufel and method for cooling a Turbomaschinenleitschaufel
05/24/2012DE102011055373A1 Kombinierter Dämpfungs- und Dichtungsstift für Turbinenlaufschaufel und verwandtes Verfahren Combined damping and sealing pin for turbine blade and related method
05/23/2012EP2455588A1 Securing module for axial securing of a blade root of a turbo engine blade
05/23/2012EP2455587A1 Rotor for a turbomachine, corrresponding turbomachine and manufacturing method
05/23/2012EP2455586A1 Rotor for a turbo engine comprising sealing and damping elements
05/23/2012EP2455585A1 Assembly for an axial turbo engine and axial turbo engine
05/23/2012EP2455584A1 Gasturbine comprising cooling control means which are made partially of Shape Memory Materials (SMM)
05/23/2012EP2454470A1 Method of applying abrasion resistant materials to rotors
05/23/2012EP2454451A2 Coupling element for mechanically coupling blades and a rotor
05/23/2012EP2238314B1 Arrangement for axially securing blades in a rotor of a gas turbine
05/23/2012EP1512837B1 Turbine blade arrangement
05/23/2012CN202228132U Turbine in turbocharger for vehicle
05/23/2012CN102472295A Hub for a propeller having variable pitch blades
05/23/2012CN102472294A 螺旋桨桨毂 Propeller hub
05/23/2012CN102472114A Multi-stage radial turbine
05/23/2012CN102472109A Turbine and turbine rotor blade
05/23/2012CN102472108A Vibration-damping shim for fan blade
05/23/2012CN102471893A 耐冲蚀性机械部件、机械部件的表面层形成方法以及蒸汽涡轮的制造方法 Resistance to erosion of mechanical parts, mechanical parts of the surface layer forming method and a method of manufacturing a steam turbine
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