Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915) |
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04/03/2012 | US8147196 Turbine airfoil with a compliant outer wall |
04/03/2012 | US8147192 Dual stage turbine shroud |
04/03/2012 | US8147188 Air cooled bucket for a turbine |
04/03/2012 | US8147182 Ceiling fan with concentric stationary tube and power-down features |
03/30/2012 | CA2754263A1 Gas turbine blade and method of protecting same |
03/30/2012 | CA2754256A1 Airfoil blade |
03/30/2012 | CA2754254A1 Nanocrystalline metal coated composite airfoil |
03/29/2012 | WO2012040214A1 High efficiency power production methods, assemblies, and systems |
03/29/2012 | WO2012038406A1 Blade arrangement and associated gas turbine |
03/29/2012 | WO2012038217A1 Turbine blade comprising a ceramic anti-erosion layer for a low-pressure stage of a steam turbine |
03/29/2012 | WO2011160061A3 Vortex propeller |
03/29/2012 | US20120076665 Cooled turbine blades for a gas-turbine engine |
03/29/2012 | US20120076662 Turbine engine component having protective coating |
03/29/2012 | US20120076661 Blade for a gas turbine engine |
03/29/2012 | US20120076659 Anti fret liner assembly |
03/29/2012 | US20120076657 Gas turbine engine and main engine rotor assembly and disassembly |
03/29/2012 | US20120076656 Horizontal Axis Logarithmic Spiral Fluid Turbine |
03/29/2012 | US20120076654 Turbine airfoil and method for cooling a turbine airfoil |
03/29/2012 | US20120076653 Turbine blade tip with vortex generators |
03/29/2012 | US20120076645 Endwall component for a turbine stage of a gas turbine engine |
03/29/2012 | DE102011053702A1 Turbinenschaufelblatt und Verfahren zur Kühlung eines Turbinenschaufelblattes Turbine blade and method for cooling a turbine airfoil |
03/29/2012 | DE102011052672A1 Spitzenströmungspfadprofil Peak flow path profile |
03/29/2012 | DE102010046331A1 Gekühlte Turbinenschaufeln für ein Gasturbinentriebwerk Cooled turbine blades for a gas turbine engine |
03/29/2012 | CA2811945A1 High efficiency power production methods, assemblies, and systems |
03/28/2012 | EP2434126A2 Shaft and turbine wheel assembly for a turbocharger |
03/28/2012 | EP2434125A1 Method for producing impeller applied to supercharger |
03/28/2012 | EP2434101A2 A damped assembly |
03/28/2012 | EP2434100A1 Turbine engine apparatus with protective coating |
03/28/2012 | EP2434099A2 Blade for a gas turbine engine |
03/28/2012 | EP2434098A1 Blade assembly and corresponding gas turbine |
03/28/2012 | EP2434097A1 Turbine blade |
03/28/2012 | EP2434096A2 Gas turbine engine airfoil comprising a conduction pedestal |
03/28/2012 | EP2434095A2 Nacelle with porous surfaces |
03/28/2012 | EP2434094A2 Steam turbine stator vane and steam turbine |
03/28/2012 | EP2434093A2 Cooled turbine blades for a gas turbine engine |
03/28/2012 | EP2432972A1 Systems and methods for transporting and assembling segmented wind turbine blades |
03/28/2012 | EP2235328B1 Blade cooling |
03/28/2012 | EP2217792B1 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 |
03/28/2012 | EP1740797B1 Gas turbine |
03/28/2012 | CN202176374U 一种烟气轮机挠性动叶围带 One kind of flexible flue gas turbine bucket shroud |
03/28/2012 | CN202176373U 用于汽轮机叶轮加热的旋转装置 Rotating means for heating the turbine impeller |
03/28/2012 | CN102392703A Double reheat steam turbine |
03/28/2012 | CN102392691A High-precision antioxidant wear-resistant stabilized turbine blade |
03/28/2012 | CN102392690A Rotating device for heating impeller of turbine |
03/28/2012 | CN102392217A Blade surface pitting corrosion resistant coating and preparation method thereof |
03/28/2012 | CN101680306B Blade structure for turbine |
03/28/2012 | CN101178015B System for manufacturing bladed rotor having an mmc ring and an monolithic airfoils |
03/28/2012 | CN101178014B Dual interstage cooled engine |
03/27/2012 | US8142165 Aerofoil |
03/27/2012 | US8142163 Turbine blade with spar and shell |
03/27/2012 | US8142161 Replaceable staking insert |
03/27/2012 | US8142155 Wind turbine generator and method for constructing wind turbine generator |
03/27/2012 | US8142153 Turbine vane with dirt separator |
03/27/2012 | US8142137 Cooled gas turbine vane assembly |
03/27/2012 | US8141879 Seals for a turbine engine, and methods of assembling a turbine engine |
03/27/2012 | CA2504165C Chevron film cooled wall |
03/27/2012 | CA2399552C Iron base high temperature alloy |
03/22/2012 | WO2012037347A1 Method and apparatus for connecting turbine rotors |
03/22/2012 | WO2012036965A1 Turbine component with multi - scale turbulation features |
03/22/2012 | WO2012036850A1 Turbine component cooling channel mesh with intersection chambers |
03/22/2012 | WO2012036068A1 Turbine |
03/22/2012 | WO2012035658A1 Wing arrangement method |
03/22/2012 | WO2012035060A1 Method for treating turbine blades and device therefor |
03/22/2012 | WO2012034906A1 Assembly of a blade and a composite carrier, obtained by sealing |
03/22/2012 | US20120070310 Axial turbomachine rotor having blade cooling |
03/22/2012 | US20120070309 Blade for a gas turbine |
03/22/2012 | US20120070308 Cooled blade for a gas turbine |
03/22/2012 | US20120070307 Turbine blades, turbine assemblies, and methods of manufacturing turbine blades |
03/22/2012 | US20120070306 Turbine component cooling channel mesh with intersection chambers |
03/22/2012 | US20120070305 Shank cavity and cooling hole |
03/22/2012 | US20120070303 Ni-BASED SINGLE CRYSTAL SUPERALLOY AND TURBINE BLADE |
03/22/2012 | US20120070302 Turbine airfoil vane with an impingement insert having a plurality of impingement nozzles |
03/22/2012 | US20120070300 Blade with minimized vulnerability |
03/22/2012 | US20120070299 Wind turbine blade |
03/22/2012 | US20120070298 Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the second stage of a turbine |
03/22/2012 | US20120070297 Aft loaded airfoil |
03/22/2012 | US20120070287 Propeller for an aircraft turbine engine comprising a vane retaining ring mounted about the hub |
03/22/2012 | US20120068464 Hydroelectric in-pipe turbine blades |
03/22/2012 | US20120067063 Rotor assembly for use in turbine engines and methods for assembling same |
03/22/2012 | DE102011112340A1 Gas turbine arrangement has annular seal arrangement, which is provided between stationary component and rotor unit, where annular seal arrangement separates annular space from radial inner cavity |
03/22/2012 | DE102011053531A1 Rotoranordnung zur Verwendung in Turbomaschinen und Verfahren zum Zusammenbau derselben Rotor assembly for use in turbomachinery and method of assembling same |
03/22/2012 | DE102010045851A1 Turbo-machine e.g. turbine stage of gas turbine of aircraft engine, has housing control unit for displacement of housing portions against each other and/or bearing control unit for displacement of housing and rotor shaft against each other |
03/22/2012 | DE102010045713A1 Method for manufacturing or repairing e.g. housing of gas turbine, involves selectively adhering material layer in chemical film when connecting material layer with substrate, where material layer is adhered in form of component |
03/22/2012 | CA2811069A1 Assembly of a blade and a composite carrier, obtained by sealing |
03/21/2012 | EP2431576A1 Method and apparatus for simulation test of centrifugal stress of turbine blade |
03/21/2012 | EP2431573A1 Turbine stator vane and gas turbine |
03/21/2012 | EP2431572A1 Thermal barrier coating for a steam turbine component |
03/21/2012 | EP2431571A1 Assembly of a blade and a composite support by secure fixing |
03/21/2012 | EP2431495A1 A method for forming thermal barrier coating and device with the thermal barrier coating |
03/21/2012 | EP2324205B1 Vibration damper device for turbomachine blade attachments, associated turbomachine and associated engines |
03/21/2012 | EP1838489B1 Method for producing a hole |
03/21/2012 | EP1761708B1 Device and method for detachably connecting an impeller to a shaft |
03/21/2012 | CN1932249B Parasitical wing sealing and selecting stator, rotor and wing sealing mould face method for turbo vane |
03/21/2012 | CN102387908A Method for producing a turbomachine blade made from a composite material |
03/21/2012 | CN102387882A Method for producing a turbine wheel for an exhaust gas turbocharger |
03/21/2012 | CN102383864A Turbine blade assembly |
03/21/2012 | CN102383863A Rotor assembly for use in gas turbine engines and method for assembling the same |
03/21/2012 | CN101272880B Method for mending component |
03/20/2012 | US8137820 Roughened coatings for gas turbine engine components |
03/20/2012 | US8137074 Wind turbine lightning protection system |