Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
11/2005
11/24/2005CA2566584A1 Fan blade curvature distribution for high core pressure ratio fan
11/24/2005CA2566524A1 Bladed disk fixing undercut
11/23/2005EP1598559A1 Automotive compressor
11/23/2005EP1598537A1 Steam turbine body and method of cooling a steam turbine
11/23/2005EP1598524A1 Assembly method for unitary vaned rotors and device for the damping of vane vibrations
11/23/2005EP1598523A1 Wall structure for hollow gas turbine blades to increase the heat transfer
11/23/2005EP1598522A1 Steam turbine components, method for cooling a steam turbine and their use.
11/23/2005EP1598521A1 Exhaust gas turbocharger
11/23/2005EP1598444A1 Process to adjust the electric conductivity of a coating on a machine component by dry ice blasting, the electric conductivity being variable by pressure
11/23/2005EP1598439A2 HVOF bi-layer coating with controlled porosity for use in thermal barrier coatings
11/23/2005EP1598438A1 TI 6-2-4-2 sheet with enhanced cold-formability
11/23/2005EP1480770B1 Method and device for producing precision investment-cast ne metal alloy members
11/23/2005CN1699615A Method for plasma coating a turbine blade and coating device
11/23/2005CN1699614A Ti6-2-4-2 sheet with enhanced cold-formability
11/23/2005CN1699292A Method for forming cove on the metal parts surface and related procedure and parts
11/22/2005US6966758 Wind turbine rotor blade comprising one or more means secured to the blade for changing the profile thereof depending on the atmospheric temperature
11/22/2005US6966756 Turbine bucket cooling passages and internal core for producing the passages
11/22/2005US6966755 Compressor airfoils with movable tips
11/22/2005US6966750 Gas turbine stationary blade
11/22/2005US6966191 Device for supplying secondary air in a gas turbine engine
11/22/2005CA2321375C An arrangement for sealing a steam-cooled gas turbine
11/22/2005CA2198225C Gas turbine blade with cooled platform
11/17/2005WO2005108759A1 Shockwave-induced boundary layer bleed for transonic gas turbine
11/17/2005WO2005108746A1 Non-positive-displacement machine bucket
11/17/2005US20050255648 Silicon based substrate hafnium oxide top environmental/thermal top barrier layer and method for preparing
11/17/2005US20050255333 On zinc or a zinc alloy; free from the presence of silicate, cerium, aluminum, and borate; clear or colorless; multicolor iridescence; chromium index greater than 10
11/17/2005US20050255329 Superalloy article having corrosion resistant coating thereon
11/17/2005US20050254991 Nickel-based alloy for producing components which have solidified in single crystal form
11/17/2005US20050254958 Natural frequency tuning of gas turbine engine blades
11/17/2005US20050254956 Fan blade curvature distribution for high core pressure ratio fan
11/17/2005US20050254955 Friction stir welded hollow airfoils and method therefor
11/17/2005US20050254953 Blade fixing relief mismatch
11/17/2005US20050254952 Bladed disk fixing undercut
11/17/2005US20050254951 Restraining device for fan blade root
11/17/2005US20050254950 Drum, in particular a drum forming a turbomachine rotor, a compressor, and a turboshaft engine including such a drum
11/17/2005US20050254942 Method of joining ceramic parts and articles so formed
11/17/2005US20050254940 Blade arrangement
11/17/2005CA2565867A1 Shockwave-induced boundary layer bleed for transonic gas turbine
11/17/2005CA2565266A1 Fluid flow machine blade
11/16/2005EP1596037A2 Blade arrangement
11/16/2005EP1596036A1 Friction stir welded hollow airfoils and method therefor
11/16/2005EP1595977A2 Superalloy article having corrosion resistant coating thereon
11/16/2005EP1595859A2 Article comprising a substrate comprising silicon and a top barrier layer comprising hafnium oxide
11/16/2005EP1595059A1 Turbine having variable throat
11/16/2005EP1595058A1 Sealing arrangement, particularly for the blade segments of gas turbines
11/16/2005EP1259348B1 Casting system and method for forming highly pure and fine grain metal castings
11/15/2005US6965834 Steam turbine system inspecting method
11/15/2005US6964791 High-temperature articles and method for making
11/15/2005US6964557 Methods and apparatus for coupling a component to a turbine engine blade
11/15/2005CA2292381C Method of removing hot corrosion products from a diffusion aluminide coating
11/15/2005CA2228786C Ventilation system for platforms of moving vanes
11/15/2005CA2196642C Labyrinth disk with built-in stiffener for turbomachine rotor
11/15/2005CA2195040C Cooling device for a turbine disk
11/13/2005CA2504264A1 Silicon based substrate hafnium oxide top environmental/thermal top barrier layer and method for preparing
11/10/2005WO2005106208A1 Blade for a gas turbine
11/10/2005WO2005106207A1 Compressor blade and compressor
11/10/2005WO2005106206A1 Gas turbine blade shroud
11/10/2005WO2005106075A1 Method for application of a protective coating to a thermally-stressed component
11/10/2005WO2005105702A1 Cement-based systems using water retention agents prepared from raw cotton linters
11/10/2005WO2005105701A1 Joint compounds using thickeners prepared from raw cotton linters
11/10/2005WO2005105700A1 Cement-based systems using plastification/extrusion auxiliaries prepared from raw cotton linters
11/10/2005WO2005105699A1 Cement-based plasters using water rentention agents prepared from raw cotton linters
11/10/2005WO2005105698A1 Gypsum-based mortars using water retention agents prepared from raw cotton linters
11/10/2005WO2005105697A1 Tile cement mortars using water retention agents
11/10/2005WO2005105376A1 Polishing method for large-sized part and polishing particles used for the method
11/10/2005WO2005105375A1 Device and method for polishing large part
11/10/2005US20050249977 Comprising zirconia-containing hafnia stabilized by silica, and rare-earth oxides, wherein silica content gradually decreases toward surface of coating material and zirconia content gradually increases toward surface of coating material; erosion protection for non-oxide ceramic-coated gas turbines
11/10/2005US20050249888 Physical vapor deposition is augmented by chemical vapor deposition from one or more organometallic compounds, preferably refractory metal carbonyls, to deposit coatings and repair material on superalloy turbine engine parts
11/10/2005US20050249602 Integrated ceramic/metallic components and methods of making same
11/10/2005US20050249601 Hybrid bucket and related method of pocket design
11/10/2005US20050249599 Turbine and turbine blade
11/10/2005US20050249593 Cooling air evacuation slots of turbine blades
11/10/2005US20050249592 Compressor blade with dovetail slotted to reduce stress on the airfoil leading edge
11/10/2005US20050249590 Turbomachine, for example a turbojet for an airplane
11/10/2005US20050249588 Seal assembly
11/10/2005US20050249586 Method for introducing a deliberate mismatch on a turbomachine bladed wheel, bladed wheel with a deliberate mismatch
11/10/2005US20050249585 Axial-flow type fan having an air outlet blade structure
11/10/2005US20050249583 Cooled turbine airfoil
11/10/2005US20050249580 System for protecting a main shaft of an engine having a fusible bearing
11/10/2005US20050249578 Shockwave-induced boundary layer bleed
11/10/2005US20050247045 High efficiency stator for the second phase of a gas turbine
11/10/2005US20050247044 High efficiency rotor for the second phase of a gas turbine
11/10/2005US20050246894 Method for manufacturing a stator or rotor component
11/10/2005US20050246893 Turbine rotor repair method
11/10/2005US20050246889 Device for assembling annular flanges together, in particular in a turbomachine
11/10/2005DE102005017148A1 Drehdichtungsanordnung für Kühlkreisläufe von Turbinenschaufeln Rotary seal assembly for cooling circuits of turbine blades
11/10/2005DE102005014871A1 Laufschaufelformkonstruktionsprogramm und Verfahren Blade shape design program and procedures
11/10/2005DE102005014017A1 Turbine und Turbinenschaufel Turbine and turbine blade
11/10/2005DE102004019531A1 Verfahren zum Verschließen einer Kernaustrittsöffnung einer Turbinenschaufel und Turbinenschaufel A method for sealing a core orifice of a turbine blade and turbine blade
11/10/2005CA2563774A1 Cement-based systems using water retention agents prepared from raw cotton linters
11/10/2005CA2563773A1 Joint compounds using thickeners prepared from raw cotton linters
11/10/2005CA2563772A1 Cement-based systems using plastification/extrusion auxiliaries prepared from raw cotton linters
11/10/2005CA2563451A1 Gypsum-based mortars using water retention agents prepared from raw cotton linters
11/10/2005CA2562439A1 Cement-based plasters using water rentention agents prepared from raw cotton linters
11/10/2005CA2562279A1 Tile cement mortars using water retention agents
11/09/2005EP1593817A1 Turbomachine provided with a protection system for the main engine shaft with frangible bearing
11/09/2005EP1593812A2 Cooled turbine airfoil
11/09/2005EP1593811A2 Hybrid turbine bucket
11/09/2005EP1593757A1 Integrated ceramic/metallic components and methods of making same
11/09/2005EP1593752A2 Multi-component coating deposition