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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08/25/2005 | DE102004006706A1 Damping arrangement for vanes, especially for vanes of a gas turbine or aircraft engine, comprises a spring element in the form of a leaf spring arranged between an inner shroud of the vanes and a seal support |
08/25/2005 | DE102004006154A1 Verfahren zum Verbinden von Bauteilen The method for joining components |
08/25/2005 | CA2555578A1 Damping arrangement for guide vanes |
08/24/2005 | EP1566531A1 Gas turbine with compressor casing protected against cooling and Method to operate a gas turbine |
08/24/2005 | EP1566520A2 Use of biased fabric to improve properties of SiC/SiC ceramic composites for turbine engine components |
08/24/2005 | EP1566519A1 High temperature resisting component for a fluidic machine and fluidic machine using this component. |
08/24/2005 | EP1565655A1 Compressor impeller |
08/24/2005 | EP1507957B1 Coolable component and method for the production of a through-opening in a coolable component |
08/24/2005 | CN1659361A Turbine moving blade |
08/23/2005 | US6933061 forming an inner layer overlaying the metal substrate, of a ceramic thermal barrier coating material, covering it with a thermally glazable coating material with high melting point, and melting with a laser beam to form protective coating |
08/23/2005 | US6933060 Thermal barrier coating resistant to sintering |
08/23/2005 | US6933052 Diffusion barrier and protective coating for turbine engine component and method for forming |
08/23/2005 | US6932898 Electrochemical process for the simultaneous stripping of diverse coatings from a metal substrate |
08/23/2005 | US6932577 Turbine blade airfoil having improved creep capability |
08/23/2005 | US6932576 Quick connect ceiling fan blade |
08/23/2005 | US6932575 Blade damper |
08/23/2005 | US6932573 Turbine blade having a vortex forming cooling system for a trailing edge |
08/23/2005 | US6932572 Film cooled article with improved temperature tolerance |
08/23/2005 | US6932571 Microcircuit cooling for a turbine blade tip |
08/23/2005 | US6932570 Methods and apparatus for extending gas turbine engine airfoils useful life |
08/23/2005 | US6932568 Turbine nozzle segment cantilevered mount |
08/23/2005 | US6932565 Turbine |
08/23/2005 | US6931861 Anti-score plates |
08/23/2005 | CA2381664C Steam tube structure of gas turbine |
08/18/2005 | WO2005075140A1 Method for connecting components |
08/18/2005 | WO2005075136A1 Repair soldering method for repairing a component comprising a base material with an oriented microstructure |
08/18/2005 | WO2005074469A2 Mitigation of unsteady peak fan blade and disc stresses in turbofan engines |
08/18/2005 | US20050182576 Methods of measuring steam turbine efficiency |
08/18/2005 | US20050181231 Method for refurbishing surfaces subjected to high compression contact |
08/18/2005 | US20050181222 Component comprising a masking layer |
08/18/2005 | US20050180852 Reduction of co-efficient of friction to reduce stress ratio in bearings and gas turbine parts |
08/18/2005 | US20050180847 Rotor |
08/18/2005 | US20050178750 Repair of article by laser cladding |
08/18/2005 | US20050178126 Combustor member and method for making a combustor assembly |
08/18/2005 | DE102004009696B3 Turbine blade profile for an axial turbine comprises an inner curve formed between a front edge and a rear edge, and an outer curve producing a negative pressure |
08/18/2005 | CA2555155A1 Method for connecting components |
08/17/2005 | EP1564495A1 Combustor member and method for making a combustor assembly |
08/17/2005 | EP1564378A2 Fir-tree and broach slot forms for turbine stage 3 buckets and rotor wheels |
08/17/2005 | EP1564377A2 Rotor blade and rotor disc for a gas turbine engine with a reduced coefficient of friction at the blade and disc interface |
08/17/2005 | EP1564376A2 Turbomachine rotor construction |
08/17/2005 | EP1564375A2 Cooled rotor blade with vibration damping device |
08/17/2005 | EP1564374A1 Turbine blade for a turbomachine |
08/17/2005 | EP1564373A1 Tubular vortex reducer |
08/17/2005 | EP1564372A1 Balancing device for a turbine disk rotor |
08/17/2005 | EP1564371A2 Method of repair for cast article |
08/17/2005 | EP1563945A2 Repair of article by laser cladding |
08/17/2005 | EP1563937A2 Method for refurbishing surfaces subjected to high compression contact |
08/17/2005 | EP1563167A2 Self-regulating turbine |
08/17/2005 | CN1656303A Axial securing means for impeller blades |
08/17/2005 | CN1654806A Turbojet having two counter-rotatable fans |
08/17/2005 | CN1654787A Advanced firtree and broach slot forms for turbine stage 3 buckets and rotor wheels |
08/17/2005 | CN1654786A Firtree and broach slot forms for turbine stage 1 and 2 buckets and rotor wheels |
08/17/2005 | CN1654785A Shroud honeycomb cutter |
08/17/2005 | CN1654784A Tailored turbulation for turbine blades |
08/17/2005 | CN1654783A Turbulent hole structure for turbine blades |
08/17/2005 | CN1215289C Transverse-flow fan and air conditioner using same |
08/16/2005 | US6930066 Highly defective oxides as sinter resistant thermal barrier coating |
08/16/2005 | US6929852 Protective overlayer for ceramics |
08/16/2005 | US6929825 Method for aluminide coating of gas turbine engine blade |
08/16/2005 | US6929453 Locking spacer assembly for slotted turbine component |
08/16/2005 | US6929451 Cooled rotor blade with vibration damping device |
08/16/2005 | US6929446 Counterbalanced flow turbine nozzle |
08/16/2005 | US6929445 Split flow turbine nozzle |
08/16/2005 | CA2366717C Division wall and shroud of gas turbine |
08/13/2005 | CA2487476A1 Cooled rotor blade with vibration damping device |
08/11/2005 | WO2005073560A1 A vortical flow rotor |
08/11/2005 | WO2005073517A1 Turbine machine |
08/11/2005 | WO2005073516A1 Gas turbine engine including airfoils having an improved airfoil film cooling configuration and method therefor |
08/11/2005 | WO2005073515A1 Disk material |
08/11/2005 | US20050175477 Turbocharger |
08/11/2005 | US20050175463 Control of leak zone under blade platform |
08/11/2005 | US20050175462 Advanced firtree and broach slot forms for turbine stage 1 and 2 buckets and rotor wheels |
08/11/2005 | US20050175461 Advanced firtree and broach slot forms for turbine stage 3 buckets and rotor wheels |
08/11/2005 | US20050175459 System for retaining an annular plate against a radial face of a disk |
08/11/2005 | US20050175454 Turbulated hole configurations for turbine blades |
08/11/2005 | US20050175453 Shroud honeycomb cutter |
08/11/2005 | US20050175452 Tailored turbulation for turbine blades |
08/11/2005 | US20050175447 Compressor airfoils with movable tips |
08/11/2005 | US20050175444 Cooling system for an airfoil vane |
08/11/2005 | US20050173496 Method of build up welding to thin-walled portion |
08/11/2005 | US20050173494 Method and apparatus for rebuilding gas turbine engines |
08/11/2005 | US20050172642 Gas turbine with stator shround in the cavity beneath the chamber |
08/11/2005 | US20050172640 Tube-type vortex reducer |
08/11/2005 | US20050172634 Gas turbine and associated cooling method |
08/11/2005 | US20050172610 Turbojet having two counter-rotatable fans secured to a counter-rotatable low-pressure compressor |
08/11/2005 | US20050172609 Turbojet having a large bypass ratio |
08/11/2005 | US20050172607 Exhaust diffuser for axial-flow turbine |
08/11/2005 | US20050172485 Method of repair for cast article |
08/11/2005 | DE102004002965A1 Verfahren und Vorrichtung zur Reparatur von integral beschaufelten Rotoren Method and apparatus for repair of integrally bladed rotors |
08/11/2005 | CA2495598A1 Jet turbine engine with two counter-rotating fans attached to a counter-rotating low pressure compressor |
08/10/2005 | EP1561906A2 Variable vane arm with dual retention capability |
08/10/2005 | EP1561905A1 Plastically deformable layer in the mounting area of a turbine blade and method of turbine blade attachment |
08/10/2005 | EP1561904A2 Honeycomb cutting device for a blade shroud |
08/10/2005 | EP1561903A2 Tailored turbulation for turbine blades |
08/10/2005 | EP1561902A2 Turbine blade comprising turbulation promotion devices |
08/10/2005 | EP1561901A2 Vibration damping device for cooled blades in a turbine rotor |
08/10/2005 | EP1561900A2 Circuit for cooling the platform of a turbine blade |
08/10/2005 | EP1561831A2 Castable high temperature aluminium alloy |
08/10/2005 | EP1561542A1 Process of removing of component layer |
08/10/2005 | EP1561536A1 Process of brazing repairing of a part having a base material with oriented microstructure |