Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
08/2005
08/25/2005DE102004006706A1 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
08/25/2005DE102004006154A1 Verfahren zum Verbinden von Bauteilen The method for joining components
08/25/2005CA2555578A1 Damping arrangement for guide vanes
08/24/2005EP1566531A1 Gas turbine with compressor casing protected against cooling and Method to operate a gas turbine
08/24/2005EP1566520A2 Use of biased fabric to improve properties of SiC/SiC ceramic composites for turbine engine components
08/24/2005EP1566519A1 High temperature resisting component for a fluidic machine and fluidic machine using this component.
08/24/2005EP1565655A1 Compressor impeller
08/24/2005EP1507957B1 Coolable component and method for the production of a through-opening in a coolable component
08/24/2005CN1659361A Turbine moving blade
08/23/2005US6933061 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
08/23/2005US6933060 Thermal barrier coating resistant to sintering
08/23/2005US6933052 Diffusion barrier and protective coating for turbine engine component and method for forming
08/23/2005US6932898 Electrochemical process for the simultaneous stripping of diverse coatings from a metal substrate
08/23/2005US6932577 Turbine blade airfoil having improved creep capability
08/23/2005US6932576 Quick connect ceiling fan blade
08/23/2005US6932575 Blade damper
08/23/2005US6932573 Turbine blade having a vortex forming cooling system for a trailing edge
08/23/2005US6932572 Film cooled article with improved temperature tolerance
08/23/2005US6932571 Microcircuit cooling for a turbine blade tip
08/23/2005US6932570 Methods and apparatus for extending gas turbine engine airfoils useful life
08/23/2005US6932568 Turbine nozzle segment cantilevered mount
08/23/2005US6932565 Turbine
08/23/2005US6931861 Anti-score plates
08/23/2005CA2381664C Steam tube structure of gas turbine
08/18/2005WO2005075140A1 Method for connecting components
08/18/2005WO2005075136A1 Repair soldering method for repairing a component comprising a base material with an oriented microstructure
08/18/2005WO2005074469A2 Mitigation of unsteady peak fan blade and disc stresses in turbofan engines
08/18/2005US20050182576 Methods of measuring steam turbine efficiency
08/18/2005US20050181231 Method for refurbishing surfaces subjected to high compression contact
08/18/2005US20050181222 Component comprising a masking layer
08/18/2005US20050180852 Reduction of co-efficient of friction to reduce stress ratio in bearings and gas turbine parts
08/18/2005US20050180847 Rotor
08/18/2005US20050178750 Repair of article by laser cladding
08/18/2005US20050178126 Combustor member and method for making a combustor assembly
08/18/2005DE102004009696B3 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
08/18/2005CA2555155A1 Method for connecting components
08/17/2005EP1564495A1 Combustor member and method for making a combustor assembly
08/17/2005EP1564378A2 Fir-tree and broach slot forms for turbine stage 3 buckets and rotor wheels
08/17/2005EP1564377A2 Rotor blade and rotor disc for a gas turbine engine with a reduced coefficient of friction at the blade and disc interface
08/17/2005EP1564376A2 Turbomachine rotor construction
08/17/2005EP1564375A2 Cooled rotor blade with vibration damping device
08/17/2005EP1564374A1 Turbine blade for a turbomachine
08/17/2005EP1564373A1 Tubular vortex reducer
08/17/2005EP1564372A1 Balancing device for a turbine disk rotor
08/17/2005EP1564371A2 Method of repair for cast article
08/17/2005EP1563945A2 Repair of article by laser cladding
08/17/2005EP1563937A2 Method for refurbishing surfaces subjected to high compression contact
08/17/2005EP1563167A2 Self-regulating turbine
08/17/2005CN1656303A Axial securing means for impeller blades
08/17/2005CN1654806A Turbojet having two counter-rotatable fans
08/17/2005CN1654787A Advanced firtree and broach slot forms for turbine stage 3 buckets and rotor wheels
08/17/2005CN1654786A Firtree and broach slot forms for turbine stage 1 and 2 buckets and rotor wheels
08/17/2005CN1654785A Shroud honeycomb cutter
08/17/2005CN1654784A Tailored turbulation for turbine blades
08/17/2005CN1654783A Turbulent hole structure for turbine blades
08/17/2005CN1215289C Transverse-flow fan and air conditioner using same
08/16/2005US6930066 Highly defective oxides as sinter resistant thermal barrier coating
08/16/2005US6929852 Protective overlayer for ceramics
08/16/2005US6929825 Method for aluminide coating of gas turbine engine blade
08/16/2005US6929453 Locking spacer assembly for slotted turbine component
08/16/2005US6929451 Cooled rotor blade with vibration damping device
08/16/2005US6929446 Counterbalanced flow turbine nozzle
08/16/2005US6929445 Split flow turbine nozzle
08/16/2005CA2366717C Division wall and shroud of gas turbine
08/13/2005CA2487476A1 Cooled rotor blade with vibration damping device
08/11/2005WO2005073560A1 A vortical flow rotor
08/11/2005WO2005073517A1 Turbine machine
08/11/2005WO2005073516A1 Gas turbine engine including airfoils having an improved airfoil film cooling configuration and method therefor
08/11/2005WO2005073515A1 Disk material
08/11/2005US20050175477 Turbocharger
08/11/2005US20050175463 Control of leak zone under blade platform
08/11/2005US20050175462 Advanced firtree and broach slot forms for turbine stage 1 and 2 buckets and rotor wheels
08/11/2005US20050175461 Advanced firtree and broach slot forms for turbine stage 3 buckets and rotor wheels
08/11/2005US20050175459 System for retaining an annular plate against a radial face of a disk
08/11/2005US20050175454 Turbulated hole configurations for turbine blades
08/11/2005US20050175453 Shroud honeycomb cutter
08/11/2005US20050175452 Tailored turbulation for turbine blades
08/11/2005US20050175447 Compressor airfoils with movable tips
08/11/2005US20050175444 Cooling system for an airfoil vane
08/11/2005US20050173496 Method of build up welding to thin-walled portion
08/11/2005US20050173494 Method and apparatus for rebuilding gas turbine engines
08/11/2005US20050172642 Gas turbine with stator shround in the cavity beneath the chamber
08/11/2005US20050172640 Tube-type vortex reducer
08/11/2005US20050172634 Gas turbine and associated cooling method
08/11/2005US20050172610 Turbojet having two counter-rotatable fans secured to a counter-rotatable low-pressure compressor
08/11/2005US20050172609 Turbojet having a large bypass ratio
08/11/2005US20050172607 Exhaust diffuser for axial-flow turbine
08/11/2005US20050172485 Method of repair for cast article
08/11/2005DE102004002965A1 Verfahren und Vorrichtung zur Reparatur von integral beschaufelten Rotoren Method and apparatus for repair of integrally bladed rotors
08/11/2005CA2495598A1 Jet turbine engine with two counter-rotating fans attached to a counter-rotating low pressure compressor
08/10/2005EP1561906A2 Variable vane arm with dual retention capability
08/10/2005EP1561905A1 Plastically deformable layer in the mounting area of a turbine blade and method of turbine blade attachment
08/10/2005EP1561904A2 Honeycomb cutting device for a blade shroud
08/10/2005EP1561903A2 Tailored turbulation for turbine blades
08/10/2005EP1561902A2 Turbine blade comprising turbulation promotion devices
08/10/2005EP1561901A2 Vibration damping device for cooled blades in a turbine rotor
08/10/2005EP1561900A2 Circuit for cooling the platform of a turbine blade
08/10/2005EP1561831A2 Castable high temperature aluminium alloy
08/10/2005EP1561542A1 Process of removing of component layer
08/10/2005EP1561536A1 Process of brazing repairing of a part having a base material with oriented microstructure