Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
08/2008
08/13/2008CN100410404C Precipitation reinforced Ni-Fe-Cr alloy and its production method
08/12/2008US7410701 E.g., for steam turbines; spray coating having a porosity of 6% to 30% covered by a fluorocarbon resin layer and an inorganic material
08/12/2008US7410342 Airfoil support
08/12/2008US7410173 Hydrodynamic brush seal
08/12/2008US7410089 Method of making aerofoil blisks
08/12/2008CA2468134C Device for supplying secondary air in a gas turbine engine
08/07/2008WO2008094972A2 Inspection tool for measuring bucket z notch position
08/07/2008WO2008094221A1 Method of repairing a stationary airfoil array directing three-dimensional flow
08/07/2008WO2008092725A1 Turbine bucket
08/07/2008WO2008046556B1 Turbocharger
08/07/2008US20080187442 Rotor blade trailing edge assembly and method of use
08/07/2008US20080187441 Fan blade made of a textile composite material
08/07/2008DE102007005384A1 Strömungsarbeitsmaschine sowie Rotorschaufel einer Strömungsarbeitsmaschine Flow machine and rotor blade of a turbomachine
08/07/2008DE102007005010A1 Exhaust-gas turbine for turbocharger, has rotor blades arranged in outer circumference of rotatably supported turbine disk, and thermal insulation arranged between inner circumferential surface of guide ring and hollow space
08/06/2008EP1953345A1 Blade ring for a turbo engine
08/06/2008EP1953344A1 Turbine blade
08/06/2008EP1953343A2 Cooling system for a gas turbine blade and corresponding gas turbine blade
08/06/2008EP1953342A1 Turbine blade
08/06/2008EP1953341A2 Turbomachine blade and method of design
08/06/2008EP1953340A2 Flow machine and rotor shovel for a flow machine
08/06/2008EP1953339A1 Method for repairing a turbine rotor disk
08/06/2008EP1953268A1 Thermal barrier coatings with low thermal conductivity comprising lanthanide sesquioxides
08/06/2008EP1953267A1 Thermal barrier coatings with low thermal conductivity comprising lanthanide sesquioxides
08/06/2008EP1953263A2 Method of treating a component of a gas turbine engine
08/06/2008EP1953253A1 Metal alloy compositions and articles comprising the same
08/06/2008EP1952931A1 Mechtrode with powder feed and method for utilising such mechtrode
08/06/2008EP1952917A2 A method of manufacturing a component by consolidating powder material
08/06/2008EP1952911A1 Turbine blade, casting core and method
08/06/2008EP1951992A1 Blade of a turbomachine
08/06/2008EP1951991A1 Turbine blade for a steam turbine
08/06/2008EP1951990A1 Method of repairing a shroud segment of a gas turbine
08/06/2008EP1807674B1 Method for determining the wall thickness of a hollow component
08/06/2008EP1497476B1 Process of masking cooling holes of a gas turbine component
08/06/2008CN101235728A Impingement cooled bucket shroud, turbine rotor incorporating the same, and cooling method
08/06/2008CN100408812C Cooled blade for a gas turbine
08/06/2008CN100408811C Gas turbine engine air baffle for rotary cavity
08/06/2008CN100408726C High temp-resistant article and its manufacturing method
08/05/2008US7407365 Cooling arrangement
07/2008
07/31/2008US20080181784 Convectively cooled gas turbine blade
07/31/2008US20080181780 Airfoil for axial-flow compressor capable of lowering loss in low Reynolds number region
07/31/2008US20080181778 Locking and fixing device for a heat shield element for a rotor unit of a turbomachine
07/31/2008US20080181775 Integrated leading edge for wind turbine blade
07/31/2008US20080181774 Blades, casting cores, and methods
07/31/2008US20080181769 Tone noise reduction in turbomachines
07/31/2008US20080181768 Axial rotor section for a rotor of a turbine
07/31/2008US20080178953 Rotary valve assembly
07/31/2008US20080178593 Compressor wheel for a turbocharger system
07/31/2008DE102008005943A1 Guide blade sealing device for gas turbo group, has compressor and turbine guide blades and axially limiting hot spot segments, which are connected among each other in gas-tight manner using temperature-resistant skeletal laminations
07/31/2008DE102007003027A1 Repaired component i.e. gas turbine component, vibration testing method, involves recording measured values during vibration simulation, and comparing measured values with reference measured values of section detached from new part
07/31/2008DE102007002518B3 Vane for e.g. water turbine, of ship machine, has blowing medium formed between cover and carrying structure, where measures are met to enable transfer of blowing medium from side of vane blade to other side of blade
07/30/2008EP1950383A1 Noise attenuation features for the casing of a turbo fan engine
07/30/2008EP1950381A1 Rotor disc for turbomachine fan
07/30/2008EP1950380A1 Turbine blade
07/30/2008EP1950379A1 Method for modular balancing of a turbomachine rotor
07/30/2008EP1950378A1 Turbocharger rotor
07/30/2008EP1950320A1 Method for restoring or regenerating an article and restored regenerated article
07/30/2008EP1949056A2 Substrate with a coating and its production process
07/30/2008EP1948907A1 Workpiece, and welding method for producing a workpiece
07/30/2008CN201092868Y Dedusting desalination injection mechanism for turbine rotor vane
07/30/2008CN101233299A Gas turbine blade and platform element for a gas turbine blade ring, supporting structure for securing gas turbine blades, gas turbine blade ring and the use of a gas turbine blade ring
07/30/2008CN101233298A Cooled turbine blade for a gas turbine and use of such a turbine blade
07/30/2008CN101233045A Rotor hub fairing system for a counter-rotating, coaxial rotor system
07/30/2008CN101230789A Turbo-propeller comprising a propeller formed by blades with adjustable orientation
07/30/2008CN100406685C Steam turbine and its cooling method and steam turbine plant
07/30/2008CN100406683C Recirculation structure for a turbocompressor
07/30/2008CN100406682C Buckling of blade pad
07/30/2008CN100406681C Turbine bucket tip shroud edge profile
07/30/2008CN100406680C Conical tip shroud fillet for a turbine bucket
07/30/2008CN100406679C Counterstagger compressor airfoil
07/30/2008CN100406678C Method and equipment for assembling rotary machine
07/29/2008US7404986 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
07/29/2008US7404700 Turbine airfoil with fibrous reinforced TBC
07/29/2008US7404699 Turbomachine
07/29/2008CA2419018C High-temperature member for use in gas turbine
07/29/2008CA2351322C Method and apparatus for production of a cast component
07/26/2008CA2619927A1 Turboprop engine with adjustable pitch propeller
07/24/2008WO2008054340A3 Multilayered erosion resistant coating for gas turbines
07/24/2008WO2008032215A3 Power recovery machine
07/24/2008US20080175716 Moving blade for a turbomachine
07/24/2008US20080175714 Dual cut-back trailing edge for airfoils
07/24/2008US20080175712 Steam turbine rotor blade
07/24/2008US20080175711 Pitch controlled wind turbine blade, a wind turbine and use thereof
07/24/2008US20080175709 High Efficiency Turbine with Variable Attack Angle Foils
07/23/2008EP1947349A1 Safety mechanism and bearing element
07/23/2008EP1947296A2 Turbine blade with reserve cooling air film hole direction
07/23/2008EP1947295A1 Vane plug of an axial turbine vane
07/23/2008EP1947294A2 Airfoil with device against boundary layer separation
07/23/2008EP1947293A1 Guide vane for a gas turbine
07/23/2008EP1946868A1 Directional solidification method and apparatus
07/23/2008EP1945931A2 Device and method for axially displacing a turbine rotor
07/23/2008EP1945913A1 A superplastically formed blade for a turbine engine and a corresponding manufacturing method therefor
07/23/2008EP1945912A2 Multistage compressor for a gas turbine, comprising discharge ports and injection ports to stabilize the compressor flow
07/23/2008CN101225753A Method and apparatus for coating gas turbine engine
07/23/2008CN101225752A Turbine blade
07/23/2008CN101225751A Compressed air engine
07/23/2008CN101225750A Energy converter
07/23/2008CN101225519A Method for restoring or regenerating an article and restored regenerated article
07/23/2008CN100404880C Quick connect ceiling fan blade
07/23/2008CN100404818C Apparatus to reduce seal rubbing within gas turbine engines
07/23/2008CN100404816C Methods and apparatus for cooling gas turbine engine rotor assemblies