Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
10/2005
10/26/2005EP1212516B1 Hydraulic seal for rotary pumps
10/26/2005CN1688749A Method for removing a layer area of a component
10/25/2005US6958084 with solid lubricant; bearings; specified tin content which acts as a powder pressing aid, a die and powder particle lubricant, enables higher green densities and hence strengths to be achieved at any given pressing pressure
10/25/2005US6957949 Internal cooling circuit for gas turbine bucket
10/25/2005US6957948 Turbine blade attachment lightening holes
10/25/2005CA2354818C Turbocharger rotor with alignment couplings
10/25/2005CA2130068C Process for repairing damaged blades of turboengines
10/20/2005WO2005098204A1 Blade fixing system for a compressor or a turbine
10/20/2005WO2005098203A1 Method for the protection of openings in a component during a machining process
10/20/2005WO2005083269A3 Turbocharger compressor wheel having a counterbore treated for enhanced endurance to stress-induced fatigue and configurable to provide a compact axial length
10/20/2005WO2005045089A3 Component anti-oxidation coating for such a component and corresponding production method
10/20/2005US20050233654 Rotatable lifting surface device having selected pitch distribution and camber profile
10/20/2005US20050232780 Turbine blisk
10/20/2005US20050232778 Blade shape creation program and method
10/20/2005US20050232777 Compressor blade with dovetail slotted to reduce stress on the airfoil leading edge
10/20/2005US20050232775 Device for fixing a rotor on a shaft
10/20/2005US20050232774 Turbine engine rotor retainer
10/20/2005US20050232773 Turbine engine disk spacers
10/20/2005US20050232772 Rotating seal arrangement for turbine bucket cooling circuits
10/20/2005US20050232771 Turbine rotor blades
10/20/2005US20050232770 Flow control arrangement
10/20/2005US20050232769 Thermal shield turbine airfoil
10/20/2005US20050232768 Teardrop film cooled blade
10/20/2005US20050232767 Template for inspecting and marking repair areas on an object
10/20/2005US20050232765 Axial flow fan
10/20/2005US20050232760 Securing assembly
10/20/2005US20050232752 Turbine shroud cooling system
10/20/2005US20050232751 Cooling arrangement
10/20/2005US20050231052 Apparatus and method of balancing a shaft
10/20/2005US20050229601 Gas Turbine Engine Cooling System and Method
10/20/2005CA2503659A1 Process for introducing voluntary detuning on a bladed wheel of a turbine engine. bladed wheelwith voluntary detuning
10/19/2005EP1586740A2 Turbine blisk
10/19/2005EP1586739A2 Thermal shield for a gas turbine airfoil
10/19/2005EP1586738A2 Method and apparatus for reducing turbine blade temperatures
10/19/2005EP1586669A1 Oxidation resistant superalloy and article
10/19/2005EP1373685B1 Gas turbine blade
10/19/2005EP1238185B1 A single or multi-bladed rotor
10/19/2005CN2735009Y Last stage blade for large-scale impulse steam turbine
10/19/2005CN2735008Y Last stage blade for large-scale steam turbine
10/19/2005CN1685160A 压缩机叶轮 Compressor impeller
10/19/2005CN1683750A Repairing tenons on turbine buckets
10/18/2005US6955525 Cooling system for an outer wall of a turbine blade
10/18/2005US6955523 Cooling system for a turbine vane
10/18/2005US6955522 Method and apparatus for cooling an airfoil
10/18/2005CA2172071C Protective coating
10/18/2005CA2130628C Steam turbine blade
10/15/2005CA2502810A1 Turbine shroud cooling system
10/15/2005CA2495926A1 Thermal shield turbine airfoil
10/13/2005WO2005095762A1 Rotor blade, particularly for a gas turbine
10/13/2005WO2005095761A1 Device for supplying cooling air to a moving blade
10/13/2005US20050227078 providing an airfoil substrate having an airfoil substrate surface, and depositing a diamond-like coating (DLC) directly on the airfoil substrate surface
10/13/2005US20050226730 Rotor for a turbomachine
10/13/2005US20050226729 Locking device for turbine blades
10/13/2005US20050226728 Device for balancing a rotating part, in particular a turbojet rotor
10/13/2005US20050226726 Cascade impingement cooled airfoil
10/13/2005US20050226725 Blade cooling
10/13/2005US20050226720 Contra rotatable turbine system
10/13/2005US20050226718 Variable turbine geometry turbocharger
10/13/2005US20050224144 Monocrystalline alloys with controlled partitioning
10/13/2005US20050223708 Gas turbine and manufacturing process of gas turbine
10/13/2005DE102004015301A1 Laufschaufel insbesondere für eine Gasturbine Rotor blade in particular for a gas turbine
10/13/2005DE102004014118A1 Anordnung zur Abdichtung eines Übergangs zwischen Kühlpassagen zweier Komponenten einer Turbomaschine Arrangement for sealing a transition between cooling passages of two components of a turbomachine
10/13/2005DE102004014117A1 Komponente einer Turbomaschine mit einer Kühlanordnung Component of a turbo engine with a cooling arrangement
10/12/2005EP1584796A2 Variable geometry turbine
10/12/2005EP1584795A2 High efficiency stator for the first phase of a gas turbine
10/12/2005EP1584794A1 Axial retention device for the blades in a disk of a turbomachine rotor
10/12/2005EP1584793A2 Turbine blade retaining system
10/12/2005EP1584792A1 Blade attachment for a compressor or a turbine
10/12/2005EP1584791A1 Turbo-machine and rotor therefor
10/12/2005EP1584790A2 Impingement cooled turbine airfoil
10/12/2005EP1584789A1 Coolable airfoil
10/12/2005EP1584788A2 High efficiency rotor for a gas turbine
10/12/2005EP1584787A2 High efficiency rotor for the first phase of a gas turbine
10/12/2005EP1584786A2 High efficiency stator for the second phase of a gas turbine
10/12/2005EP1584785A1 Balancing weight for a rotor, especially for a rotor of a jet engine
10/12/2005EP1584784A1 Assembly device for annular flanges, in particular in turbomachines
10/12/2005EP1584702A1 Deposition repair of hollow items
10/12/2005EP1584402A2 Welding process
10/12/2005EP1412547B1 Sintered tin-containing cobalt-based alloys
10/12/2005CN1682013A Method for testing a component in a non-destructive manner and for producing a gas turbine blade
10/12/2005CN1682012A Gas turbine pressurizing air supply system
10/12/2005CN1680683A 可变几何结构透平 The variable geometry turbine
10/12/2005CN1680611A Oxidation resistant superalloy and article
10/12/2005CN1680068A Deposition repair of hollow items
10/12/2005CN1222684C Steam turbine and blades thereof
10/12/2005CN1222683C Nozzle of steam turbine
10/11/2005US6953533 Process for removing chromide coatings from metal substrates, and related compositions
10/11/2005CA2481812C Shaft structure and bearing structure for tail end of rotor of gas turbine
10/11/2005CA2367570C Split ring for gas turbine casing
10/09/2005CA2502796A1 High efficiency rotor for the first phase of a gas turbine
10/09/2005CA2502793A1 High efficiency rotor for the second phase of a gas turbine
10/09/2005CA2502788A1 High efficiency stator for the second phase of a gas turbine
10/06/2005WO2005093220A1 Method and device for identifying the state of the rotor of a non-positive-displacement machine
10/06/2005WO2005093219A1 Non-positive-displacement machine and rotor for a non-positive-displacement machine
10/06/2005WO2005093218A1 Welded turbine shaft and method for producing said shaft
10/06/2005WO2005093128A1 Cold gas-dynamic spray repair on gas turbine engine components
10/06/2005US20050220995 Cold gas-dynamic spraying of wear resistant alloys on turbine blades
10/06/2005US20050220627 Tip sealing for a turbine rotor blade
10/06/2005US20050220626 Impingement cooling of gas turbine blades or vanes
10/06/2005US20050220625 Transonic blade profiles