Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
02/2005
02/08/2005CA2067406C Turbine blade assembly
02/07/2005CA2478750A1 Thermal barrier compound, superalloy mechanical part coated with such a compound, ceramic coating, and process for manufacturing the said coating
02/07/2005CA2476014A1 Alloys for high temperature applications, articles made therefrom, and method for repair of articles
02/03/2005WO2005010323A1 Device for fixing the blade root on a turbomachine
02/03/2005WO2005009920A1 Sintered silicon nitride
02/03/2005WO2004048775A3 Method and apparatus for determining the thermal performance of actively cooled turbine components
02/03/2005US20050025627 Contoured disk bore
02/03/2005US20050025625 Connection between bladed discs on the rotor line of a compressor
02/03/2005US20050025623 Cooling circuits for a gas turbine blade
02/03/2005US20050025622 Blade inlet cooling flow deflector apparatus and method
02/03/2005US20050025618 Airfoil shape for a turbine nozzle
02/03/2005US20050025617 Geothermal turbine
02/03/2005US20050025614 Turbine engine and a method for cooling a turbine engine
02/03/2005US20050025613 Integral turbine composed of a cast single crystal blade ring diffusion bonded to a high strength disk
02/03/2005US20050023249 Non-separating diffuser for holes produced by a two step process
02/03/2005US20050022535 Heat exchanger on a turbine cooling circuit
02/03/2005US20050022529 Steam turbine power plant
02/03/2005US20050022501 Turbofan case and method of making
02/03/2005DE10333304A1 Air-cooled gas turbine compressor blade has partition air passage with thickened blade material around the passage
02/03/2005DE10331635A1 Gekühlte Schaufel für eine Gasturbine Cooled blade for a gas turbine
02/03/2005DE10331599A1 Bauteil für eine Gasturbine sowie Verfahren zur Herstellung desselben Of the same component for a gas turbine and processes for preparing
02/03/2005DE102004029109A1 Francis turbine wheel blades have scalloped trailing edge profile delaying the onset of cavitation
02/03/2005CA2532599A1 Rotor blade tip section
02/02/2005EP1503061A1 Method for cooling hot turbine parts using air partly cooled by an external heat exchanger and correspondingly cooled gas turbine engine
02/02/2005EP1503046A2 Device for separating foreign particles out of the cooling air that can be fed to the rotor blades of a turbine
02/02/2005EP1503044A1 Inter blade platforms with resilient lateral edges
02/02/2005EP1503040A1 Lightweight inter-blade platform for a blade support disk of a turbo engine
02/02/2005EP1503039A1 Fixing inter blade platforms on hub by means of pins
02/02/2005EP1503038A1 Cooling circuit for a turbine blade
02/02/2005EP1503037A2 Airfoil shape for a turbine nozzle
02/02/2005EP1503036A2 Contoured turbine disk bore
02/02/2005EP1502966A2 Steam turbine power plant
02/02/2005EP1502690A2 Non-separating diffuser holes
02/02/2005EP1502008A1 Device for fixing a rotor on a shaft
02/02/2005CN1573089A Francis turbine
02/02/2005CN1573052A Methods and apparatus for supplying cooling fluid to turbine nozzles
02/02/2005CN1573022A Methods and apparatus for designing gas turbine engine rotor assemblies
02/02/2005CN1573021A Airfoil shape for a turbine bucket
02/02/2005CN1573020A Apparatus and methods for coupling axially aligned turbine rotors
02/02/2005CN1573019A Francis turbine
02/02/2005CN1187520C Steam turbine operating method, and turbine device provided with steam turbine that functions according to said method
02/01/2005US6848884 Three-dimensional axial-flow turbine stage
02/01/2005US6848258 Gas transfer energy recovery and effervescence prevention apparatus and method
02/01/2005US6848180 Turbocharger turbine shaft joining method
02/01/2005CA2365090C Gas turbine
02/01/2005CA2316576C A cooling air supply system for a rotor
02/01/2005CA2308847C A gas-turbine rotor
01/2005
01/31/2005CA2475152A1 Fixation pin interblade platform with variable shear constraints for a turbojet blade support disk
01/27/2005WO2005008067A2 Impeller and cutting elements for centrifugal chopper pumps
01/27/2005WO2005008032A1 Lightweight blade for gas turbine and method for making same
01/27/2005WO2005007334A1 Method and device for laser-welding structural parts by means of a wire and inductive preheating
01/27/2005US20050019160 Airfoil shape for a turbine bucker
01/27/2005US20050019157 Axial flow turbine
01/27/2005US20050019152 Recirculation structure for a turbocompressor
01/27/2005US20050016842 Fixture for electro-chemical machining
01/27/2005US20050015983 Slot machining
01/27/2005US20050015980 Repair of combustion turbine components
01/27/2005US20050015964 Foam wall combustor construction
01/27/2005DE10332563A1 Turbinenschaufel mit Prallkühlung Turbine blade with impingement cooling
01/27/2005DE10332561A1 Gekühltes Turbinenlaufrad, insbesondere Hochdruckturbinenlaufrad für ein Flugtriebwerk Cooled turbine impeller, in particular high-pressure turbine rotor for an aircraft engine
01/27/2005DE10329463A1 Turax engine with multiple working principle has combustion chambers opening out symmetrically on both sides into nozzle inlets to bladed rotor wheel of turbine
01/27/2005DE10257044B4 Gasturbine Gas turbine
01/26/2005EP1500880A2 A transpiration cooling system
01/26/2005EP1500787A1 De-icing device for inlet vanes of a turbo engine, the vane using the same de-icing device and the aeronautical engine using such vanes.
01/26/2005EP1500453A1 Slot machining
01/26/2005EP1500444A1 Process for the manufacture of forgings by precision forging
01/26/2005EP1260602A9 Process for producing a thermally insulating coating system on a metallic substrate
01/26/2005CN2674106Y Mixing type turbine rotator
01/26/2005CN1570171A Nickel base heat resistant cast alloy and turbine wheels made thereof
01/25/2005US6847004 Process of removing a ceramic coating deposit in a surface hole of a component
01/25/2005US6846575 Article having turbulation and method of providing turbulation on an article
01/25/2005US6846160 Turbine bucket
01/25/2005US6846159 Chamfered attachment for a bladed rotor
01/25/2005US6846156 Gas turbine
01/20/2005WO2005005785A1 Cooled blade for a gas turbine
01/20/2005WO2005005784A1 Turbine blade
01/20/2005WO2005005783A1 Steam turbine
01/20/2005WO2005005690A1 Method for producing a protective layer, protective layer, use thereof, and part provided with a protective layer
01/20/2005WO2005005688A1 Layer structure and method for producing such a layer structure
01/20/2005WO2004101969A3 Turbo compressor system for an internal combustion engine comprising a compressor of radial type and provided with an impeller with backswept blades
01/20/2005WO2004101968A3 A turbochanger system for internal combustion engine comprising two compressor stages of the radial type provided with compressor wheels having backswept blades
01/20/2005US20050014629 product of silicon nitride, scandium oxide, silicon carbide and scandium disilicate; resistance to corrosion and oxidation resistance; for hot section components of gas turbine engines, such as blades, nozzles, and combustion liners
01/20/2005US20050013994 Thermal barrier coating with stabilized compliant microstructure
01/20/2005US20050013696 Perfected device for securing an engine shaft on a bearing support
01/20/2005US20050013695 Airfoil shape for a turbine bucket
01/20/2005US20050013693 Blade structure in a gas turbine
01/20/2005US20050013692 Turbine bucket tip shroud edge profile
01/20/2005US20050013691 Francis turbine
01/20/2005US20050013686 Turbine vane plate assembly
01/20/2005US20050011863 Method for inspecting a titanium-based component
01/20/2005US20050011192 Surface-reformed exhaust gas guide assembly of vgs type turbo charger, and method surface-reforming component member thereof
01/20/2005US20050011070 Spun metal form used to manufacture dual alloy turbine wheel
01/20/2005DE20221061U1 Laser welded rotor discs for turbines and compressors consist of base rotating body and individually manufactured guide blades which are optimized in their strength values
01/20/2005DE102004029833A1 Nickelbasis-Superlegierung und Einkristall-Gussstücke Nickel-base superalloy and single crystal castings
01/20/2005DE102004004424A1 Aktive Kühltafel aus Thermostruktur-Kompositwerkstoff und Verfahren zur Herstellung selbiger Active cooling panel of thermostructural composite material and method for producing Selbiger
01/19/2005EP1498731A2 Method for inspecting a titanium-base component
01/19/2005EP1498624A1 Device for fixing a motor shaft onto a bearing support
01/19/2005EP1498579A1 Retaining device for mounting a flask onto a rotor
01/19/2005EP1498578A1 Turbine bucket tip shroud edge profile
01/19/2005EP1498577A2 Airfoil shape for a turbine bucket