Patents
Sitemap › F01 - Machines or engines in general; Engine plants in general; Steam engines › F01D - Non-positive-displacement machines or engines, e.g. steam turbines › F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
11/2005
11/09/2005EP1593445A1 Process of making a hollow member having an internal coating
11/09/2005EP1185764B1 Device for controlling air flow in a turbine blade
11/09/2005EP1029153B1 Turbine engine vane assembly and method of repairing the same
11/09/2005CN2739360Y Steam turbine end-stage moving vane
11/09/2005CN2739359Y Large-sized full-speed steam turbine end-stage blade
11/09/2005CN1693687A Nozzle with build-in rib part and assemble of cooling insertion part
11/09/2005CN1693678A Hybrid turbine bucket and correlation method
11/09/2005CN1693677A Manufacturing method of small sized turbine
11/09/2005CN1693676A Manufacturing method of small sized compression impellor
11/09/2005CN1693675A Manufacturing method of small sized turbine shaft
11/09/2005CN1693534A Multi-component coating deposition
11/09/2005CN1693006A Process of making a hollow member having an internal coating
11/08/2005US6963044 Coating apparatus and processes for forming low oxide coatings
11/08/2005US6962484 Moving blade for a turbomachine
11/08/2005CA2363313C Ultrasonic shot-peening process and system for rotor blade attachment centre sockets
11/06/2005CA2504449A1 Integrated ceramic/metallic components and methods of making the same
11/06/2005CA2500503A1 Cooled turbine airfoil
11/03/2005WO2005103452A1 Turbine blade with an impact cooling insert
11/03/2005WO2005103451A1 Method for obturating a core outlet of a turbine bucket and turbine bucket
11/03/2005WO2005103331A1 Hard, ductile coating system
11/03/2005WO2005102831A1 Rotatable lifting surface device having selected pitch distribution and camber profile
11/03/2005US20050244663 Adds the minimum weight while providing the maximum thermal insulation capability; for long life, stability, economy, gas turbines. coated part comprising a thermal barrier coating offering lower thermal conductivity but which exhibits suitable resistance to spallation
11/03/2005US20050244275 Composite shaft
11/03/2005US20050244274 Method for removing aluminide coating from metal substrate and turbine engine part so treated
11/03/2005US20050244272 Rotor balancing device and method
11/03/2005US20050244270 Cooling system for a tip of a turbine blade
11/03/2005US20050244268 Self-regulating turbine
11/03/2005US20050244265 Rotary apparatus for a gas turbine engine
11/03/2005US20050244264 Turbine nozzle trailing edge cooling configuration
11/03/2005US20050242526 Hot gas seal
11/03/2005US20050241797 Method for producing a hollow cast component having an inner coating
11/03/2005US20050241543 Cement-based systems using plastification/extrusion auxiliaries prepared from raw cotton linters
11/03/2005US20050241542 Cement-based systems using water retention agents prepared from raw cotton linters
11/03/2005US20050241541 Gypsum-based mortars using water retention agents prepared from raw cotton linters
11/03/2005US20050241540 Cement-based plasters using water retention agents prepared from raw cotton linters
11/03/2005US20050241539 Tile cement mortars using water retention agents
11/03/2005US20050241288 High efficiency rotor for the first phase of a gas turbine
11/03/2005US20050241287 High efficiency stator for the first phase of a gas turbine
11/03/2005US20050241148 Thermally insulating layer incorporating a distinguishing agent and method for inspecting the same
11/03/2005US20050241147 Method for repairing a cold section component of a gas turbine engine
11/03/2005DE19537549B4 Schaufel- und Radschwalbenschwanzverbindung für Turbinenrotoren Shovel and Radschwalbenschwanzverbindung for turbine rotors
11/03/2005DE112004000100T5 Gekühlte Schaufeln eines Gasturbinentriebwerks -Cooled blades of a gas turbine engine
11/03/2005DE102005016557A1 Method for producing cooling insert for stator blades in gas turbines involves shaping outwardly curved and inwardly curved walls from single plate which is then bent about rear edge and welded along leading edge
11/03/2005DE102005015015A1 Fluidpumpengerät Fluid pumping device
11/03/2005DE102004016977A1 Rotor for turbine has blades secured in anchored position by at least two locking rings preventing movement in either direction
11/02/2005EP1591626A1 Blade for gas turbine
11/02/2005EP1591625A1 Gas turbine blade shroud
11/02/2005EP1591624A1 Compressor blade and compressor.
11/02/2005EP1591623A2 Turbine engine and assembly method for this engine
11/02/2005EP1591622A2 Turbine Engine disk spacers
11/02/2005EP1591561A1 Method for applying a protective coating over a high temperature component
11/02/2005EP1591550A1 Thermal barrier coating having an interfacial layer for spallation life enhancement and low conductivity
11/02/2005EP1591549A1 Method for repairing local damage to a thermal barrier coating of a component
11/02/2005EP1591432A2 Environmental barrier coating for silicon-containing substrates and process therefor
11/02/2005EP1590552A1 Apparatus and method for inspecting and marking damaged areas on a blade
11/02/2005EP1242719A4 Viscous drag impeller components incorporated into pumps, turbines and transmissions
11/02/2005EP1173656B1 High pressure turbine cooling of gas turbine engine
11/02/2005CN1692213A Cambered vane for use in turbochargers
11/02/2005CN1691996A Turbine rotor repair method
11/02/2005CN1690486A Steam turbine rotor temperature control at oil deflector
11/02/2005CN1690448A Fluid pump apparatus
11/02/2005CN1690447A Axial flow fan
11/02/2005CN1690389A Rotating seal arrangement for turbine bucket cooling circuits
11/02/2005CN1690366A Frequency-tuned compressor stator blade and related method
11/02/2005CN1690365A Methods and apparatus for assembling gas turbine engine rotor assemblies
11/02/2005CN1690364A Turbulator on the underside of a turbine blade tip turn and related method
11/02/2005CN1689800A Thin 7YSZ, interfacial layer as cyclic durability (spallation) life enhancement for low conductivity tbcs
11/01/2005US6960395 zirconia and stabilizer with three metal oxides (yttria, lanthana and ytterbia); physical vapor deposition onto metal substrate exposed to high temperatures; columnar microstructure
11/01/2005US6960060 Dual coolant turbine blade
10/2005
10/27/2005WO2005100941A1 Apparatus and method of balancing a shaft of an aircraft engine
10/27/2005WO2005100753A1 Strut comprising a sound-absorbing material for a turbine engine
10/27/2005WO2005100751A1 Non-positive-displacement machine and rotor for a non-positive-displacement machine
10/27/2005WO2005100750A1 Method for designing a low-pressure turbine of an aircraft engine, and low-pressure turbine
10/27/2005US20050238907 Highly oxidation resistant component
10/27/2005US20050238894 Mixed metal oxide ceramic compositions for reduced conductivity thermal barrier coatings
10/27/2005US20050238893 Substrate with protective coating; chromium, aluminum, yttrium alloy interface
10/27/2005US20050238888 Barium-strontium aluminosilicate; for protecting components exposed to high-temperature environments, such as the hot gas flow path through a gas turbine engine; performance in corrosive environments and exhibit increased volatilization resistance
10/27/2005US20050238526 Nickel alloys; used in turbine wheels, turbochargers;
10/27/2005US20050238525 Alloy containing silicon, nickel, carbon, at least a refractory metal which promotes work hardening is selected from molybdenum, niobium, tungsten, tantalum, rhenium, balance is cobalt; having good wear resistance, as well as good ductility due to content of hard particles (e.g. carbide) reduced
10/27/2005US20050238493 Multiple alloy rotor and method therefor
10/27/2005US20050238492 Reduced weight control stage for a high temperature steam turbine
10/27/2005US20050238491 Ceramic matrix composite airfoil trailing edge arrangement
10/27/2005US20050238488 Turbulator on the underside of a turbine blade tip turn and related method
10/27/2005US20050238485 Steam turbine rotor temperature control at oil deflector
10/27/2005US20050238483 Turbomachine with fluid removal
10/27/2005US20050238423 Fastener system for fastening together parts using pins having collars
10/27/2005US20050235878 Joint compounds using thickeners prepared from raw cotton linters
10/27/2005US20050235493 In-frame repair of gas turbine components
10/27/2005US20050235492 Turbine airfoil trailing edge repair and methods therefor
10/27/2005DE102004017193A1 Turbinenschaufelarretiervorrichtung Turbinenschaufelarretiervorrichtung
10/27/2005DE102004017096A1 Strebe für ein Turbinentriebwerk Strut for a turbine engine
10/27/2005DE102004016244A1 Rotor für eine Turbomaschine Rotor for a turbomachine
10/27/2005CA2562710A1 Apparatus and method of balancing a shaft
10/26/2005EP1589193A2 Coolable rotor blade for a gas turbine engine
10/26/2005EP1589192A1 Turbine blade with an insert for impingement cooling
10/26/2005EP1589191A1 Method for intentionally mistuning a turbomachine bladed rotor and rotors with intentionally mistuned blades
10/26/2005EP1589190A2 Steam turbine rotor cooling at oil deflector
10/26/2005EP1589189A1 Attachment system for stud connections carrying projections
10/26/2005EP1588992A1 Mixed metal oxide ceramic compositions for reduced conductivity thermal barrier coatings
10/26/2005EP1588024A2 Cooling fan with reinforced blade
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