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)
12/2003
12/11/2003US20030228223 Turbine blade cover cooling apparatus and method of fabrication
12/11/2003US20030228222 Turbine blade core cooling apparatus and method of fabrication
12/11/2003US20030228221 Turbine blade wall cooling apparatus and method of fabrication
12/11/2003US20030226878 Refractory metal backing material for weld repair
12/11/2003US20030226362 Structural cover for gas turbine engine bolted flanges
12/10/2003EP1369554A1 Cooling of a double walled turbine blade and method of fabrication
12/10/2003EP1369553A2 Rotor blade for a centripetal turbine
12/10/2003EP1369552A2 Structural cover for gas turbine engine bolted flanges
12/10/2003EP1369404A2 Method for protecting a substrate with a multilayer oxide/phosphate coating having a temperature-stepped cure
12/10/2003EP1163427B1 Gas turbine rotor with internally-cooled gas turbine blade
12/10/2003CN1460785A Gas turbine and gas turbin generator
12/09/2003US6660102 Method of decoating a turbine blade
12/09/2003US6659725 Vibration damping
12/09/2003US6659714 Baffle cooling device
12/04/2003WO2003100220A1 Axial securing means for impeller blades
12/04/2003WO2003100110A2 Method for removing at least one partial area of a component made of metal or a metallic compound
12/04/2003US20030224200 Thermal barrier coating material
12/04/2003US20030224124 Dense, strain-tolerant, vertically- cracked YSZ-containing ceramic layer on a second layer that is either a combination of YSZ and mullite or YSZ and a alkaline-earth metal aluminosilicate
12/04/2003US20030223893 Cooling the upstream end plate of a high pressure turbine by means of a system of dual injectors at the end of the combustion chamber
12/04/2003US20030223873 Inertia welding of blades to rotors
12/04/2003US20030223872 Covers for turbine buckets and methods of assembly
12/04/2003US20030223870 Method and apparatus for reducing turbine blade tip region temperatures
12/04/2003US20030223862 Methods and apparatus for cooling gas turbine engine nozzle assemblies
12/04/2003US20030223861 Ceramic matrix composite gas turbine vane
12/04/2003US20030223856 Gas turbine and method of bleeding gas therefrom
12/04/2003US20030223855 Axial compressor and gas bleeding method to thrust balance disk thereof
12/04/2003US20030221315 Mehtod for repairing damaged rotor blades of the turbine part of a gas turbine
12/03/2003EP1367250A1 Counter-rotatable booster compressor assembly for a gas turbine engine
12/03/2003EP1367226A1 Method and system for damage detection of an aircraft engine rotor
12/03/2003EP1367225A2 Gas turbine cooling arrangement and method of bleeding gas therefrom
12/03/2003EP1367224A1 Methods and apparatus for cooling gas turbine engine nozzle assemblies
12/03/2003EP1367223A2 Ceramic matrix composite gas turbine vane
12/03/2003EP1367222A2 Method and apparatus for reducing turbine blade tip region temperatures
12/03/2003EP1367221A1 Double injector arrangement for cooling of the sideplate of a high pressure turbine
12/03/2003EP1367147A1 Wear-resistant coating and method for applying it
12/03/2003EP1367144A1 Process for removing portions of a metallic article
12/03/2003EP1367037A2 Ceramic matrix composite turbine vane
12/03/2003EP1366271A1 Method and apparatus for cooling gas turbine engine blade tips
12/03/2003EP1038092B1 Cover plate for gas turbine rotor
12/03/2003EP0921273B1 Rotor for gas turbines
12/03/2003CN1459556A Returnable pressurzing air compressor for gas turbine
12/03/2003CN1459550A Method and device for enhancing use life of gas turbine wing surface
12/02/2003US6656605 Low-sulfur article coated with a platinum-group metal and a ceramic layer, and its preparation
12/02/2003US6656533 By diffusion coating; turbine blades or vanes
12/02/2003US6655921 Rotor blade
12/02/2003US6655920 Turbomachine rotor assembly with two bladed-discs separated by a spacer
12/02/2003US6655906 Axial compressor and gas bleeding method to thrust balance disk thereof
12/02/2003US6655153 Gas turbine shaft and heat shield cooling arrangement
12/02/2003CA2275515C Method of treating metal components
11/2003
11/27/2003WO2003098020A2 Gas turbine with stator shroud in the cavity beneath the chamber
11/27/2003WO2003098008A1 Coolable component and method for the production of a through opening in a coolable component
11/27/2003WO2003097901A1 Heat insulating layer
11/27/2003WO2003064818A3 Geothermal steam turbine
11/27/2003US20030219338 Methods and apparatus for extending gas turbine engine airfoils useful life
11/27/2003US20030217548 Gas turbine and gas turbine power generator
11/27/2003US20030217546 Counterrotatable booster compressor assembly for a gas turbine engine
11/26/2003EP1365343A1 Method and apparatus for managing a maintenance operation
11/26/2003EP1365154A2 Counterrotatable booster compressor assembly for a gas turbine engine
11/26/2003EP1365108A2 Blade for a gas turbine engine and method for manufacturing such blade
11/26/2003EP1365107A1 Combustion engine, gas turbine, and polishing layer
11/26/2003EP1365106A1 Fluid machinery
11/26/2003EP1212516A4 Hydraulic seal for rotary pumps
11/26/2003EP1159533B1 Centrifugal air flow control
11/26/2003CN1458393A 陶瓷涡轮罩 Ceramic turbine shroud
11/26/2003CN1457953A Device and method for renewing cooling path in turbine wing surface
11/25/2003US6654710 Method for designing a flow device
11/25/2003US6652914 Method for selective surface protection of a gas turbine blade which has previously been in service
11/25/2003US6652237 Bucket and wheel dovetail design for turbine rotors
11/25/2003US6652235 Method and apparatus for reducing turbine blade tip region temperatures
11/25/2003US6652226 Methods and apparatus for reducing seal teeth wear
11/25/2003US6652220 Methods and apparatus for cooling gas turbine nozzles
11/24/2003CA2429511A1 Method and apparatus for managing an operation
11/20/2003WO2003095801A1 Gas turbine engine with active tip clearance control
11/20/2003US20030215665 Thermal barrier coating material
11/20/2003US20030215330 Turbines and their components
11/20/2003US20030215329 Turbine nozzle segment and method of repairing same
11/20/2003US20030215328 Ceramic turbine shroud
11/20/2003US20030215325 Reduced noise fan stationary blade
11/20/2003US20030215323 Micro gas turbine engine with active tip clearance control
11/20/2003US20030213786 Hand held powder-fed laser fusion welding torch
11/20/2003US20030213427 Method of welding single crystals
11/19/2003EP1363217A2 Rotation planning apparatus and rotation planning system
11/19/2003EP1362983A2 Ceramic turbine shroud
11/19/2003EP1362982A1 Turbine airfoil with single aft flowing three pass serpentine cooling circuit
11/19/2003EP1362933A1 Thermal barrier coating
11/19/2003EP1123457B1 Gas turbine engine
11/19/2003EP1015736B1 Turbine bucket and use thereof
11/19/2003CN1457384A Combustion engine, gas turbine and polishing layer
11/19/2003CN1457375A Wear-resistant coating and method fr applying it
11/19/2003CN1456791A Turbine blades with notches on roots
11/18/2003US6648601 Labyrinth seal for fan assembly
11/18/2003US6648600 Turbine rotor
11/18/2003US6648597 Ceramic matrix composite turbine vane
11/18/2003US6648596 Lighter weight
11/18/2003US6648593 Tip treatment bars for gas turbine engines
11/18/2003US6648592 Centripetal air-bleed system
11/18/2003US6648591 Tip treatment assembly for a gas turbine engine
11/18/2003US6647732 Gas turbine engine with compressor and turbine inside a hollow shaft
11/18/2003US6647730 Turbine engine having turbine cooled with diverted compressor intermediate pressure air
11/18/2003US6647602 Fixation device for blading of a turbo-machine
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