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)
09/2005
09/15/2005US20050201859 Gas turbine ventilation circuitry
09/15/2005US20050201857 Mounting arrangement for turbine blades
09/15/2005US20050201856 Bifurcated outlet guide vanes
09/15/2005US20050201611 Non-contact measurement method and apparatus
09/15/2005US20050199683 Method of joining material
09/15/2005US20050198967 Smart component for use in an operating environment
09/15/2005DE102004009755A1 Gasturbinenschaufel Gas turbine blade
09/15/2005DE102004007327A1 Rotor Rotor
09/15/2005CA2536093A1 Round honeycomb rotor
09/14/2005EP1574818A2 Non-contact measurement method and apparatus
09/14/2005EP1574685A1 Turbojet having two counterrotating fans integral with a counterrotating low pressure compressor
09/14/2005EP1574670A2 A mounting arrangement for turbine blades
09/14/2005EP1574669A2 Impingement cooling arrangement witin turbine blades
09/14/2005EP1574668A2 Bifurcated outlet guide vanes
09/14/2005EP1574667A1 Diffuser for compressor
09/14/2005EP1574666A1 Turbine blade array
09/14/2005EP1574665A1 Rotor for a turbomachine
09/14/2005EP1574270A1 Method for making a reinforced leading or trailing edge for a fan blade
09/14/2005EP1573171A1 Passively cooled blade platform
09/14/2005CN2725533Y High power steam turbine low pressure self crown carried long blade stepped surrounding belt
09/14/2005CN1667245A Pressure balance of flange connection in the overflow pipe between live steam valve and high pressure turbine
09/13/2005US6942460 Vane wheel for radial turbine
09/13/2005US6942457 Fan assembly and method
09/13/2005US6942455 Strain isolated trim tab
09/13/2005US6942450 Differential pressure sensing system for airfoils usable in turbine engines
09/13/2005US6942449 Trailing edge cooling
09/13/2005CA2142423C Process for welding two blade parts
09/09/2005WO2005083269A2 Turbocharger compressor wheel having a counterbore treated for enhanced endurance to stress-induced fatigue and configurable to provide a compact axial length
09/09/2005WO2005083236A1 Blade or vane for a rotary machine
09/09/2005WO2005083235A1 Blade or vane for a turbomachine
09/09/2005WO2005083234A1 Gas turbine vane
09/08/2005US20050196278 Turbine blade arrangement
09/08/2005US20050196277 Gas turbine bucket tip cap
09/08/2005US20050196273 Power tool
09/08/2005US20050196268 High modulus metallic component for high vibratory operation
09/08/2005US20050196088 Turbomachine with a compact roller bearing
09/08/2005US20050194068 Nickel-based superalloy having very high resistance to hot-corrosion for monocrystalline blades of industrial turbines
09/07/2005EP1571342A2 Swept turbomachinery blade
09/07/2005EP1571297A2 High elasticity modulus turbine metallic component for high vibratory operation
09/07/2005EP1571296A1 Cooled blade of a turbomachine and method of cooling
09/07/2005EP1571295A1 Cooled blade of a turbomachine and method of cooling
09/07/2005EP1571294A1 Hook-shaped sideplate for a rotor disc
09/07/2005EP1571236A1 Process for surface conversion of an article
09/07/2005CN1665960A Highly oxidation resistant component
09/07/2005CN1665959A Highly oxidation resistant component
09/07/2005CN1665623A Diffusion bond mixture for healing single crystal alloys
09/07/2005CN1664331A Closed circuit blade-cooled turbine
09/07/2005CN1664319A Turbomachine rolling bearing assembly having a reduced space requirement
09/07/2005CN1664316A Gas turbine bucket tip cap
09/07/2005CN1663749A Power tool
09/07/2005CN1218115C Turbine blade capable of bearing high load
09/06/2005US6939603 Thermal barrier coating having subsurface inclusions for improved thermal shock resistance
09/06/2005US6939108 Cooling fan with reinforced blade
09/06/2005US6939107 Spanwisely variable density pedestal array
09/06/2005US6939106 Sealing of steam turbine nozzle hook leakages using a braided rope seal
09/06/2005US6939104 Turbine blade with sealing element
09/06/2005US6939102 Flow guide component with enhanced cooling
09/06/2005US6938447 Apparatus and method of correcting deformation of gas turbine blade
09/01/2005US20050191422 Applying mask material to cooling holes so that holes are at partially filled with mask material in portion closest to external surface and up to the level of the external surface, thickening portion of mask material within cooling holes, coating, removing thickened mask material
09/01/2005US20050191182 Turbine blade shroud cutter tip
09/01/2005US20050191181 Rotor disk balancing device, disk fitted with such a device and rotor with such a disk
09/01/2005US20050191177 Compressor stator vane
09/01/2005US20050191172 Inducer with shrouded rotor for high speed applications
09/01/2005US20050191168 Rolled ring air baffle for a gas turbine engine rotating cavity
09/01/2005US20050191167 Fanned trailing edge teardrop array
09/01/2005US20050189827 Gas turbomachinery generator
09/01/2005US20050188765 Method and machine for rotor imbalance determination
09/01/2005DE10393116T5 Turbinenrotor-Reparaturverfahren Turbine rotor repair method
08/2005
08/31/2005EP1568868A2 High by-pass ratio turbofan
08/31/2005EP1568848A2 A method and machine for rotor imbalance determination
08/31/2005EP1568795A1 Heat resistant superalloy and its use
08/31/2005EP1568486A1 Method for manufacturing of workpieces or semifinished products containing titanium aluminide alloys and products made thereby
08/31/2005EP1567749A1 Turbine shaft and production of a turbine shaft
08/31/2005EP1360342B1 Method for plasma coating a turbine blade and coating device
08/31/2005CN2721283Y Composite crystallizer for single crystal and directional cylindrulite composite crystalline blade
08/31/2005CN1661200A Return blade rotary machinery using same
08/31/2005CN1661199A Profile of aerofoil section for turbine bucket
08/31/2005CN1660540A Process for producing components or semi-finished products which contain intermetallic titanium aluminide alloys, and components producible by the process
08/31/2005CN1660524A Crystalloid laminae composited from single crystal and directional column crystal and preparing method
08/31/2005CN1217105C Impeller for axial flow fan and method for mounting blade on hub for such fan
08/31/2005CN1217092C Gas turbine, gas turbomachine and coolant collecting method for blades of the same
08/31/2005CN1217091C Closed circulation cooling blade turbomachine
08/31/2005CN1217088C Fixed blades of steam turbine
08/30/2005US6936116 Nickel-based alloy for producing components solidified in single crystal form
08/30/2005US6935840 Low cycle fatigue life (LCF) impeller design concept
08/30/2005US6935836 Compressor casing with passive tip clearance control and endwall ovalization control
08/30/2005US6935833 Recirculation structure for turbo chargers
08/30/2005US6935120 Approach to extending life of gas turbine engine
08/30/2005US6935006 Spun metal form used to manufacture dual alloy turbine wheel
08/30/2005CA2266449C Gas turbine airfoil cooling
08/25/2005WO2005078242A1 Damping arrangement for guide vanes
08/25/2005WO2005059313A3 Vane and throat shaping for a radial turbine assembly
08/25/2005US20050187676 Approach to extending life of gas turbine engine
08/25/2005US20050186082 High-temperature component for a turbomachine, and a turbomachine
08/25/2005US20050186080 Fan or compressor blisk
08/25/2005US20050186079 Gas turbine tip shroud rails
08/25/2005US20050186076 Wind turbine with outer noise shell
08/25/2005US20050186075 Gas turbine nozzle guide vane
08/25/2005US20050186074 Moving blade and gas turbine using the same
08/25/2005US20050186069 Use of biased fabric to improve properties of SiC/SiC ceramic composites for turbine engine components
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