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)
10/2012
10/31/2012CN202510225U Micro gas turbine power generation system with wave rotor top regenerative cycle
10/31/2012CN202510170U Device for cooling gas turbine blade
10/31/2012CN202510169U Turbine blade of gas turbine
10/31/2012CN202510168U Gas turbine unit
10/31/2012CN1936275B Steam turbine blade capable of reducing top leakage loss
10/31/2012CN102762817A 涡轮机翼面 Turbine airfoil surface
10/31/2012CN102762816A A method and a device of tangentially biasing internal cooling on nozzle guide vane
10/31/2012CN102762815A Removal of stuck blade in a turbine engine
10/31/2012CN102762778A Method for the electrolytic deposition of a composite coating having a metal matrix containing particles for repairing a metal blade
10/31/2012CN102762336A Method for repairing a flange of a housing
10/31/2012CN102758652A Adaptor assembly for coupling turbine blades to rotor disks
10/31/2012CN102758651A Component and methods of fabricating a coated component using multiple types of fillers
10/30/2012US8297935 Turbine blades and methods of forming modified turbine blades and turbine rotors
10/30/2012US8297932 Blade insert
10/30/2012US8297931 Annulus filler
10/30/2012US8297927 Near wall multiple impingement serpentine flow cooled airfoil
10/30/2012US8297926 Turbine blade
10/30/2012US8297925 Aerofoil configuration
10/30/2012US8297915 Real-time turbomachinery blade breakage monitoring unit and turbo-apparatus
10/30/2012CA2500548C Turbine engine for example a gas turbine engine for an aircraft
10/26/2012WO2012145121A1 Cooled airfoil in a turbine engine
10/26/2012WO2012144244A1 Vane member and rotary machine
10/25/2012US20120269650 Turbine wheel for a turbine engine
10/25/2012US20120269649 Turbine blade with improved trailing edge cooling
10/25/2012US20120269648 Serpentine cooling circuit with t-shaped partitions in a turbine airfoil
10/25/2012US20120269647 Cooled airfoil in a turbine engine
10/25/2012US20120269646 Nickel base superalloy
10/25/2012US20120269638 Compressor having blade tip features
10/25/2012US20120269637 Methods for controlling friction between heterogeneous contact surfaces
10/25/2012US20120269636 Blade features for turbocharger wheel
10/25/2012US20120269635 Hub features for turbocharger wheel
10/24/2012EP2514924A2 System and method for modifying a slot in a rotor
10/24/2012EP2514923A1 Screen device, integrated bladed rotor base body, method and fluid flow engine
10/24/2012EP2514922A2 Compressor with blade tip geometry for reducing tip stresses
10/24/2012EP2514921A1 Method of modifying excitation response characteristics of a system, corresponding process for designing a component, and system having a controlled limit cycle amplitude
10/24/2012EP2514850A1 Method for producing a heat-shielding coating, turbine member provided with said heat-shielding coating, and gas turbine
10/24/2012EP2513427A1 Composite material turbine engine blade and method for manufacturing same
10/24/2012EP2513426A2 Turbine blade damping device with controlled loading
10/24/2012EP2513425A1 Turbine blade damping device with controlled loading
10/24/2012EP2512727A1 Method for repairing a titanium blade by laser recharging and moderate hip pressing
10/24/2012EP2512722A1 Process for manufacturing a component
10/24/2012CN102753788A Turbine engine air blower
10/24/2012CN102753787A Airfoil incorporating tapered cooling structures defining cooling passageways
10/24/2012CN101696685B Impeller overspeed testing apparatus
10/24/2012CN101067381B Gas turbine has cooling air transfer system
10/23/2012US8292586 Annulus filler
10/23/2012US8292584 Component having a film cooling hole
10/23/2012US8292583 Turbine blade having a constant thickness airfoil skin
10/23/2012US8292582 Turbine blade with serpentine flow cooling
10/23/2012US8292581 Air cooled turbine blades and methods of manufacturing
10/23/2012US8292580 CMC vane assembly apparatus and method
10/23/2012US8292578 Material having internal cooling passage and method for cooling material having internal cooling passage
10/23/2012US8291557 Apparatus for rebuilding gas turbine engines
10/23/2012CA2500942C Ceramic-based bushing for a variable setting system for turbine engine blades
10/23/2012CA2491619C Bifurcated outlet guide vanes
10/18/2012WO2012141858A1 Low pressure cooling seal system for a gas turbine engine
10/18/2012WO2012140806A1 Gas turbine rotor blade and gas turbine
10/18/2012WO2012140062A2 Wind turbine blade with tapering root bushings
10/18/2012WO2012140049A2 Wind turbine blade comprising cylindrical metal inserts in a root region thereof
10/18/2012WO2012140048A2 Wind turbine blade having a root region with elongated fastening members provided with metal fibres
10/18/2012WO2012140043A2 Wind turbine blade with elongated fastening members in the root region thereof
10/18/2012WO2012140041A2 A wind turbine blade comprising metal fibres and a transition region
10/18/2012WO2012140039A2 Wind turbine blade comprising circumferential retaining means in root regions
10/18/2012US20120263603 Turbine blade and gas turbine
10/18/2012US20120263599 Impeller and turbomachinery including the impeller
10/18/2012US20120263597 Turbomachine rotor with anti-wear shim between a disk and an annulus
10/18/2012US20120263595 Annulus filler system
10/18/2012US20120263575 Low pressure cooling seal system for a gas turbine engine
10/18/2012DE112009004286T5 Keramikmatrixverbundwerkstofflaufschaufel mit integralen Plattformstrukturen und Verfahren zu ihrer Herstellung Ceramic matrix composite blade with integral platform structures and processes for their preparation
10/18/2012DE102011007224A1 Verfahren und Herstellung eines einstückigen Rotorbereiches und einstückiger Rotorbereich Process and producing a piece rotor portion and an integral rotor area
10/18/2012DE102007024591B4 Gasturbine mit einem Stator, einem Rotor sowie einer Dichteinrichtung Gas turbine having a stator, a rotor as well as a sealing device
10/17/2012EP2511480A2 Annulus filler system
10/17/2012EP2511479A2 Annulus filler system
10/17/2012EP2511478A1 Liner for a composite blade of a gas turbine engine and corresponding blade assembly
10/17/2012EP2511476A1 Turbine and turbine rotor blade
10/17/2012EP2511475A2 Methods of fabricating a coated component using multiple types of fillers
10/17/2012EP2511398A1 Application of treatment fluids to components
10/17/2012EP2510228A1 Vertical axis wind turbine with self-starting capabilities
10/17/2012EP2510194A1 Coupling for rotor balancing
10/17/2012EP2509739A1 Method of beam welding of an impeller with performance of two passes on a slot; impeller and turbo machine having such weld configuration
10/17/2012CN202493293U Beveling clapboard body type structure of steam turbine
10/17/2012CN202493292U Novel balanced structure of impeller of steam turbine
10/17/2012CN102741522A Turbine wheel and method for the production thereof
10/17/2012CN102741506A Rotor blade for gas turbine, method for manufacturing same, and gas turbine using rotor blade
10/17/2012CN102741043A Method for manufacturing a vane having composite internal channels and composite turbine engine vane
10/17/2012CN102741007A Method of beam welding of an impeller with performance of two passes on a slot
10/17/2012CN102733866A Compact high-load power turbine generator
10/17/2012CN102733864A Flexible seal for turbine engine
10/17/2012CN102733862A Locking device arrangement for rotating bladed stage
10/17/2012CN102733861A Method and system for sealing dovetail
10/17/2012CN102733860A Turbine shroud segment cooling system and method
10/17/2012CN102733859A Microstructures for reducing noise of fluid dynamic structure
10/17/2012CN102733858A Turbomachine rotor
10/17/2012CN102732883A Precious metal particle dispersed toughened composite thermal barrier coating and its preparation method
10/17/2012CN102732817A Methods for forming an oxide-dispersion strengthened coating
10/17/2012CN101349167B Axial flow turbine
10/16/2012US8287239 Annulus filler
10/16/2012CA2472299C Improvement in the retention capacity of an assymetric hammer attachment blade
10/11/2012WO2012137898A1 Turbine vane
10/11/2012WO2012136917A1 Sealing ring for a turbine stage of an aircraft turbomachine, comprising slotted anti-rotation pegs
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