Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
01/2011
01/06/2011US20110002772 Control device and method for an aerodynamic brake of a wind energy converter
01/06/2011US20110002771 Rotor blade over-tip leakage control
01/06/2011CA2766661A1 Propeller hub
01/06/2011CA2766552A1 Nickel base superalloy compositions and superalloy articles
01/06/2011CA2766534A1 Rotor blade and method for reducing tip rub loading
01/05/2011EP2270337A1 Blade of a gas turbine engine for an airplane, and a method for manufacturing the same
01/05/2011EP2270314A2 An assembly providing contaminant removal
01/05/2011EP2270313A2 High-temperature resistant gas turbine component
01/05/2011EP2270312A1 Aero- or hydrodynamic construction
01/05/2011EP2270258A2 High reliability turbine metal sealing material
01/05/2011EP2269966A2 Turbine engine components
01/05/2011EP2268901A1 Turbine blade with tip cooling and corresponding turbine and turboengine
01/05/2011EP2268900A1 Blade for a rotating thermal engine
01/05/2011DE19926949B4 Kühlungsanordnung für Schaufeln einer Gasturbine Cooling arrangement for a gas turbine blades
01/05/2011DE102010017489A1 Turbinenmaschinenzugehörige Systeme und Vorrichtungen und Dichtungen für Turbinenmaschinen Related turbine engine systems and devices and seals for turbine engines
01/05/2011DE102010017435A1 Verfahren und Vorrichtung zum Zusammenbau von Rotationsmaschinen Method and apparatus for the assembly of rotating machinery
01/05/2011DE102009030042A1 Turbinenläufer für einen Turbolader und Verfahren zur Herstellung eines Turbinenläufers A turbine rotor for a turbo charger and method for manufacturing a turbine rotor
01/05/2011CN201696100U Ship axial flow propulsor
01/05/2011CN101939509A Arrangement for axially securing blades in a rotor of a gas turbine
01/05/2011CN101936191A Method and apparatus for assembling rotating machines
01/05/2011CN101936190A Turbine rotor blade
01/05/2011CN101936189A 涡轮机转子 Turbine rotor
01/05/2011CN101935818A Functionally gradient coating of rotor vane
01/05/2011CN101935781A Nickel-base superalloys and components formed thereof
01/05/2011CN101935780A Method of controlling and refining final grain size in supersolvus heat treated nickel-base superalloys
01/05/2011CN101934405A Brazing method
01/04/2011US7862901 Gas turbine engine component; coating system, superalloy substrate; adherent ceramic thermal barrier of yttria stabilized zirconia, hafnia, gadolinia, neodymia, erbia, dysprosia, europia, tantala, yttebria, titania; turbine blade, vane, shroud; survive higher operating temperatures, increase reliability
01/04/2011US7862300 Turbomachinery blade having a platform relief hole
01/04/2011US7862299 Two piece hollow turbine blade with serpentine cooling circuits
01/04/2011US7862294 Labyrinth seal in a stationary gas turbine
01/04/2011US7862291 Gas turbine engine component cooling scheme
01/04/2011CA2481111C Process of masking cooling holes of a gas turbine component
12/2010
12/30/2010US20100329888 Turbomachinery blade having a platform relief hole, platform cooling holes, and trailing edge cutback
12/30/2010US20100329887 Coolable gas turbine engine component
12/30/2010US20100329884 Turbine rotor blade
12/30/2010US20100329883 Method of controlling and refining final grain size in supersolvus heat treated nickel-base superalloys
12/30/2010US20100329882 Ceramic Heat-Insulating Layers Having Increased Corrosion Resistance to Contaminated Fuels
12/30/2010US20100329878 Adjustable camber aerofoil
12/30/2010US20100329877 Method for producing a forging from a gamma titanium aluminum-based alloy
12/30/2010US20100329875 Rotor blade with reduced rub loading
12/30/2010US20100329874 Hp turbine blade airfoil profile
12/30/2010US20100329873 Retaining and sealing ring assembly
12/30/2010US20100329872 Method and apparatus for assembling rotating machines
12/30/2010US20100329863 Method for reducing tip rub loading
12/30/2010US20100329862 Cooling Hole Exits for a Turbine Bucket Tip Shroud
12/30/2010US20100329855 Fan shroud with modular vane sets
12/30/2010US20100329849 Turbine rotor
12/30/2010US20100329848 Shroudless blade
12/30/2010US20100329847 Stationary blade and steam turbine
12/30/2010US20100329846 Turbine engine components
12/30/2010DE102010017363A1 Kühllochaustritte für ein Turbinenschaufelspitzendeckband Cooling hole outlets for a turbine blade tip shroud
12/30/2010DE102009030566A1 Deckbandsegment zur Anordnung an einer Schaufel Shroud segment for placement on a shovel
12/30/2010DE102009030398A1 Verfahren zum Herstellen und/oder Reparieren einer Schaufel für eine Strömungsmaschine A method for producing and / or repairing a blade for a turbomachine
12/30/2010DE102009030397A1 Befestigungsvorrichtung einer Turbinen- oder Verdichterschaufel Fastening device of a turbine or compressor blade
12/30/2010CA2699029A1 Hp turbine blade airfoil profile
12/29/2010WO2010150567A1 Turbine rotor
12/29/2010WO2010149555A1 Rotor blade for an axial flow turbomachine and mounting for such a rotor blade
12/29/2010WO2010149480A1 Turbine rotor for a turbocharger, turbocharger and method for producing a turbine rotor
12/29/2010WO2010149462A1 Method for the production of a turbine rotor for a turbocharger, including determining an axis of unbalance and a cylindrical grinding process; turbocharger comprising a cylindrically ground welded pin
12/29/2010WO2010149146A2 Fastening device of a turbine blade or compressor blade
12/29/2010WO2010149141A2 Method for producing and/or repairing a blade for a turbo-machine
12/29/2010WO2010149139A2 Shroud segment to be arranged on a blade
12/29/2010WO2010054633A3 Wear-resistant layer for tial
12/29/2010WO2010054632A3 Blade cluster having offset axial mounting base
12/29/2010WO2010000228A3 Rotor blade and flow engine comprising a rotor blade
12/29/2010EP2267278A2 Turbine rotor blade with hardened region
12/29/2010EP2267277A2 Annulus filler and method of mounting the annulus filler to a rotor disc of a gas turbine engine
12/29/2010EP2267276A2 Airfoil with hybrid drilled and cutback trailing edge
12/29/2010EP2267275A2 A shroudless blade
12/29/2010EP2267274A2 A compressor blade
12/29/2010EP2267273A2 Adjustable camber aerofoil
12/29/2010EP2265800A1 Cooling duct arrangement within a hollow-cast casting
12/29/2010EP2265799A1 Guide vane for a gas turbine
12/29/2010EP2044291B1 Method for repairing a guide blade segment for a jet engine
12/29/2010EP1869290B1 Component with film cooling holes
12/29/2010CN201687526U Steam turbine blade assembling, adjusting and positioning device
12/29/2010CN201687525U Turbo charger rotary shaft capable of monitoring rotation speed
12/29/2010CN101929414A Turbine and hydroturbine rotor
12/29/2010CN101929358A Cooling hole exits for a turbine bucket tip shroud
12/29/2010CN101929357A Systems, methods, and apparatus for thermally isolating a turbine rotor wheel
12/29/2010CN101927568A Method for manufacturing braided preforms
12/29/2010CN101457657B Axial positioning structure for firtree type blade root and blade
12/29/2010CN101421427B Nickel-based heat resistant alloy for gas turbine combustor
12/29/2010CN101349168B Last stage movable vane of air cooling steam turbine
12/29/2010CA2708467A1 Method and apparatus for providing rotor discs
12/28/2010US7857595 Molded reinforced shear web cores
12/28/2010US7857594 Turbine exhaust strut airfoil profile
12/28/2010US7857589 Turbine airfoil with near-wall cooling
12/28/2010US7857588 Reinforced airfoils
12/28/2010US7857587 Turbine blades and turbine blade cooling systems and methods
12/25/2010CA2707966A1 Turbine rotor blade
12/23/2010WO2010147691A2 Trapped spring balance weight and rotor assembly
12/23/2010WO2010146999A1 FERRITIC Cr-STEEL FOR HEAT-RESISTANT PRECISION COMPONENT AND METHOD FOR PRODUCING SAME, AND HEAT-RESISTANT PRECISION COMPONENT AND METHOD FOR PRODUCING SAME
12/23/2010WO2010146288A1 Turbine distributor element made of cmc, method for making same, distributor and gas turbine including same
12/23/2010WO2010105597A3 Tandem blade design
12/23/2010WO2010098939A8 Method and apparatus for pre-spinning rotor forgings
12/23/2010US20100322798 Rapidly rotating vacuum pump
12/23/2010US20100322783 Rotor or stator blade and method for forming such rotor or stator blade
12/23/2010US20100322781 Impeller and turbocharger
12/23/2010US20100322777 Compressor blade