Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
12/2006
12/07/2006WO2006052278A3 Ceramic matrix composite airfoil trailing edge arrangement
12/07/2006US20060275132 Composite aerofoil
12/07/2006US20060275130 Blade/disk dovetail backcut for blade/disk stress reduction (9FA+e, stage 2)
12/07/2006US20060275129 Blade/disk dovetail backcut for blade/disk stress reduction (9FA+e, stage 1)
12/07/2006US20060275127 Rotor for a gas turbine and gas turbine
12/07/2006US20060275124 Methods and systems for assembling shrouded turbine bucket and tangential entry dovetail
12/07/2006US20060275119 Vortex cooling for turbine blades
12/07/2006US20060275118 Turbine airfoil with integrated impingement and serpentine cooling circuit
12/07/2006US20060272152 Method for the maintenance of gas turbines
12/07/2006DE102005025213A1 Schaufel einer Axialströmungsmaschine A blade axial flow
12/07/2006DE102005024932A1 Turbinenschaufelaxialsperre Turbinenschaufelaxialsperre
12/07/2006DE102004003354B4 Turbinen-Laufschaufel und Gasturbine Turbine blade and gas turbine
12/07/2006CA2548692A1 Blade neck fluid seal
12/07/2006CA2548251A1 Combined blade attachment and disk lug fluid seal
12/06/2006EP1728972A2 Blocking element for a turbine blade
12/06/2006EP1728971A1 Integral turbine composed of a cast single crystal blade ring diffusion bonded to a high strength disk
12/06/2006EP1728970A2 Turbine blade cooling system
12/06/2006EP1728969A2 Cooled airfoil
12/06/2006EP1728886A1 Steam turbine blade, and steam turbine and steam turbine power plant using the same
12/06/2006EP1727970A1 Method and apparatus for establishing the state of the rotor of a turbomachine
12/06/2006EP1581386B1 Layer system
12/06/2006EP1530669B1 Method for testing a component in a non-destructive manner
12/06/2006CN1875169A Turbine cascade structure
12/06/2006CN1872491A Methods and systems for assembling shrouded turbine bucket and tangential entry dovetail
12/06/2006CN1288333C Turbine and supercharger thereof
12/06/2006CN1288329C Cooling arrangement for gas-turbine components
12/06/2006CN1288266C Ni base sintered alloy
12/06/2006CA2548361A1 Integrated counterrotating turbofan
12/06/2006CA2548339A1 Turbine airfoil with integrated impingement and serpentine cooling circuit
12/06/2006CA2548133A1 Counterrotating turbofan engine
12/05/2006US7144303 Method of polishing a large part and abrasive for use in the method
12/05/2006US7144222 Propeller
12/05/2006US7144221 Method and apparatus for assembling gas turbine engines
12/05/2006US7144220 Investment casting
12/05/2006US7144216 Wind turbine with outer noise shell
12/05/2006US7144215 Method and apparatus for cooling gas turbine engine rotor blades
12/05/2006CA2343888C Sealing device for segmented stator ring
12/02/2006CA2843079A1 Angled blade firtree retaining system
12/02/2006CA2547176A1 Angled blade firtree retaining system
11/2006
11/30/2006WO2006127159A1 Detection of gas turbine airfoil failure
11/30/2006WO2006126993A1 Turbocharger compressor having improved erosion-corrosion resistance
11/30/2006WO2006125959A1 Water turbine with bi-symmetric airfoil
11/30/2006US20060269759 Method for producing a protective layer, protective layer, use thereof, and part provided with a protective layer
11/30/2006US20060269417 Bladed rotor wheel for reinforcing blade locking
11/30/2006US20060269416 Blower and impeller structure thereof
11/30/2006US20060269415 Coated forward stub shaft dovetail slot
11/30/2006US20060269412 Fan and impeller thereof
11/30/2006US20060269410 Turbine blade cooling system
11/30/2006US20060269409 Gas turbine moving blade having a platform, a method of forming the moving blade, a sealing plate, and a gas turbine having these elements
11/30/2006US20060269408 Turbine airfoil trailing edge cooling system with segmented impingement ribs
11/30/2006US20060269403 Rotor
11/30/2006US20060269396 Wind power station
11/30/2006US20060266801 Assembly and method for manufacture of component by hot isostatic pressing
11/30/2006US20060266050 Gas turbine disk slots and gas turbine engine using same
11/30/2006DE19819267B4 Seitenkanalverdichter Side channel blowers
11/30/2006DE19757945B4 Rotor für thermische Turbomaschine Rotor for thermal turbomachinery
11/30/2006DE102006004437A1 Plattform einer Laufschaufel einer Gasturbine, Verfahren zur Herstellung einer Laufschaufel, Dichtungsplatte und Gasturbine Platform of a moving blade of a gas turbine process for the production of a blade, seal plate and gas turbine
11/30/2006DE102005025086A1 Anordnung zum Feinauswuchten des Rotors eines Gasturbinentriebwerks Arrangement for precision balancing of the rotor of a gas turbine engine
11/30/2006CA2609014A1 Water turbine with bi-symmetric airfoil
11/30/2006CA2548894A1 Deflectors for controlling entry of fluid leakage into the working fluid flowpath of a gas turbine engine
11/29/2006EP1726831A2 Coated forward stub shaft dovetail slot
11/29/2006EP1726804A2 Shroud for an Air Turbine Starter
11/29/2006EP1726785A2 Turbine airfoil platform cooling circuit
11/29/2006EP1726784A2 Gas turbine disk slots and gas turbine engine using same
11/29/2006EP1726783A1 Hollow rotor blade for the turbine of a gas turbine engine, provided with a tip cup
11/29/2006EP1726782A2 Turbine blade trailing edge construction
11/29/2006EP1726781A1 Turbine airfoil with tapered trailing edge ribs
11/29/2006EP1726780A2 Device for a precision balancing of turbine rotors
11/29/2006EP1725741A1 Non-positive-displacement machine and rotor for a non-positive-displacement machine
11/29/2006EP1636461B1 Turbomachine, in particular gas turbine
11/29/2006CN1869410A Turbine airfoil platform cooling circuit
11/29/2006CN1869409A Platform of gas turbine moving blade, a method of forming the moving blade, a sealing plate, and a gas turbine having these elements
11/29/2006CN1869408A Coated forward stub shaft dovetail slot
11/29/2006CN1869407A Compressor wheel
11/28/2006US7141128 Intermetallic material and use of this material
11/28/2006US7140841 Rotor blade connecting arrangement for a turbomachine
11/28/2006US7140346 Diesel-type piston engine and a method for controlling a diesel-type piston engine
11/28/2006CA2383404C Method for replacing a turbine vane airfoil
11/28/2006CA2284759C Process for manufacturing or repairing turbine engine or compressor components
11/26/2006CA2548603A1 Improvement to a rotor impeller wheel to reinforce locking of blades
11/23/2006WO2006124617A2 BLADE/DISK DOVETAIL BACKCUT FOR BLADE/DISK STRESS REDUCTION (9FA+e, STAGE 1)
11/23/2006WO2006124614A2 Blade/disk dovetail backcut for blade/disk stress reduction (9fa+e, stage 2)
11/23/2006WO2006065445A3 Dual pressure euler steam turbine
11/23/2006US20060263222 Composite filled gas turbine engine blade with gas film damper
11/23/2006US20060263218 Angled cooling divider wall in blade attachment
11/23/2006US20060263217 Gas turbine airfoil with adjustable cooling air flow passages
11/23/2006US20060263204 Sealing arrangement, in particular for the blade segments of gas turbines
11/23/2006US20060263200 Centrifugal pump and an impeller thereof
11/23/2006DE19845147B4 Vorrichtung und Verfahren zur Kühlung einer einseitug von Heißgas umgebenen Wand Apparatus and method for cooling a hot gas einseitug surrounding wall
11/23/2006DE102004016977B4 Rotor für eine Turbomaschine Rotor for a turbomachine
11/23/2006CA2547172A1 Angled cooling divider wall in blade attachment
11/23/2006CA2547121A1 Mass calibration process for parts to be assembled around a rotor
11/22/2006EP1724455A2 Drive arrangement
11/22/2006EP1724442A1 Turbine blade root
11/22/2006EP1724441A2 Tip shroud relief fillet for a turbine bucket
11/22/2006EP1724440A1 Process for optimizing the flow in multistage turbomachines
11/22/2006EP1724439A2 Method for making a compositionally graded gas turbine disk
11/22/2006EP1724438A2 Method for making a compositionally graded gas turbine disk
11/22/2006EP1724437A1 Turbine shaft
11/22/2006EP1723339A1 Compressor of a gas turbine and gas turbine