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