Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
12/1999
12/16/1999WO1999064725A1 Turbine nozzle vane
12/16/1999WO1999064724A1 Turbine engine vane segment
12/16/1999WO1999064200A1 Method and apparatus for repairing a turbine engine vane segment
12/16/1999WO1999055527A3 Product with an anticorrosion protective layer and a method for producing an anticorrosion protective
12/15/1999EP0964135A2 Steam turbine rotor welded together from different materials
12/15/1999EP0964077A2 A metallic article having a thermal barrier coating and a method of application thereof
12/15/1999CN2353894Y Radical energy-saving power booster for internal combustion engine
12/14/1999US6001492 First layer nearest substrate is intermetallic of aluminum and chromium, the second layer has chromium phase, and third layer chromium-platinum phase; graded thermal expansion properties moderate transition between substrate, insulation
12/14/1999US6000909 Cooling medium path in gas turbine moving blade
12/14/1999US6000908 Cooling for double-wall structures
12/14/1999US6000906 Ceramic airfoil
12/09/1999WO1999063204A1 Gas turbine and method for cooling a turbine stage
12/09/1999DE19824766A1 Gasturbine sowie Verfahren zur Kühlung einer Turbinenstufe Gas turbine and method for cooling a turbine stage
12/09/1999DE19824583A1 Turbine blade with tip capable of repetitive cutting of sealing grooves at high temperatures and in oxidizing atmospheres
12/08/1999EP0962874A1 Method for designing a flow device
12/08/1999EP0962545A1 Ceramic coating having a low thermal conductivity
12/07/1999US5998755 Tooling assembly for positioning airfoils of a rotary machine
12/07/1999US5997251 Ribbed turbine blade tip
12/07/1999US5997249 Turbine, in particular steam turbine, and turbine blade
12/07/1999US5997248 Silicon carbide composition for turbine blade tips
12/07/1999US5997245 Cooled shroud of gas turbine stationary blade
12/07/1999US5997244 Cooling airflow vortex spoiler
12/02/1999WO1999061756A1 A component for a gas turbine
12/01/1999EP0961017A2 High temperature resistant coating
12/01/1999EP0960308A1 Gas turbine installation with a ceramic-covered combustion chamber housing
12/01/1999EP0769093B1 Turbine vane assembly with integrally cast cooling fluid nozzle
12/01/1999CN1046881C Process for hard-rolling component
11/1999
11/30/1999US5993980 Protective coating for protecting a component from corrosion, oxidation and excessive thermal stress, process for producing the coating and gas turbine component
11/30/1999US5993976 A first metal oxide selected from the group consisting of oxides of yttrium, calcium, magnesium, and cerium, and a second metal oxide selected from the group consisting of oxides of zirconium, aluminum, and chromium
11/30/1999US5993162 Ramped dovetail rails for rotor blade assembly
11/30/1999US5993161 Rotors with mistuned blades
11/30/1999US5993160 Cover plate for gas turbine rotor
11/30/1999US5993156 Turbine vane cooling system
11/30/1999US5993155 Cooled gas-turbine blade
11/30/1999US5993154 Welded rotor of a turbo-engine
11/30/1999US5993149 Variable area compensation valve
11/29/1999CA2272815A1 A metallic article having a thermal barrier coating and a method of application thereof
11/25/1999WO1999060253A1 Cooled turbine blade platform
11/25/1999DE19823157A1 Fixing device for running blades of axial-flow turbine machines
11/24/1999EP0959228A1 Film-cooling holes in staggered rows
11/23/1999US5988982 Altering vibration frequencies of workpieces, such as gas turbine engine blades
11/23/1999US5988980 Blade assembly with splitter shroud
11/23/1999US5988522 Synthetic jet actuators for modifiying the direction of fluid flows
11/17/1999EP0957236A1 Turbine rotor blade
11/17/1999CN1235654A Cooling passages for airfoil leading edge
11/17/1999CN1046572C Angle adjustable vane suspension device
11/16/1999US5985467 Nitrogen-doped alumina anchoring layer; heat, erosion and corrosion resistance; nickel or cobalt-based alloy
11/16/1999US5985122 Method for preventing plating of material in surface openings of turbine airfoils
11/16/1999US5984639 Blade retention apparatus for gas turbine rotor
11/16/1999US5984638 Turbomachine radial impeller vibration constraining and damping mechanism
11/16/1999US5984637 Cooling medium path structure for gas turbine blade
11/16/1999US5984636 Cooling arrangement for turbine rotor
11/16/1999US5984631 Tandem turbine-blade cascade
11/16/1999US5984630 Reduced windage high pressure turbine forward outer seal
11/16/1999US5983623 System for cooling gas turbine blades
11/11/1999DE19820766A1 Impeller for pneumatic or hydraulic power generator
11/10/1999EP0955449A1 Gas turbine blade
11/10/1999EP0954680A1 Turbine blade and its use in a gas turbine system
11/10/1999EP0954679A1 Coolable airfoil for a gas turbine engine
11/10/1999EP0954406A2 Segmented mechanical shafting alignment tool and method
11/10/1999CN2348099Y Energy conversion machine
11/10/1999CN1234310A Non-circular shape cooling hole and processing method
11/09/1999US5981091 Article including thermal barrier coated superalloy substrate
11/09/1999US5981088 Thermal barrier coating system
11/09/1999US5980209 Turbine blade with enhanced cooling and profile optimization
11/09/1999US5980204 Method of establishing hook diameters on diaphragm packing ring dovetails
11/09/1999US5980202 Gas turbine stationary blade
11/09/1999US5979156 Cooling steam system for steam cooled gas turbine
11/04/1999WO1999055637A1 Cr2O3-Al2O3 BASE SINTER AND PROCESS FOR PRODUCING THE SAME
11/04/1999WO1999055527A2 Product with an anticorrosion protective layer and a method for producing an anticorrosion protective
11/04/1999DE19818928A1 Welded centrifugal pump rotor
11/04/1999DE19817705A1 Kühlluftentnahme auf der Saugseite einer Diffusorschaufel einer radialen Kompressorstufe von Gasturbinen Cooling air extraction on the suction side of a diffuser vane radial compressor stage of gas turbines
11/03/1999EP0953730A2 Repairing method for dovetail grooves
11/03/1999EP0953728A1 Booster compressor with tandem blading
11/03/1999EP0953100A1 Steam turbine
11/03/1999EP0619856B1 Aluminide-silicide coatings, coating compositions, process for coating and improved coated products
11/02/1999US5976337 The brazing material is accurately deposited and does not flow into and interfere with the passageway after the braze joint is formed.
11/02/1999US5975852 Thermal barrier coating system and method therefor
11/02/1999US5975851 Turbine blade with trailing edge root section cooling
11/02/1999US5975850 Turbulated cooling passages for turbine blades
11/02/1999US5975845 Turbomachinery abradable seal
11/02/1999US5975841 Heat pipe cooling for turbine stators
10/1999
10/28/1999WO1999054597A1 Turbine blade
10/28/1999WO1999047792B1 Turbine blade assembly with cooling air handling device
10/28/1999DE19918900A1 High temperature component, especially metallic gas turbine component
10/28/1999DE19807163C1 Wärmedämmaterial und Verfahren zum Herstellen eines solchen Thermal insulating material and method for producing such
10/27/1999EP0951614A1 Cooling system for gas turbine vane
10/27/1999EP0951579A2 Method of manufacturing hollow metal objects with elaborated cavities
10/26/1999US5972424 Removing ceramic and aluminum oxide layers from engine run gas turbine engine component, such that atleast some bond coat remains on the component, analyzing if it meets minimum standard, coating flash layer, new alumina and ceramic layers
10/26/1999US5971710 Turbomachinery blade or vane with a permanent machining datum
10/26/1999US5971708 Branch cooled turbine airfoil
10/26/1999US5971707 Gas turbine moving blade steam cooling system
10/26/1999US5971706 Inter-rotor bearing assembly
10/26/1999US5971010 Shaft device and a method of cooling a shaft device
10/20/1999EP0950463A1 Non-circular cooling hole and method of manufacturing the same
10/20/1999CN1232524A Gas turbine airfoil cooling system and method
10/19/1999US5967755 Product with a metallic basic body and method for manufacturing a product
10/19/1999US5967752 Slant-tier turbine airfoil
10/19/1999US5967745 Gas turbine shroud and platform seal system
10/19/1999US5966927 Efficiency enhanced turbine engine