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)
10/2002
10/31/2002DE4042729C2 Axial flow turbine for gas turbine engine
10/31/2002DE10120532A1 Vorrichtung und Verfahren zur Befestigung einer Laufschaufel längs einer innerhalb eines Rotors einer axial durchströmten Turbomaschine verlaufenden Umfangsnut Apparatus and method for attaching a blade along a line extending within a rotor of an axial flow turbomachinery circumferential groove
10/30/2002EP1253295A2 Axial-flow turbine having a stepped portion in a flow passage
10/30/2002EP1253293A2 Attaching a rotor blade on a rotor of a turbomachine
10/30/2002EP1253292A2 Methods and systems for cooling gas turbine engine airfoils
10/30/2002EP1253291A1 A turbine blade having a cooled tip shroud
10/30/2002EP1253290A2 Damping rotor assembly vibrations
10/30/2002EP1253289A2 Integrally bladed rotor airfoil fabrication and repair techniques
10/30/2002EP1252424A1 Variable cycle gas turbine engine
10/30/2002EP1252370A1 Chemical cleaning solution for gas turbine blades
10/29/2002US6472018 Diffusion aluminide bondcoat has higher concentration of al and lower concentration of refractory metal at outermost region, abrasion, heat treated to thermally grow a stable alumina layer, ceramic layer; insulation for gas turbine
10/29/2002US6471881 Thermal barrier coating having improved durability and method of providing the coating
10/29/2002US6471485 Rotor with integrated blading
10/29/2002US6471484 Methods and apparatus for damping rotor assembly vibrations
10/29/2002US6471483 Turbine disc
10/29/2002US6471482 Frequency-mistuned light-weight turbomachinery blade rows for increased flutter stability
10/29/2002US6471480 Thin walled cooled hollow tip shroud
10/29/2002US6471479 Turbine airfoil with single aft flowing three pass serpentine cooling circuit
10/29/2002US6471478 Axial seal system for a gas turbine steam-cooled rotor
10/29/2002US6471474 Method and apparatus for reducing rotor assembly circumferential rim stress
10/29/2002US6470568 Method for repairing a gas turbine component
10/24/2002WO2002083985A1 Thermal barrier coating having subsurface inclusions for improved thermal shock resistance
10/24/2002WO2002068716A1 Wear-resistant coating and method for applying it
10/24/2002US20020155316 Oxidation resistance; noncracking
10/24/2002US20020155269 Multilayer; heat resistant exterior; toughness, impact strength interior
10/24/2002US20020155000 Turbine blade or vane
10/24/2002US20020153729 Controllable camber windmill blades
10/24/2002US20020153500 Apparatus and method for focal point control for laser machining
10/24/2002US20020153405 Method of applying braze materials to a substrate
10/24/2002US20020152753 Fuel mixing in a gas turbine engine
10/24/2002DE10207279A1 Gießverfahren und Gussteil Casting and casting
10/24/2002DE10160107A1 Reinigung eines inneren Kanals einer Gasturbinenschaufel Cleaning an interior channel of a gas turbine blade or vane
10/23/2002EP1251243A1 Turbine blade with cooling air baffle
10/23/2002EP1251191A1 A method of repairing a ceramic coating
10/23/2002EP1250516A1 Turbine engine damper
10/23/2002EP1062407B1 Turbine blade assembly with cooling air handling device
10/23/2002EP1007271B1 Gas turbine vane and method for producing a gas turbine vane
10/22/2002WO2002068799A1 Combustion engine, gas turbine, and polishing layer
10/22/2002US6468669 Article having turbulation and method of providing turbulation on an article
10/22/2002US6468367 Superalloy weld composition and repaired turbine engine component
10/22/2002US6468040 Environmentally resistant squealer tips and method for making
10/22/2002US6468032 Further cooling of pre-swirl flow entering cooled rotor aerofoils
10/22/2002US6468031 Nozzle cavity impingement/area reduction insert
10/22/2002US6467339 Method for deploying shroud segments in a turbine engine
10/22/2002US6467272 Means for wear reduction in a gas turbine combustor
10/22/2002US6467168 Method of manufacturing an article by diffusion bonding and superplastic forming
10/22/2002US6467167 Method of producing a lining artefact
10/17/2002WO2002081906A2 Shaped element for aerodynamic or hydrodynamic parts
10/17/2002WO2002081868A1 Gas turbine blade
10/17/2002US20020150474 Thin walled cooled hollow tip shroud
10/17/2002US20020150471 Wide angle guide vane
10/17/2002US20020150470 Gas turbine
10/17/2002US20020150468 Turbine blade or vane and process for producing a turbine blade or vane
10/17/2002US20020150419 Ceramic to metal joint assembly
10/17/2002US20020148817 Laser repair method for nickel base superalloys with high gamma prime content
10/17/2002US20020148589 Ceramic core with locators and method
10/17/2002US20020148488 Method of decoating a turbine blade
10/17/2002US20020148233 Gas turbine
10/17/2002US20020148115 Transient liquid phase bonding repair for advanced turbine blades and vanes
10/17/2002DE10115947A1 Verfahren zur Relativpositionierung von aufeinander folgenden Statoren oder Rotoren einer transsonischen Hochdruckturbine A method for relative positioning of successive stators or rotors of a transonic high-pressure turbine
10/16/2002EP1249591A2 Cooling structure for gas turbines
10/16/2002EP1249581A2 Gas turbine combined plant
10/16/2002EP1249578A1 Cooling of a gas turbine
10/16/2002EP1249576A2 Vibration damper for a gas turbine
10/16/2002EP1249575A1 Turbine vane
10/16/2002EP1249515A2 Yttria-stabilized zirconia with reduced thermal conductivity
10/16/2002EP1249300A1 Laser repair method for nickel base superalloys with high gamma prime content
10/16/2002EP1058772B1 Turbine blade attachment stress reduction rings
10/16/2002CN1092748C Gas turbine airfoil cooling system and method
10/16/2002CN1092747C Compressor impeller apparatus for turbo chargers and its mounting/dismonting apparatus and method
10/15/2002US6465902 Controllable camber windmill blades
10/15/2002US6465090 Protective coating for thermal barrier coatings and coating method therefor
10/15/2002US6464463 Blade locking device with hammer fastener on a disk
10/15/2002US6464462 Gas turbine bucket wall thickness control
10/15/2002US6464461 Steam cooling system for a gas turbine
10/15/2002US6464460 Turbine blade with actively cooled shroud-band element
10/15/2002US6464456 Turbine vane assembly including a low ductility vane
10/15/2002US6464455 Debris trap in a turbine cooling system
10/15/2002US6464453 Turbine interstage sealing ring
10/15/2002US6464128 Braze repair of a gas turbine engine stationary shroud
10/10/2002US20020146584 Process for producing sandwich structures between metallic and nonmetallic materials
10/10/2002US20020146541 Sandwich structure between metallic and non-metallic materials
10/10/2002US20020146322 Vibration damping
10/10/2002US20020146320 Diffuser for a centrifugal compressor
10/10/2002US20020146317 Vapor tube structure of gas turbine
10/10/2002US20020144505 Gas turbine combined plant
10/10/2002DE10117128A1 Verfahren zur Herstellung von Verbundaufbauten zwischen metallischen und nichtmetallischen Materialien A method for producing composite structures between metallic and non-metallic materials
10/10/2002DE10117127A1 Verbundaufbau zwischen metallischen und nichtmetallischen Materialien Composite structure between metallic and non-metallic materials
10/09/2002EP1247941A1 Gas turbine blade
10/09/2002EP1247940A1 Gas turbine stationary blade
10/09/2002EP1247939A1 Turbine blade and process of manufacturing such a blade
10/09/2002EP1247938A2 Clocking of stator- or rotorblades
10/09/2002EP1247937A1 Gas turbine blade and gas turbine
10/09/2002EP1247874A1 Composite construction with metallic and non-metallic materials
10/09/2002EP1247607A2 Connecting part manufacturing method used between metallic and non-metallic materials
10/09/2002EP1247602A1 Method for producing an airfoil
10/09/2002EP1247003A1 Turbine blade and method of repair
10/09/2002EP1246711A1 Method for producing an opening in a metallic structural part
10/08/2002US6461746 Nickel-base superalloy article with rhenium-containing protective layer, and its preparation
10/08/2002US6461110 First-stage high pressure turbine bucket airfoil
1 ... 240 241 242 243 244 245 246 247 248 249 250 251 252 253 254 255 256 257 258 259 260 ... 330