Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
04/2008
04/09/2008EP1908921A2 Method for impingement cooling of a turbine airfoil with large platform to airfoil fillet radius, as well as corresponding system and airfoil
04/09/2008EP1908920A2 Guide vane and gas turbine comprising a plurality of these guide vanes
04/09/2008EP1908919A1 Composite vane of a turbomachine with metal reinforcement
04/09/2008EP1907671A1 Gas turbine blade and platform element for a gas-turbine blade ring, supporting structure for fastening it, gas-turbine blade ring and its use
04/09/2008EP1907670A1 Cooled turbine blade for a gas turbine and use of such a turbine blade
04/09/2008EP1907669A1 Cooled turbine blade for a gas turbine and use of such a turbine blade
04/09/2008CN101160452A Locking arrangement for radial entry turbine blades
04/09/2008CN101158292A Ladder type interleaving rib cooling blade suitable for gas-turbine unit
04/09/2008CN101158291A Steam turbine rotor blade
04/09/2008CN101158290A Bucket root platform double wedge shape blocks damping structure of turbine bucket
04/09/2008CN101158289A 涡轮转子以及汽轮机 Turbine rotor and turbine
04/09/2008CN100379946C Rotor insert assembly and method of retrofitting
04/09/2008CN100379942C Airfoil shape for a turbine nozzle
04/09/2008CN100379941C Airfoil shape for a turbine bucket
04/09/2008CN100379940C Fan vane with same shape as its seat
04/09/2008CN100379515C Composite component, manufacturing method thereof and turbine using the same
04/08/2008US7354651 Bond coat for corrosion resistant EBC for silicon-containing substrate and processes for preparing same
04/08/2008US7354249 LP turbine blade airfoil profile
04/08/2008US7354246 Electronics cooling fan with collapsible fan blade
04/08/2008US7354243 Axial compressor blading
04/08/2008US7354242 Variable nozzle for a gas turbine
04/08/2008US7354241 Rotor assembly with cooling air deflectors and method
04/08/2008US7353588 Installation tool for assembling a rotor blade of a gas turbine engine fan assembly
04/03/2008WO2008039224A1 Method and apparatus for geometric rotor stacking and balancing
04/03/2008WO2008038306A2 An improved ceramic integral vanes impeller
04/03/2008WO2008037661A1 Securing apparatus of a turbine blade
04/03/2008WO2008037550A1 Turbine rotor with locking plates and corresponding assembly method
04/03/2008WO2008037236A1 Heat-curing coating composition
04/03/2008US20080080980 Hybrid vapor and film cooled turbine blade
04/03/2008US20080080979 Airfoil cooling circuits and method
04/03/2008US20080080977 Wind turbine rotor blade with acoustic lining
04/03/2008US20080080970 Gas turbine engine vane arrangement
04/03/2008DE102007044727A1 Verfahren und Geräte für die Herstellung von Turbinenantrieben Methods and apparatus for the manufacture of turbine engines
04/03/2008DE102006044706A1 Schichtstruktur und Verfahren zur Herstellung einer Schichtstruktur Layer structure and process for producing a layer structure
04/03/2008DE102006044555A1 Reparaturverfahren Repair method
04/02/2008EP1905963A2 Impeller baffle with air cavity deswirlers
04/02/2008EP1905959A2 Variable pitch wedge retention in vane outer base
04/02/2008EP1905957A1 Locking device of a turbine blade
04/02/2008EP1905956A2 Ceramic matrix composite vane insulator
04/02/2008EP1905955A1 Turbine rotor with locking plates and corresponding assembly method
04/02/2008EP1905954A1 Turbine blade
04/02/2008EP1905953A2 Low plasticity burnishing of coated titanium parts
04/02/2008EP1905952A2 Turbine engine compressor vane and spacer
04/02/2008EP1905951A2 Structual members in a pedestal array
04/02/2008EP1905950A1 Turbine blade
04/02/2008EP1905949A1 Cooling of a steam turbine component
04/02/2008EP1905948A1 Power recovery machine
04/02/2008EP1905852A2 Varying fluence as a function of thickness during laser shock peening
04/02/2008EP1904730A1 Variable nozzle turbocharger
04/02/2008EP1904717A2 Hot gas-conducting housing element, protective shaft jacket, and gas turbine system
04/02/2008EP1904257A1 Method for the production of an armor plating for a blade tip
04/02/2008CN101155973A Component of a steam turbine installation, steam turbine installation, use thereof and method for producing the same
04/02/2008CN101153548A Stationary-rotating assemblies having surface features for enhanced containment of fluid flow, and related processes
04/02/2008CN101153545A Stationary-rotating assemblies having surface features for enhanced containment of fluid flow, and related processes
04/02/2008CN101153544A Ceramic matrix composite vane insulator and its use method
04/02/2008CN101153400A Method for preparing strain tolerant coatings from a green material
04/01/2008US7351482 Ceramic compositions for thermal barrier coatings stabilized in the cubic crystalline phase
04/01/2008US7351039 Compressor rotor blade
04/01/2008US7351038 HP turbine vane airfoil profile
04/01/2008US7351037 Y-connect fastener for ceiling fan blades
04/01/2008US7351036 Turbine airfoil cooling system with elbowed, diffusion film cooling hole
04/01/2008US7351035 Hollow rotor blade for the turbine of a gas turbine engine, the blade being fitted with a “bathtub”
04/01/2008US7350352 Fluid coupling
04/01/2008CA2363306C Process for increasing the life of rotor blade attachments
04/01/2008CA2284363C Thermal barrier coating systems and materials
03/2008
03/27/2008WO2008034739A1 Method for electrochemically coating or stripping the coating from components
03/27/2008WO2008034413A1 Method of repair
03/27/2008US20080075879 metal substrate, metal bonding layer, ceramics thermal barrier; columnar structure of stabilized zirconia, or ZrO2-HfO2 solid solution; simultaneously melting two ZrO2 deposition and Lanthanum oxide deposition materials by electron beam physical vapor deposition; low thermal conductivity; durability
03/27/2008US20080075604 Process For The Electrolytic Treatment Of A Component, And A Component With Through-Hole
03/27/2008US20080075601 Composite turbomachine blade with metal reinforcement
03/27/2008US20080075596 Fan for generating an air flow
03/27/2008US20080075595 Cross Flow Twist Turbine
03/27/2008US20080075593 Apparatus for preventing ice accretion
03/27/2008DE102007042829A1 Hinterschnittener Übergangsradius für Laufschaufelschwalbenschwänze Behind-cut fillet radius for blade dovetails
03/27/2008DE102007039402A1 Hybrid-Keramikmatrixverbund-Turbinenschaufelbaueinheit und dazugehöriges Verfahren Hybrid ceramic matrix composite Turbinenschaufelbaueinheit and associated method
03/27/2008DE102006044416A1 Verfahren zum elektrochemischen Be- oder Entschichten von Bauteilen A method for electrochemical treatment or stripping of components
03/27/2008DE102006043462A1 Aerodynamic component e.g. rotor blade, for use in wind turbine, has pair of surface units on high pressure side engaged between two surface units on low pressure side in main extension direction of trailing edge
03/27/2008DE102006042647A1 Turbine einer Gasturbine Turbine of a gas turbine
03/27/2008CA2633319A1 First stage turbine airfoil
03/27/2008CA2602314A1 Guide vane and method of fabricating the same
03/26/2008EP1903185A2 Thermal and external load isolating impeller shroud
03/26/2008EP1903183A2 Tip ramp turbine blade
03/26/2008EP1903182A2 Rebonding a metallized fabric to an underlying layer
03/26/2008EP1903127A1 Process of manufacturing of workpieces by cold gas spraying and turbine workpiece
03/26/2008EP1902160A1 Ceramic heat insulating layer
03/26/2008CN101148994A 灰孔圆顶叶片 Gray leaf dome hole
03/26/2008CN101148993A Methods and apparatus for fabricating turbine engines
03/26/2008CN100376774C Turbo charge diesel-type piston engine and method for controlling such an engine
03/26/2008CN100376766C Reinforcement and cooling structure of a turbine blade
03/26/2008CN100376765C Three-dimensional sequential effect maximization method for multi-stage turbomachine
03/26/2008CA2603003A1 Composite turbine engine blade with metal reinforcement
03/25/2008US7347672 Rotor disk balancing device, disk fitted with such a device and rotor with such a disk
03/25/2008US7347671 Turbine blade turbulator cooling design
03/25/2008US7347664 High-temperature component for a turbomachine, and a turbomachine
03/25/2008CA2430106C Gas turbine and method of bleeding gas therefrom
03/20/2008WO2008032806A1 Heat resistant member
03/20/2008WO2008031395A1 Turbine of a gas turbine
03/20/2008WO2008031371A1 Method for producing a particle-containing functional layer and functional element comprising such a layer
03/20/2008WO2007141596A3 Turbine nozzle blade airfoil geometry
03/20/2008US20080069959 Thermal barrier composition, a superalloy machine part provided with a coating having such a composition, a ceramic coating, and a method of fabricating the coating