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)
11/2013
11/06/2013EP2660145A1 Propeller blade with lightweight insert
11/06/2013EP2660144A1 Propeller blade with modified spar stiffness.
11/06/2013EP2660003A2 Method of repairing a turbine component
11/06/2013EP2659095A1 Gas turbine engine and cooled flowpath component therefor
11/06/2013EP2659094A1 Rotor with cooling passage
11/06/2013CN203271827U E-class combined cycle three-pressure straight condensing turbine
11/06/2013CN103382857A Gas turbine blade and gas turbine equipped with the same
11/06/2013CN102637233B Parameterized modeling method for turbine blade root extension segment profile
11/06/2013CN102174902B Coated turbine component and method for coating turbine component
11/06/2013CN101970802B Cover for cooling passage, method of manufacturing the cover, and gas turbine
11/06/2013CN101397918B Shim for a blade of a turbomachine
11/06/2013CN101344013B Turbomachine rotor assembly
11/05/2013US8573949 Method and system for focused energy brazing
11/05/2013US8573948 Airfoil
11/05/2013US8573947 Composite fan blade dovetail root
11/05/2013US8573946 Compressor blade
11/05/2013US8573945 Compressor stator vane
11/05/2013US8573944 Anti-wear device of a turbomachine rotor
11/05/2013US8573943 Gas turbine having sealing plates on the turbine disc
11/05/2013US8573941 Tandem blade design
11/05/2013US8573939 Shroud for rotating blades of a turbo machine, and turbo machine
11/05/2013US8573938 Turbine vane with endwall film cooling
11/05/2013US8573936 Blade for turbomachine receiving part, comprising an airfoil part including a mechanical fuse
11/05/2013US8573923 Cooled aerofoil for a gas turbine engine
10/2013
10/31/2013WO2013163150A1 Turbine airfoil with local wall thickness control
10/31/2013WO2013163049A1 Airfoil including loose damper
10/31/2013WO2013163048A1 Airfoil with powder damper
10/31/2013WO2013163047A1 Airfoil including damper member
10/31/2013WO2013163046A1 Airfoil having tapered buttress
10/31/2013WO2013163037A1 Gas turbine engine airfoil impingement cooling
10/31/2013WO2013163032A1 Gas turbine engine airfoil geometries and cores for manufacturing process
10/31/2013WO2013163029A1 Airfoil cooling enhancement and method of making the same
10/31/2013WO2013163020A1 Gas turbine engine core providing exterior airfoil portion
10/31/2013WO2013162946A1 Blade having porous, abradable element
10/31/2013WO2013162928A1 Turbine nozzle outer band and airfoil cooling apparatus
10/31/2013WO2013162900A1 Airfoil including member connected by articulated joint
10/31/2013WO2013162897A1 Turbine hub with surface discontinuity and turbocharger incorporating the same
10/31/2013WO2013162896A1 Turbocharger shroud with cross-wise grooves and turbocharger incorporating the same
10/31/2013WO2013162887A1 Airfoil with break-way, free-floating damper member
10/31/2013WO2013162874A1 Turbocharger blade with contour edge relief and turbocharger incorporating the same
10/31/2013WO2013162866A1 Airfoil support method and apparatus
10/31/2013WO2013162854A1 Durable turbine vane
10/31/2013WO2013162664A2 Turbine blade having improved flutter capability and increased turbine stage output
10/31/2013WO2013160584A1 Fibrous blank woven in one piece by three-dimensional weaving for producing a platform with a closed box structure for a turbomachine fan made of composite material
10/31/2013US20130288072 Alloy, protective layer and component
10/31/2013US20130287590 Generatively produced turbine blade and device and method for producing same
10/31/2013US20130287587 Composite turbine blade and method of manufacture
10/31/2013US20130287586 Propeller blade with lightweight insert and bulkheads
10/31/2013US20130287585 Propeller blade with lightweight insert
10/31/2013US20130287584 Propeller blade with modified spar layup
10/31/2013US20130287582 High efficiency propeller blade with increased pressure side surface
10/31/2013US20130287580 Stress corrosion cracking resistance in superalloys
10/31/2013US20130287579 Blade of a turbomachine, having passive boundary layer control
10/31/2013US20130287578 Blade dovetail bottom
10/31/2013US20130287571 Electrical wiring system for a rotor hub
10/31/2013US20130283820 Hollow fan bladed with braided fabric tubes
10/31/2013DE19811294B4 Gasturbinen-Dichtungssystem zwischen Schaufelumhüllung und -plattform Gas turbine sealing system between the blade enclosure and deck
10/31/2013CA2844741A1 Gas turbine engine sump pressurization system
10/30/2013EP2657452A1 Turbine
10/30/2013EP2657451A2 Turbine shroud cooling assembly for a gas turbine system
10/30/2013EP2657450A2 System and method for reconditioning turbine engines in power generation systems
10/30/2013EP2657449A2 Resistive band for turbomachine blade
10/30/2013EP2655804A1 Pressure compensating wet seal chamber
10/30/2013EP2655005A1 Method for repairing gas turbine components
10/30/2013CN203257487U 320MW steam condensing back-pressure steam turbine
10/30/2013CN103380267A Fan rotor and associated turbojet engine
10/30/2013CN103375186A Turbomachine blade mounting system
10/30/2013CN103375185A Turbomachine blade tip shroud with parallel casing configuration
10/30/2013CN103375184A Resistive band for turbomachine blades
10/30/2013CN103375183A Turbine vibration reduction system
10/30/2013CN103375182A Systems for heating rotor disks in a turbomachine
10/30/2013CN103375181A 涡轮机组件 Turbine assembly
10/30/2013CN103375180A Turbine diaphragm construction
10/30/2013CN103375179A Double-action turbine
10/30/2013CN101910620B Turbine assembly
10/30/2013CN101344014B Airfoil for use in rotary machines and method for fabricating same
10/29/2013US8568101 Fan rotor blade support structure and turbofan engine having the same
10/29/2013US8568100 Bi-axial compliant bearing
10/29/2013US8568097 Turbine blade with core print-out hole
10/29/2013US8568086 Cooling system
10/29/2013US8568085 High pressure turbine vane cooling hole distrubution
10/29/2013US8568082 Blade and a method for making a blade
10/24/2013WO2013158483A1 Trapped spring balance weight and rotor assembly
10/24/2013WO2013158194A1 Turbine airfoil tip shelf and squealer pocket cooling
10/24/2013WO2013156711A1 Method for creating a metal reinforcement with insert for protecting a leading edge made of composite
10/24/2013WO2013156322A1 Guide blade ring for an axial turbomachine and method for designing the guide blade ring
10/24/2013WO2013034857A3 Method for manufacturing a sector of a turbine nozzle or compressor stator vane made of a composite material for a turbine engine, and turbine or compressor including a nozzle or stator vane consisting of said sectors
10/24/2013WO2012059324A3 Method for component testing and for operating a machine
10/24/2013US20130280093 Gas turbine engine core providing exterior airfoil portion
10/24/2013US20130280092 Airfoil cooling enhancement and method of making the same
10/24/2013US20130280091 Gas turbine engine airfoil impingement cooling
10/24/2013US20130280088 Wind turbine component comprising radar-absorbing material
10/24/2013US20130280084 Propeller blade with internal stiffener
10/24/2013US20130280083 Rotor blade arrangement for a turbo machine
10/24/2013US20130280082 Airfoil with powder damper
10/24/2013US20130280079 Propeller blade with metallic foam spar core
10/24/2013US20130280076 Airfoil blade of a bearingless rotor of a helicopter
10/24/2013US20130280069 Ventilation device for generating uniform fluid flows, and a drive unit for a device of said type
10/24/2013US20130280049 Blade having porous, abradable element
10/24/2013US20130280045 Airfoil including damper member
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