Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
12/2011
12/08/2011US20110299993 Composite structural member with progressive rigidity
12/08/2011US20110299992 Rotor assembly for gas turbine engine
12/08/2011US20110299990 Turbine airfoil with outer wall thickness indicators
12/08/2011US20110299989 Blade union of a turbo machine
12/08/2011US20110299985 Apparatus For Harvesting Energy From A Body Of Water And A Method
12/08/2011US20110296811 Heat transfer arrangement for fluid-washed surfaces
12/08/2011DE102006061448B4 Verfahren zur Herstellung einer Blisk oder eines Blings einer Gasturbine und danach hergestelltes Bauteil A method of manufacturing a blisk of a gas turbine or a bling and then component produced
12/08/2011DE10057187B4 Verfahren für die Herstellung von Verbundaufbauten zwischen metallischen und nichtmetallischen Materialien A process for the production of composite structures between metallic and non-metallic materials
12/08/2011CA2800259A1 Measuring the damage to a turbine-blade thermal barrier
12/07/2011EP2392778A2 Composite gas turbine engine component
12/07/2011EP2392777A2 Heat transfer arrangement for fluid-washed surfaces
12/07/2011EP2392776A2 Fluid transfer arrangement in particular for a gasturbine
12/07/2011EP2392775A1 Blade for use in a fluid flow of a turbine engine and turbine engine
12/07/2011EP2392774A1 Turbine engine airfoil with wrapped leading edge cooling passage
12/07/2011EP2392773A2 Rotor assembly for gas turbine engine
12/07/2011EP2392687A1 Method for manufacturing an oxidation resistant component with improved high temperature strength and corresponding oxidation resistant component with improved high temperature strength
12/07/2011EP2392685A1 Method for manufacturing an oxidation resistant component and corresponding oxidation resistant component
12/07/2011EP2392684A1 Alloy, protective layer and component
12/07/2011EP2391744A2 Coating having thermal and non-thermal coating method
12/07/2011EP1645659B1 Method for repairing machine part, method for forming restored machine part, method for manufacturing machine part, gas turbine engine, electric discharge machine, method for repairing turbine component, and method for forming restored turbine component
12/07/2011CN202065055U Turbocharger
12/07/2011CN202065013U 汽轮机叶片 Turbine blades
12/07/2011CN202065012U 气动螺旋发动机 Pneumatic screw engine
12/07/2011CN101905415B 一种用于盘式周向多根拉杆转子的拉杆液压预紧装置 A plurality of circumferential disc rotor rod rod hydraulic tensioners for
12/07/2011CN101240719B 带有反转高压和低压涡轮的燃气涡轮 With a reverse pressure and low-pressure turbine gas turbine
12/07/2011CN101213353B 涡轮机叶片 Turbine blade
12/06/2011US8070454 Turbine airfoil with trailing edge
12/06/2011US8070451 Modular construction for wind turbine blade
12/06/2011US8070450 High temperature turbine rotor blade
12/06/2011US8070449 Wind turbine
12/06/2011US8070444 Turbine with coaxial sets of blades
12/06/2011US8070443 Turbine blade with leading edge cooling
12/06/2011US8070442 Turbine airfoil with near wall cooling
12/06/2011US8070441 Turbine airfoil with trailing edge cooling channels
12/06/2011US8070440 Cooling channel formed in a wall
12/06/2011US8070438 Fan blade for a gas turbine engine
12/06/2011US8070436 Cooling airflow modulation
12/06/2011US8070432 Static gas turbine component and method for repairing such a component
12/06/2011US8070422 Turbine stator vane and rotor blade arrangement
12/06/2011CA2669202C Method of machining airfoils by disc tools
12/06/2011CA2657264C Method of machining airfoil root fillets
12/06/2011CA2622013C Vane assembly with grommet
12/06/2011CA2528049C Airfoil platform impingement cooling
12/06/2011CA2480393C Impingement cooling of gas turbine blades or vanes
12/06/2011CA2467810C Method of manufacturing a hollow blade for a turbine engine
12/01/2011WO2011148935A1 Vibration damping blade for fluid
12/01/2011WO2011148101A1 Vortex generators for generating vortices upstream of a cascade of compressor blades
12/01/2011WO2011148074A1 Method for machining cavities in a turbomachine turbine disc, turbomachine turbine and milling machine
12/01/2011WO2011147401A1 Blade of a turbomachine, having passive boundary layer control
12/01/2011WO2011124214A3 Guide blade of a turbomachine
12/01/2011WO2010086202A3 Coating having thermal and non-thermal coating method
12/01/2011US20110293438 Pump with axial conduit
12/01/2011US20110293437 Wind turbine blade with a conductively doped coating for lightning protection of the wind turbine blade and method for manufacturing the wind turbine blade
12/01/2011US20110293436 Turbine blade with pressure side stiffening rib
12/01/2011US20110293435 Composite aerofoil
12/01/2011US20110293434 Method of casting a component having interior passageways
12/01/2011US20110293431 Component having varying structures and method for production
12/01/2011US20110293430 Turbine blade walking prevention
12/01/2011US20110293429 Blade fixing design for protecting against low speed rotation induced wear
12/01/2011US20110293428 Method for optimizing the contact surfaces of shroud segments, which abut against one another, of adjacent blades of a gas turbine
12/01/2011US20110293423 Articles which include chevron film cooling holes, and related processes
12/01/2011US20110293422 System and method for enhanced turbine wake mixing via fluidic-generated vortices
12/01/2011US20110293421 Rotor blade having passive bleed path
12/01/2011US20110290942 Electrical power supply and control device for equipment of a rotor, and an aircraft fitted with such a device
12/01/2011US20110289909 Torque converter with asymmetric blade spacing
12/01/2011DE102010021925A1 Schaufel einer Strömungsmaschine mit passiver Grenzschichtbeeinflussung Blade of a turbomachine with passive boundary layer control
12/01/2011DE102008035270A1 Method for cleaning exhaust gases produced from petrol engine, involves coating respective parts of petrol engine and exhaust system of petrol engine with catalyst or catalytically active substances
12/01/2011CA2800074A1 Method for machining cavities in a turbomachine turbine disc, turbomachine turbine and milling machine
12/01/2011CA2798680A1 Vortex generators for generating vortices upstream of a cascade of compressor blades
11/2011
11/30/2011EP2390467A1 Protective coating for reducing drop impact erosion
11/30/2011EP2390466A1 A cooling arrangement for a gas turbine
11/30/2011EP2390465A2 Gas turbine components which include chevron film cooling holes, and related processes
11/30/2011EP2390464A2 Turbine blade with enhanced wake mixing via fluidic-generated vortices
11/30/2011EP2390374A1 Multi-Alloy article, and method of manufacturing thereof
11/30/2011EP2390024A2 Ceramic core tapered trip strips
11/30/2011EP2158062B1 Turbine vane restoration system
11/30/2011CN202055870U 燃气轮机的涡轮转子叶片 Turbine rotor blades of the gas turbine
11/30/2011CN202055869U 一种汽轮机双胞胎动叶片 Twin steam turbine rotor blades
11/30/2011CN202055868U 汽轮机末级动叶片 Last stage turbine rotor blades
11/30/2011CN202055867U 一种汽轮机整体三胞胎调节动叶片 Triplets adjust overall steam turbine rotor blades
11/30/2011CN102265000A 用于连接锤夹叶片、相关的压缩机毂、压缩机和涡轮引擎的装置 Hammer blade clamp used to connect the associated compressor wheel, compressor and turbine engines means
11/30/2011CN102264999A 透平叶片、特别是蒸汽透平的工作叶片及其制造方法 Turbine blades, in particular the work and method of manufacturing the blades of steam turbine
11/30/2011CN102264670A 用于含硅的耐火基底的环境阻挡层 Refractory substrates for silicon barrier environment
11/30/2011CN102261281A 包括人字形薄膜冷却孔的物品与相关工艺 Chevron film cooling holes including the items associated with the process
11/30/2011CN102261266A 防止移动的涡轮机叶片 Preventing movement of the turbine blade
11/30/2011CN101263277B 风轮机叶片 A wind turbine blade
11/29/2011US8066489 Aerofoil assembly
11/29/2011US8066488 Highly slenderness rotor
11/29/2011US8066486 Method and apparatus for vibration-based automatic condition monitoring of a wind turbine
11/29/2011US8066485 Turbine blade with tip section cooling
11/29/2011US8066484 Film cooling hole for a turbine airfoil
11/29/2011US8066483 Turbine airfoil with non-parallel pin fins
11/29/2011US8066482 Shaped cooling holes for reduced stress
11/29/2011US8066479 Non-integral platform and damper for an airfoil
11/29/2011US8066478 Preventing hot-gas ingestion by film-cooling jet via flow-aligned blockers
11/29/2011CA2498144C Blade retention scheme using a retention tab
11/28/2011CA2736838A1 Turbine blade with pressure side stiffening rib
11/25/2011CA2740105A1 Blade fixing design for protecting against low speed rotation induced wear
11/24/2011WO2011145762A1 Counter/contra-rotating device for fluid machinery
11/24/2011WO2011145326A1 Turbine of gas turbine engine
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