Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
09/2014
09/18/2014US20140271227 Manufacture of hollow aerofoil
09/18/2014US20140271226 Turbine Blade Tip With Tip Shelf Diffuser Holes
09/18/2014US20140271225 Interior cooling circuits in turbine blades
09/18/2014US20140271221 Usage of a witness mark to distinguish support structure from part
09/18/2014US20140271220 Erosion resistant coating
09/18/2014US20140271219 Molten metal rotor with hardened top
09/18/2014US20140271218 Low conductivity thermal barrier coating
09/18/2014US20140271216 Horizontal axis wind or water turbine with forked or multi-blade upper segments
09/18/2014US20140271215 Systems and Methods of Constructing Composite Assemblies
09/18/2014US20140271214 Amorphous metal rotor blade abrasion strip
09/18/2014US20140271212 Failsafe system for load compensating device
09/18/2014US20140271209 Fiber Orientation to Allow for Automated Ply Placement With Composite Rotor Yokes
09/18/2014US20140271208 Systems and method for a composite blade with fillet transition
09/18/2014US20140271207 Fan blade
09/18/2014US20140271200 Flexing Clevis Arrangement Bolted Joint Attachment For Flexible Rotor Hub With High Offset And High Flapping
09/18/2014US20140271196 Apparatus for propelling fluid, especially for propulsion of a floating vehicle
09/18/2014US20140271190 Wind Turbine Blade having a Conductive Root Bushing
09/18/2014US20140271179 Blade Safety Mechanism for Open Rotor Engine System
09/18/2014US20140271178 Fan Blades for Gas Turbine Engines with Reduced Stress Concentration at Leading Edge
09/18/2014US20140271161 Ceramic matrix composite
09/18/2014US20140271153 Cooled ceramic matrix composite airfoil
09/18/2014US20140271129 Cast-in cooling features especially for turbine airfoils
09/18/2014US20140271120 Disk turbine using heat pipes
09/18/2014US20140271115 Adjustable turbine vane cooling
09/18/2014US20140262524 Downhole turbine motor and related assemblies
09/18/2014US20140261986 Method for making gas turbine engine composite structure
09/18/2014US20140261080 Rare earth silicate environmental barrier coatings
09/18/2014US20140259667 System, kit and method for surface repair and reconditioning of industrial sized fan blades such as incorporated into a cooling tower
09/18/2014US20140259665 Mechanical repair of damaged airfoil structure
09/18/2014DE102014103009A1 Gehäuse mit Kühleinheit für eine Gasturbine Housing with cooling unit for a gas turbine
09/18/2014DE102014103007A1 Kühlkanäle für Turbinenschaufeln einer Gasturbine Cooling channels for turbine blades of a gas turbine
09/18/2014DE102014103005A1 Verfahren und Vorrichtung zur Verbesserung der Wärmeübertragung in Turbinenabschnitten von Gasturbinen A method and apparatus for improving the heat transfer in the turbine sections of gas turbines
09/18/2014DE102014103000A1 Bauteil mit mikrogekühlter laserabgeschiedener Materialschicht und Verfahren zur Herstellung Component with micro-cooled laser deposited material layer and processes for preparing
09/18/2014DE102014100239A1 Systeme und Verfahren für ein Verbundstoffschaufelblatt mit Hohlkehlenübergang Systems and method for a composite blade with fillet transition
09/17/2014EP2778740A2 Photography system
09/17/2014EP2778427A2 Compressor bleed self-recirculating system
09/17/2014EP2778369A1 Impingement cooling mechanism, turbine blade, and combustor
09/17/2014EP2778348A1 Steam turbine
09/17/2014EP2778347A1 Rotor blade assembly, turbomachine comprising a rotor blade assembly and method of assembling a rotor blade assembly
09/17/2014EP2778346A1 Rotors for a gas turbine engine, corresponding gas turbine engine and method
09/17/2014EP2778345A1 Cooled composite sheets for a gas turbine
09/17/2014EP2778344A1 Film cooling structure and turbine wing
09/17/2014EP2778343A1 Compressor stator
09/17/2014EP2778258A1 Erosion resistant coating
09/17/2014EP2778256A1 Methods utilizing cold spray techniques for repairing and protecting rotary components of aviation propulsion systems
09/17/2014EP2778251A1 A maskant for use in aluminizing a turbine component
09/17/2014EP2778249A1 Coating methods and pressurized masking systems for controlling coating microstructures
09/17/2014EP2778241A1 Heat-resistant nickel-based superalloy
09/17/2014EP2778147A2 Calcium-magnesium-aluminosilicate resistant coating and process of forming a calcium-magnesium-aluminosilicate resistant coating
09/17/2014EP2777867A1 Methods for the repair of gas turbine engine components using additive manufacturing techniques
09/17/2014EP2777857A2 Joining methods and temperature controlled fluid treating systems for joining
09/17/2014EP2777827A2 Pressure masking systems and methods for using same in treating techniques
09/17/2014EP2776680A1 Method for making a shaped turbine aerofoil
09/17/2014EP2776679A1 Rotor for a turbomachine
09/17/2014EP2776380A1 High temperature thermal barrier coating
09/16/2014US8834129 Turbofan flow path trenches
09/16/2014US8834128 Tension-torque-transmission element for a fenestron blade and method for producing it
09/16/2014US8834126 Fan blade protection system
09/16/2014US8834125 Hybrid rotor disk assembly with a ceramic matrix composite airfoil for a gas turbine engine
09/16/2014US8834124 Device for attaching hammer clamp blades, associated compressor hub, compressor and turbine engine
09/16/2014US8834123 Turbomachinery component
09/16/2014US8834122 Turbine bucket angel wing features for forward cavity flow control and related method
09/16/2014US8834116 Fluid flow machine with peripheral energization near the suction side
09/16/2014US8834114 Turbine drum rotor retrofit
09/16/2014US8834107 Turbine blade tip shroud for use with a tip clearance control system
09/16/2014US8834104 Vanes for directing exhaust to a turbine wheel
09/16/2014US8834101 Mechanical seal for large pumps
09/16/2014US8834098 Detuned vane airfoil assembly
09/16/2014US8834096 Axial flow gas turbine
09/16/2014CA2612744C Method for making a laser hole in a part made of composite material with ceramic matrix, hole obtained by the method, composite material with ceramic matrix comprising said hole, turboreactor comprising said part
09/16/2014CA2552794C Cooled turbine shroud
09/16/2014CA2536859C Bell-shaped fan cooling holes for turbine airfoil
09/14/2014CA2846376A1 Turbo-machinery rotors with rounded tip edge
09/13/2014CA2841490A1 Blade safety mechanism for open rotor engine system
09/12/2014WO2014138320A1 Gas turbine engine component having variable width feather seal slot
09/12/2014WO2014138108A1 High temperature tolerant ceramic matrix composites and environmental barrier coatings
09/12/2014WO2014137804A1 Long life low cost environmental barrier coating for ceramic matrix composites
09/12/2014WO2014137686A1 Gas turbine engine high lift airfoil cooling in stagnation zone
09/12/2014WO2014137479A1 Gas turbine engine shrouded blades and corresponding methods
09/12/2014WO2014137470A1 Gas turbine engine component arrangement
09/12/2014WO2014137468A1 Gas turbine engine comprising an outboard insertion system of vanes and corresponding assembling method
09/12/2014WO2014137465A1 Gas turbine engine with a clearance control system and corresponding method of operating a gas turbine engine
09/12/2014WO2014137457A1 Method for forming a gas turbine engine composite airfoil assembly and corresponding airfoil assembly
09/12/2014WO2014137448A1 Fan blades with protective sheaths and galvanic shields
09/12/2014WO2014137446A1 Hybrid fan blades for jet engines
09/12/2014WO2014137441A1 Rotor blade and corresponding manufacturing method
09/12/2014WO2014137438A1 Aluminum fan blades with root wear mitigation
09/12/2014WO2014137415A1 Covers for cavities in aircraft fan blades
09/12/2014WO2014137406A1 Disc arrangement, retention system, and method of retaining two separate rotating members of a gas turbine machine
09/12/2014WO2014136235A1 Method for forming aluminide coating film on base
09/12/2014WO2014135354A1 Gas turbine including bellyband seal anti-rotation device
09/12/2014WO2014135345A1 Method for repairing an outer surface of a free-standing wall of a component
09/12/2014WO2014135324A1 Method for new production of a diffuser in a layer system
09/11/2014US20140255652 Surface having specially formed recesses and component
09/11/2014US20140255208 Gas Turbine Blade
09/11/2014US20140255207 Turbine rotor blades having mid-span shrouds
09/11/2014US20140255206 Turbine blade cooling channel formation
09/11/2014US20140255205 Reduced Drag System for Windmills, Fans, Propellers, Airfoils and Hydrofoils
09/11/2014US20140255201 Removable Rotor Blade Tip
09/11/2014US20140255200 Film cooling of turbine blades or vanes
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