145342 ⎘
Manufacture; Heat treatment Hardening; Annealing
Sub-classes:Nacelle inlet assembly with composite lipskin
#2TURBINE COMPONENT WITH A THIN INTERIOR PARTITION
#3High-efficiency epicyclic gear assemblies for turbomachines and method of manufacturing thereof
#4RELIEF VALVE FOR A TURBOCHARGER AND PROCESS FOR MANUFACTURING A RELIEF VALVE
#5Molten metal rotor with hardened blade tips
#6Time lapse shooting apparatus and observation method
#7Method of forming a cure tool and method of forming a textured surface using a cure tool
#8Airfoil with improved coating system and methods of forming the same
#9Method for tight control of bolt holes in fan assembly
#10SLURRY-BASED METHODS FOR FORMING A BOND COAT AND ARTICLES FORMED BY THE METHODS
#11Braze repair of turbomachine engine component
#12Turbine component with a thin interior partition
#13Variable vane mechanism for turbocharger with unison ring and bearing members having independent material characteristics
#14Method for spin forming lipskins
#15Annulus filler
#16Turbocharger
#17Sealing unit for turbocharger
#18NICKEL-BASED SUPERALLOY COMPONENTS AND ADDITIVE MANUFACTURING PROCESSES USING NICKEL-BASED SUPERALLOYS
#19ADDITIVE MANUFACTURING PROCESSES USING NICKEL-BASED SUPERALLOYS
#20Method of treating superalloy articles
#21Method for producing forged TiAl components
#22Turbine Rotor Blade Manufacturing Method
#23Time lapse shooting apparatus and observation method
#24Method for manufacturing components for gas turbine engines
#25METHOD FOR PRODUCING A BLADE FOR A TURBOMACHINE
#26Fan motor
#27METHOD OF FORMING A THERMAL BARRIER COATING
#28Methods for processing bonded dual alloy rotors including differential heat treatment processes
#29PROCESS FOR PRODUCING A BLADE FOR A TURBOMACHINE
#30POWER NOZZLE REPAIR WITH COOLING HARDWARE INSTALLED
#31METHOD FOR PRODUCING A PREFORM FROM AN ALPHA+GAMMA TITANIUM ALUMINIDE ALLOY FOR PRODUCING A COMPONENT WITH HIGH LOAD-BEARING CAPACITY FOR PISTON ENGINES AND GAS TURBINES, IN PARTICULAR AIRCRAFT ENGINES
#32Composite material vane with integrated aerodynamic covering element and manufacturing method thereof
#33NICKEL-BASED SUPERALLOYS AND ADDITIVE MANUFACTURING PROCESSES USING NICKEL-BASED SUPERALLOYS
#34Molten metal rotor with hardened blade tips
#35Method for tight control of bolt holes in fan assembly
#36Wear resistant material, wear resistant impeller and preparation method of wear resistant impeller
#37Process of forming and a seal for an engine
#38Ti—Al-based heat-resistant member
#39Method for producing forged components from a TiAl alloy and component produced thereby
#40CENTRIFUGAL GAS COMPRESSOR WITH A HARDENED SHAFT FOR A BEARING SYSTEM
#41HIGH TEMPERATURE SEAL SYSTEM
#42Method for generating a stress reduction in erected tube walls of a steam generator
#43Method of manufacturing material for rotary machine component, method of manufacturing rotary machine component, material for rotary machine component, rotary machine component, and centrifugal compressor
#44Time lapse shooting apparatus and observation method
#45TREATMENT FOR PREVENTING STRESS CORROSION CRACKING
#46Blade row for the final stage of a steam turbine
#47Method for determining laser shock peening approach accessibility
#48Turbine rotor blade
#49Method and device for the surface peening of a partial element of a component of a gas turbine
#50Method for producing a shaft for compressors
#51Uniform heat treatment process for hardening steel
#52METHOD FOR PRODUCING A WELDED ROTOR OF A LOW-PRESSURE STEAM TURBINE
#53ANNULAR GAS TURBINE ENGINE CASE AND METHOD OF MANUFACTURING
#54Turbine blade for a gas turbine engine
#55Countering laser shock peening induced blade twist
#56Plain bearing between two parts which are movable with respect to each other
#57Cantilevered stator stage