136829 ⎘
Blades; Blade-carrying members ; Heating, heat-insulating, cooling or antivibration means on the blades or the members; Blades; Form or construction; Hollow blades, i.e. blades with cooling or heating channels or cavities ; Heating, heat-insulating or cooling means on blades Liquid cooling
FAN EXIT GUIDE VANE THERMAL MANAGEMENT SYSTEM FOR CONVENTIONAL GAS TURBINE ENGINES
#2GAS TURBINE STATIONARY BLADE AND GAS TURBINE
#3Internal core profile for a turbine nozzle airfoil
#4Trailing edge tip cooling of blade of a gas turbine blade
#5Nozzle assembly with alternating inserted vanes for a turbine engine
#6Engine component with cooling hole
#7Ceramic matrix composite vane with trailing edge radial cooling
#8Turbine airfoil with trailing edge framing features
#9Blade for gas turbine
#10Airfoils including plurality of nozzles and venturi
#11Baffle assembly for gas turbine engine components
#12Enhanced film cooling system
#13Airfoil coupon attachment
#14Turbine bucket with a cooling circuit having an asymmetric root turn
#15Turbine blade or a turbine vane for a gas turbine
#16Aircraft turbo machine exit guide vane comprising a bent lubricant passage of improved design
#17Turbine blade comprising a cooling circuit
#18Turbine shroud cooling
#19Turbine shroud cooling
#20METHOD FOR ADDITIVE MANUFACTURING OF A COMPONENT AND COMPONENT MANUFACTURED BY THAT METHOD
#21Enhanced film cooling system
#22Adaptive cover for cooling pathway by additive manufacture
#23Intermediate case for an aircraft turbomachine comprising a lubricant passage end-piece connected to a case vane by a connection piece
#24Augmentor vane assembly of a gas turbine engine with an additively manufactured augmentor vane
#25Intermediate case for an aircraft turbomachine made from a single casting with a lubricant duct
#26ELECTROSPARK DEPOSITION PROCESS FOR OXIDATION RESISTANT COATING OF COOLING HOLE
#27Cooled component having effusion cooling apertures
#28Turbine engine airfoil with cooling
#29Staged fuel and air injection in combustion systems of gas turbines
#30Staged fuel and air injection in combustion systems of gas turbines
#31Article and manifold for thermal adjustment of a turbine component
#32Gas powered turbine component including serpentine cooling
#33Gas turbine engine airfoil crossover and pedestal rib cooling arrangement
#34Plate for metering flow
#35Method and assembly for reducing secondary heat in a gas turbine engine
#36Electrospark deposition process for oxidation resistant coating of cooling hole
#37TURBULATING COOLING STRUCTURES
#38Tapered thermal barrier coating on convex and concave trailing edge surfaces
#39Gas turbine engine component having surface indicator
#40Rotating turbine component with preferential hole alignment
#41Thermal management article and method of forming the same, and method of thermal management of a substrate
#42Method for manufacturing an airfoil
#43Gas turbine engine component having foam core and composite skin with cooling slot
#44Disk turbine using heat pipes
#45Fuel injection insert for a turbine nozzle segment
#46Fuel-cooled bladed rotor of a gas turbine engine
#47ELECTROSPARK DEPOSITION PROCESS FOR OXIDATION RESISTANT COATING OF COOLING HOLE
#48Axial compressor and associated operating method
#49APPARATUS AND METHOD FOR TURBINE ENGINE COOLING
#50Gas turbine engine rotary injection system and method
#51Vane with enhanced heat transfer
#52Cooling system for a gas turbine
#53Gas turbine engine cooling system and method
#54Integral cooling system for turbine casing and guide vanes in aeroengine
#55Turbine blade cooling hole arrangement