145519 ⎘
Function; Heat transfer, e.g. cooling by the use of microcircuits
HYBRID BONDED CONFIGURATION FOR BLADE OUTER AIR SEAL (BOAS)
#2COOLING METHOD AND APPARATUS USING HOT GAS PATH COMPONENTS INCLUDING AFT END EXHAUST CONDUITS AND AFT END FLANGES
#3Turbine blade for a stationary gas turbine
#4Hourglass airfoil cooling configuration
#5HYBRID BONDED CONFIGURATION FOR BLADE OUTER AIR SEAL (BOAS)
#6Edge detection via window grid normalization
#7Fuel injection for integral combustor and turbine vane
#8High-temperature component and method of producing the high-temperature component
#9Cooling passage configuration
#10Hourglass airfoil cooling configuration
#11OGV electroformed heat exchangers
#12Turbine blade
#13HOT GAS PATH COMPONENTS INCLUDING AFT END EXHAUST CONDUITS AND AFT END FLANGES
#14Fuel injection for integral combustor and turbine vane
#15Hourglass airfoil cooling configuration
#16Cooling passages for gas turbine engine component
#17Turbine tip shroud assembly with plural shroud segments having inter-segment seal arrangement
#18Ceramic matrix composite airfoil cooling
#19Airfoil with cavity lobe adjacent cooling passage network
#20Airfoil with wall that tapers in thickness
#21HGP component with effusion cooling element having coolant swirling chamber
#22Coolant channel
#23Gas engine component with cooling passages in wall and method of making the same
#24Multi-wall deposited thin sheet structure
#25Refractory metal core finishing technique
#26Turbine component and methods of making and cooling a turbine component
#27Dual-walled components for a gas turbine engine
#28Turbine airfoil with multiple walls and internal thermal barrier coating
#29Combustor cap assembly with cooling microchannels
#30Blade outer air seal fin cooling assembly and method
#31System and method for cleaning cooling passages of a combustion chamber
#32Airfoil leading edge cooling channels
#33Turbine component and methods of making and cooling a turbine component
#34Dual-wall airfoil with leading edge cooling slot
#35Microchannel heat exchangers for gas turbine intercooling and condensing
#36Airfoil cooling circuits
#37Turbine blade
#38Cooled fuel injector system for a gas turbine engine and a method for operating the same
#39Turbine shroud block segment with near surface cooling channels
#40Shroud for gas turbine engine
#41Method for forming single crystal components using additive manufacturing and re-melt
#42AIRFOIL HAVING COOLING CIRCUIT
#43Cupped contour for gas turbine engine blade assembly
#44TURBO ENGINE, IN PARTICULAR TURBO GENERATOR AND EXCHANGER FOR SUCH TURBO ENGINE
#45Cooling passage with structural rib and film cooling slot
#46Airfoil with varying wall thickness
#47Gas turbine engine component cooling with resupply of cooling passage
#48Double wall turbine gas turbine engine vane platform cooling configuration with main core resupply
#49Double wall turbine gas turbine engine vane platform cooling configuration with baffle impingement
#50Double wall turbine gas turbine engine vane with discrete opposing skin core cooling configuration
#51Aerofoil and method of manufacture
#52Aerofoil
#53Double wall turbine gas turbine engine blade cooling configuration
#54Double wall turbine gas turbine engine blade cooling configuration
#55Double wall turbine gas turbine engine blade cooling configuration
#56Double wall turbine gas turbine engine blade cooling configuration
#57Double wall turbine gas turbine engine blade cooling configuration
#58Double wall turbine gas turbine engine blade cooling configuration
#59MANAGEMENT OF HEAT CONDUCTION USING PHONONIC REGIONS HAVING NON-METALLIC NANOSTRUCTURES
#60OGV electroformed heat exchangers
#61Aft frame assembly for gas turbine transition piece
#62Turbine blade ring segment, and turbine and gas turbine including the same
#63Aft frame assembly for gas turbine transition piece
#64AFT frame assembly for gas turbine transition piece
#65Liquid bond coatings for barrier coatings
#66Turbine blade having an additive manufacturing trailing edge
#67Engine component with hollow turbulators
#68Interior cooling configurations in turbine blades and methods of manufacture relating thereto
#69Airfoil edge cooling channels
#70TURBINE BLADE COOLING
#71Gas turbine engine component cooling circuit
#72Gas turbine engine with microchannel cooled electric device
#73Turbine engine component with an insert
#74Gaspath component including minicore plenums
#75Turbine tip shroud assembly with plural shroud segments having inter-segment seal arrangement
#76System and method for near wall cooling for turbine component
#77System and method for cleaning cooling passages of a combustion chamber
#78Platform cooling arrangement in a turbine rotor blade
#79Adaptively opening cooling pathway
#80Component for a fluid flow engine and method
#81Adaptively opening backup cooling pathway
#82Gas turbine engine component having vascular engineered lattice structure
#83Component for a gas turbine engine
#84Cooling circuits for a multi-wall blade
#85CMC components having microchannels and methods for forming microchannels in CMC components
#86Turbine vane and gas turbine including the same
#87Method for forming passages in composite components
#88Actively cooled component
#89DRILL TO FLOW MINI CORE
#90Internally cooled engine components
#91Blade for a turbo engine
#92Multi-wall deposited thin sheet structure
#93Integrated casting core-shell structure for making cast component with cooling holes in inaccessible locations
#94Turbine engine components with cooling features
#95Cooling structure for a turbine component
#96Method for making ceramic turbine engine article
#97Dual-wall airfoil with leading edge cooling slot
#98Airfoil leading edge impingement cooling
#99Transition manifolds for cooling channel connections in cooled structures
#100Airfoil cooling circuits
#101Interwoven near surface cooled channels for cooled structures
#102Turbine airfoil trailing edge coolant passage created by cover
#103COMBUSTOR IGNITER COOLING
#104Combustor aft frame cooling
#105Dual-walled components for a gas turbine engine
#106Cast gas turbine engine cooling components
#107Dual walled component for a gas turbine engine
#108Turbine blade trailing edge with low flow framing channel
#109System for removing heat from turbomachinery components
#110Gas turbine engine turbine vane baffle and serpentine cooling passage
#111Turbine vane with coupon having corrugated surface(s)
#112Blade with corrugated outer surface(s)
#113Turbine rotor blade with coupon having corrugated surface(s)
#114Turbomachine component having impingement heat transfer feature, related turbomachine and storage medium
#115Gas engine component with cooling passages in wall
#116Turbine component and methods of making and cooling a turbine component
#117Turbine component and methods of making and cooling a turbine component
#118Turbine component and methods of making and cooling a turbine component
#119Ceramic matrix composite airfoil cooling
#120Airfoil having cooling circuit
#121Airfoil with cooling circuit
#122Airfoil with cooling circuit
#123Airfoil with cooling circuit
#124Engine casing with internal coolant flow patterns
#125Cooled component having effusion cooling apertures
#126Gas turbine engine turbine vane baffle and serpentine cooling passage
#127Cooling device for cooling platforms of a guide vane ring of a gas turbine
#128Article and method of forming an article
#129Fuel heat exchanger with leak management
#130Gas turbine engine component having vascular engineered lattice structure
#131Turbine engine airfoil with cooling
#132Cooled wall of a turbine component and a method for cooling this wall
#133Core component having toroidal structures
#134Axial flowing cooling passages for gas turbine engine components
#135Turbine blade with optimised cooling at the trailing edge of same comprising upstream and downstream ducts and inner side cavities
#136Turbine blade comprising a central cooling duct and two side cavities connected downstream from the central duct
#137Turbine blade with optimised cooling
#138System and method for cooling turbine shroud
#139Segmented micro-channel for improved flow
#140System and method for cooling turbine shroud trailing edge
#141Cooling circuits for a multi-wall blade
#142Baffle insert for a gas turbine engine component and component with baffle insert
#143Multi-chamber platform cooling structures
#144Ceramic matrix composite component and process of producing a ceramic matrix composite component
#145Cylinder for combustor, combustor, and gas turbine
#146Turbine blade
#147Turbine nozzle with cooling channel coolant distribution plenum
#148Turbine nozzle with cooling channel coolant discharge plenum
#149Heat-exchange and noise-reduction panel for a propulsion assembly
#150Blade outer air seal fin cooling assembly and method
#151Cupped contour for gas turbine engine blade assembly
#152Components with microchannel cooling
#153Turbo-engine component having outer wall discharge openings
#154Gas turbine engine component cooling with resupply of cooling passage
#155Hot gas path component having near wall cooling features
#156Hot gas path component cooling system having a particle collection chamber
#157Hot gas path component trailing edge having near wall cooling features
#158Turbine component having surface cooling channels and method of forming same
#159Wall cooling arrangement for a gas turbine engine
#160Gas turbine engine component cooling circuit with respirating pedestal
#161Method for additively constructing internal channels
#162Tortuous cooling passageway for engine component
#163Airfoil with skin core cooling
#164Fan by-pass duct for intercooled turbo fan engines
#165Manufacturing method for a dual wall component
#166Bore-cooled film dispensing pedestals
#167Baffle for gas turbine engine vane
#168Microchannel heat exchangers for gas turbine intercooling and condensing
#169Gas turbine blade with cooling passages
#170Reversible flow blade outer air seal
#171Cooling of engine components
#172Drill to flow mini core
#173Tapered cooling channel for airfoil
#174Leading edge cooling channel for airfoil
#175Dual wall components for gas turbine engines
#176Actively cooled blade outer air seal
#177Components with cooling channels and methods of manufacture
#178Gas turbine system with a transition duct having axially extending cooling channels
#179Gas turbine engine component having shaped pedestals
#180Cooled composite sheets for a gas turbine
#181Gas turbine engine component cooling channels
#182Components with cooling channels and methods of manufacture
#183Gas turbine engine v-shaped film cooling hole
#184Cast component having corner radius to reduce recrystallization
#185Gas turbine engine component external surface micro-channel cooling
#186Multi-airfoil split and rejoin method
#187Gas turbine engine component having surface indicator
#188Blade for a turbomachine
#189Micro jet gas film generation apparatus
#190Gas turbine engine component having vascular engineered lattice structure
#191Gas turbine engine component having vascular engineered lattice structure
#192Gas turbine engine component having vascular engineered lattice structure
#193Cooled fuel injector system for a gas turbine engine and method for operating the same
#194Method for forming a directionally solidified replacement body for a component using additive manufacturing
#195Layered arrangement, hot-gas path component, and process of producing a layered arrangement
#196Repair methods for cooled components
#197Single phase micro/mini channel heat exchangers for gas turbine intercooling
#198Micro channel and methods of manufacturing a micro channel
#199Ceramic matrix composite component and method of forming thereof
#200Turbine endwall with micro-circuit cooling
#201METHODS FOR THE FORMATION OF COOLING CHANNELS, AND RELATED ARTICLES OF MANUFACTURE
#202Methods for the formation and shaping of cooling channels, and related articles of manufacture
#203Hot gas path component with impingement and pedestal cooling
#204Method and system for providing cooling for turbine components
#205Three-dimensional printing process, swirling device and thermal management process
#206Method and system for providing cooling for turbine components
#207Augmented cooling system
#208Dual source cooling air shroud arrangement for a gas turbine engine
#209Shroud arrangement for a gas turbine engine
#210Method for producing a near-surface cooling passage in a thermally highly stressed component, and component having such a passage
#211Repair method of plate member, plate member, combustor, ring segment, and gas turbine
#212Dust mitigation for turbine blade tip turns
#213Turbine blade cooling channel formation
#214Micro-channel coating deposition system and method for using the same
#215Gas turbine engine airfoil with vane platform cooling passage
#216Components with micro cooled coating layer and methods of manufacture
#217COMPONENTS WITH ASYMMETRIC COOLING CHANNELS AND METHODS OF MANUFACTURE
#218Serpentine cooling of nozzle endwall
#219Aerofoil cooling arrangement
#220Gas turbine engine component cooling circuit
#221Airfoil cooling circuits
#222Airfoil
#223Channel marker and related methods
#224Turbine blade root with microcircuit cooling passages
#225Cooling structures in the tips of turbine rotor blades
#226Components with microchannel cooled platforms and fillets and methods of manufacture
#227Turbine engine component wall having branched cooling passages
#228Turbine shroud cooling assembly for a gas turbine system
#229Components with microchannel cooling
#230ROTOR BLADE WITH ONE OR MORE SIDE WALL COOLING CIRCUITS
#231Cooled turbine blade and method for cooling a turbine blade
#232COMPONENTS WITH LASER CLADDING AND METHODS OF MANUFACTURE
#233Bucket assembly for turbine system
#234REPAIR METHODS FOR COOLED COMPONENTS
#235Components with cooling channels and methods of manufacture
#236COMPONENTS WITH COOLING CHANNELS AND METHODS OF MANUFACTURE
#237AIRFOIL WITH NONLINEAR COOLING PASSAGE
#238Components with cooling channels and methods of manufacture
#239Turbine shroud segment cooling system and method
#240Methods of fabricating a coated component using multiple types of fillers
#241Drill to flow mini core
#242Platform with cooling circuit
#243Methods of fabricating and coating a component
#244METHOD OF FABRICATING A COMPONENT USING A FUGITIVE COATING
#245Turbine blades and turbine rotor assemblies
#246Endwall component for a turbine stage of a gas turbine engine
#247Cooling arrangement for a turbine component
#248Turbine airfoil with body microcircuits terminating in platform
#249Branched airfoil core cooling arrangement
#250Serpentine cored airfoil with body microcircuits
#251Microcircuit cooling for blades
#252Modular serpentine cooling systems for turbine engine components
#253Particle resistant in-wall cooling passage inlet
#254Turbine blade
#255Airfoil mini-core plugging devices
#256Turbine component with axially spaced radially flowing microcircuit cooling channels
#257Firm cooling method and hole manufacture
#258Turbine blade cooling system having multiple serpentine trailing edge cooling channels
#259Network cooled coated wall
#260Turbine blade with micro sized near wall cooling channels