136832 ⎘
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; Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
Sub-classes:GAS TURBINE ENGINE VANE OUTER DIAMETER PLATFORM INTEGRATED WITH BLADE OUTER AIR SEAL
#2NOTCHED TURBINE VANE BAFFLE
#3COOLING CIRCUIT FOR A STATOR VANE BRAZE JOINT
#4TURBINE ENGINE WITH A BLADE ASSEMBLY HAVING A SET OF COOLING CONDUITS
#5AIRFOIL ASSEMBLY WITH PLATFORM COOLING
#6GAS TURBINE ENGINE VANE OUTER DIAMETER PLATFORM INTEGRATED WITH BLADE OUTER AIR SEAL
#7TURBOMACHINE VANE PROVIDED WITH A COOLING CIRCUIT AND METHOD FOR LOST-WAX MANUFACTURING OF SUCH A VANE
#8ENGINE COMPONENT WITH A COOLING SUPPLY CIRCUIT
#9AIRFOIL WITH THICK WISHBONE FIBER STRUCTURE
#10COOLING CIRCUIT FOR A STATOR VANE BRAZE JOINT
#11GAS TURBINE ENGINE VANE AND SPAR COMBINATION WITH VARIABLE AIR FLOW PATH
#12PLATFORM FOR STATOR VANE
#13Cooling circuit for a stator vane braze joint
#14Vane Forward Rail for Gas Turbine Engine Assembly
#15Cooling method and structure of vane of gas turbine
#16Components for gas turbine engines
#17Airfoil with rib having connector arms
#18TURBINE COMPONENT WITH A THIN INTERIOR PARTITION
#19Vane with baffle and recessed spar
#20ENGINE COMPONENT ASSEMBLY
#21Impingement jet cooling structure with wavy channel
#22AIRFOIL HAVING CAVITY INSERT TO SEPARATE FLOW
#23Baffle with two datum features
#24Method and casting core for forming a landing for welding a baffle inserted in an airfoil
#25Cast turbine nozzle having heat transfer protrusions on inner surface of leading edge
#26Turbine blade cooling hole for side wall
#27Turbomachine rotor blade with a cooling circuit having an offset rib
#28Turbine nozzle segment and a turbine nozzle comprising such a turbine nozzle segment
#29Triple-walled impingement insert for re-using impingement air in an airfoil, airfoil comprising the impingement insert, turbomachine component and a gas turbine having the same
#30Insert for re-using impingement air in an airfoil, airfoil comprising an impingement insert, turbomachine component and a gas turbine having the same
#31Turbine rotor blade with integral impingement sleeve by additive manufacture
#32Combustion turbine vane cooling system
#33Component having a dirt tolerant passage turn
#34Ceramic airfoil with cooling air turn
#35Ceramic airfoil trailing end configuration
#36Impingement cooling with impingement cells on impinged surface
#37Turbine vane assembly incorporating ceramic matrix composite materials and cooling
#38Multi-flow cooling circuit for gas turbine engine flowpath component
#39Airfoil with rib having connector arms
#40Baffle with two datum features
#41Tip rail cooling insert for turbine blade tip cooling system and related method
#42Brazed in heat transfer feature for cooled turbine components
#43Components for gas turbine engines
#44TURBINE BLADE WITH INTEGRAL FLOW METER
#45Trailing edge pressure and flow regulator
#46Blade for gas turbine
#47Turbine blade and gas turbine
#48AIRCRAFT ROTOR BLADE INSERT
#49Film-cooled multi-walled structure with one or more indentations
#50Component for a turbine engine with a cooling hole
#51Turbine blade with a coupled serpentine channel
#52Turbine blade and gas turbine
#53Airfoils including plurality of nozzles and venturi
#54Baffle assembly for gas turbine engine components
#55Turbine assembly for impingement cooling and method of assembling
#56Airfoil with arced pedestal row
#57Gas turbine engine airfoil with wishbone baffle cooling scheme
#58Divided baffle for components of gas turbine engines
#59Turbine airfoil with multiple walls and internal thermal barrier coating
#60Ceramic Matrix Composite Airfoil Cooling
#61ADDITIVE MANUFACTURED HEAT EXCHANGER
#62Turbine blade having an improved structure
#63Cooling structure for turbine airfoil
#64Leading edge hybrid cavities for airfoils of gas turbine engine
#65Cooling structure for turbine airfoil
#66TURBINE ELEMENT FOR HIGH PRESSURE DROP AND HEAT TRANSFER
#67Trip strips for augmented boundary layer mixing
#68Trip strip configuration for gaspath component in a gas turbine engine
#69Structure for cooling turbine blade
#70Multiple source impingement baffles for gas turbine engine components
#71Aircraft turbo machine exit guide vane comprising a bent lubricant passage of improved design
#72CMC aerofoil
#73Spiral cavities for gas turbine engine components
#74Platform cover plates for gas turbine engine components
#75Turbine vane equipped with insert support
#76Turbine airfoil multilayer exterior wall
#77Turbine component with a thin interior partition
#78Turbine vane including a cooling-air intake portion including a helical element for swirling the cooling air
#79Multiple piece engine component
#80Dual-wall impingement cavity for components of gas turbine engines
#81Segregated cooling air passages for turbine vane
#82Turbine blade comprising a cooling circuit
#83Airfoil with rib communication
#84Gas turbine engine airfoil with cooling path
#85Platform flow turning elements for gas turbine engine components
#86Gas turbine engine components having internal cooling features
#87Gas turbine engine cooling component
#88Gas turbine engine cooling component
#89Shroud for a gas turbine engine
#90Guide vane having a connecting tube
#91Gas turbine engines with improved leading edge airfoil cooling
#92Turbine airfoil with internal cooling channels having flow splitter feature
#93ADDITIVE MANUFACTURING BAFFLES, COVERS, AND DIES
#94Turbine airfoil with turbulating feature on a cold wall
#95Turbine vane having impingement plate for gas turbine and gas turbine including the same
#96Woven skin cores for turbine airfoils
#97Endwall cooling system
#98Turbine airfoil having flow displacement feature with partially sealed radial passages
#99TURBOMACHINE IMPINGEMENT COOLING INSERT
#100HELICAL SKIN COOLING PASSAGES FOR TURBINE AIRFOILS
#101Sliding baffle inserts
#102Turbomachine rotor blade
#103Adaptive cover for cooling pathway by additive manufacture
#104Turbomachine cooling system
#105Turbine engine airfoil insert
#106Method of providing cooling structure for a component
#107Low turn loss baffle flow diverter
#108Outlet guide vane for aircraft turbomachine, with improved lubricant cooling function
#109Internally cooled turbine airfoil with flow displacement feature
#110Thermal isolation structure for rotating turbine frame
#111Composite turbine vane with three-dimensional fiber reinforcements
#112Gas turbine
#113Cooling structure for vane
#114Leading edge hybrid cavities and cores for airfoils of gas turbine engine
#115Gas turbine engine article with panel retained by preloaded compliant member
#116Turbine cooling system
#117Airfoil with sealed baffle
#118Airfoil having panel with geometrically segmented coating
#119Airfoil with laterally insertable baffle
#120Airfoil with airfoil piece having axial seal
#121Airfoil having panels
#122Partially wrapped trailing edge cooling circuit with pressure side serpentine cavities
#123Turbine blade with integral flow meter
#124Flow directing cover for engine component
#125Gas turbine engine component having platform cooling channel
#126Air metering baffle assembly
#127Blade with parallel corrugated surfaces on inner and outer surfaces
#128Cooling system for a gaspath component of a gas powered turbine
#129GAS TURBINE ENGINE COMPONENT
#130Engine component assembly
#131Ceramic matrix composite airfoil cooling
#132Perforated ceramic matrix composite ply, ceramic matrix composite article, and method for forming ceramic matrix composite article
#133HOLLOW BLADE BODY, INSERTION RIB, AND HOLLOW BLADE
#134Blade
#135Internal cooling system with insert forming nearwall cooling channels in midchord cooling cavities of a gas turbine airfoil
#136Internal cooling system with insert forming nearwall cooling channels in an aft cooling cavity of an airfoil usable in a gas turbine engine
#137Rotor wheel and impeller inserts
#138Nozzle segment for a gas turbine engine with ribs defining radially spaced internal cooling channels
#139Turbine airfoil having near-wall cooling insert
#140Air shredder insert
#141Airfoil having impingement openings
#142Accelerator insert for a gas turbine engine airfoil
#143Cooling concept for turbine blades or vanes
#144Airfoil for a gas turbine engine
#145Modulated turbine vane cooling
#146Turbine vane, turbine, and turbine vane modification method
#147Turbine blade comprising a central cooling duct and two side cavities connected downstream from the central duct
#148Gas turbine engine airfoil cooling circuit arrangement
#149Method and apparatus for cooling gas turbine engine component
#150Baffle insert for a gas turbine engine component and method of cooling
#151Baffle insert for a gas turbine engine component and component with baffle insert
#152Baffle insert for a gas turbine engine component
#153Gas turbine engine component with a baffle insert
#154Gas turbine engine with fillet film holes
#155Cooled turbine runner, in particular for an aircraft engine
#156Turbine airfoil internal core profile
#157Article and method of cooling an article
#158Airfoil cooling with internal cavity displacement features
#159TURBINE AIRFOIL COOLING SYSTEM WITH LEADING EDGE IMPINGEMENT COOLING SYSTEM AND NEARWALL IMPINGEMENT SYSTEM
#160Article, component, and method of forming an article
#161Article and method of forming an article
#162Article and method of forming an article
#163Using inserts to balance heat transfer and stress in high temperature alloys
#164Airfoil baffle with wedge region
#165Low turn loss baffle flow diverter
#166Partial cavity baffles for airfoils in gas turbine engines
#167Article, airfoil component and method for forming article
#168Turbine with cooled turbine guide vanes
#169Gas turbine blade
#170Turbine blade
#171Low loss baffled serpentine turns
#172Hot gas path component having near wall cooling features
#173Hot gas path component cooling system having a particle collection chamber
#174Heat shield for a vane assembly of a gas turbine engine
#175CMC airfoil with cooling channels
#176Method and casting core for forming a landing for welding a baffle inserted in an airfoil
#177Flow directing cover for engine component
#178Thermal shielding in a gas turbine
#179Thermal shielding in a gas turbine
#180Film cooled multi-walled structure with one or more indentations
#181Multiple piece engine component
#182Baffle inserts
#183Gas powered turbine component including serpentine cooling
#184Incident tolerant turbine vane cooling
#185Gas turbine engine component having platform cooling channel
#186Trip strip restagger
#187Gas turbine engine airfoil with wishbone baffle cooling scheme
#188Sliding baffle inserts
#189Vane, gas turbine provided with the same, method of manufacturing vane, and method of remodeling vane
#190Cooling having tailored flow resistance
#191Turbomachine blade, comprising intersecting partitions for circulation of air in the direction of the trailing edge
#192Cooled component
#193Gas turbine engines with improved leading edge airfoil cooling
#194Gas turbine engine component having trip strips
#195Internal cooling of engine components
#196Plate for metering flow
#197Gas turbine nozzles with embossments in airfoil cavities
#198Turbine blades and methods of forming turbine blades having lifted rib turbulator structures
#199Additive manufacturing baffles, covers, and dies
#200Gas turbine engine airfoil leading edge cooling
#201Blade for a turbomachine
#202Gas turbine engine component having contoured rib end
#203Angled impingement insert
#204Fastback vorticor pin
#205Gas path components of gas turbine engines and methods for cooling the same using porous medium cooling systems
#206Insulating coating to permit higher operating temperatures
#207Method of reducing manufacturing variation related to blocked cooling holes
#208Enclosed baffle for a turbine engine component
#209Turbine vane with cooled fillet
#210INTERNAL COOLING SYSTEM WITH CORRUGATED INSERT FORMING NEARWALL COOLING CHANNELS FOR AIRFOIL USABLE IN A GAS TURBINE ENGINE
#211Structural configurations and cooling circuits in turbine blades
#212Turbine airfoil with an internal cooling system having trip strips with reduced pressure drop
#213Structural configurations and cooling circuits in turbine blades
#214Structural configurations and cooling circuits in turbine blades
#215Structural configurations and cooling circuits in turbine blades
#216Interior cooling circuits in turbine blades
#217Structural configurations and cooling circuits in turbine blades
#218TURBINE AIRFOIL COOLING PASSAGE WITH DIAMOND TURBULATOR
#219Modified turbine components with internally cooled supplemental elements and methods for making the same
#220Turbine airfoil with laterally extending snubber having internal cooling system
#221Gas turbine engine airfoil trailing edge passage and core for making same
#222Hot gas path component with impingement and pedestal cooling
#223Impingement cooling of turbine blades or vanes
#224Turbine guide vane with a throttle element
#225Pin-fin array
#226Airfoil cooling circuit
#227Method and apparatus for cooling gas turbine and rotor blades
#228Cooling system including wavy cooling chamber in a trailing edge portion of an airfoil assembly
#229Dust mitigation for turbine blade tip turns
#230Turbine airfoil assembly
#231Modulated turbine vane cooling
#232GAS TURBINE ENGINE SERPENTINE COOLING PASSAGE
#233Impingement cooling of turbine blades or vanes
#234Gas turbine engine serpentine cooling passage with chevrons
#235Cooling hole cleaning method and apparatus
#236Trailing edge and tip cooling
#237Aerofoil cooling
#238Turbine nozzle having non-linear cooling conduit
#239Turbine airfoil vane with an impingement insert having a plurality of impingement nozzles
#240GAS TURBINE ENGINE COMPONENT
#241Cooled turbine blade with leading edge flow redirection and diffusion
#242GAS TURBINE ENGINE COMPONENT
#243Turbine blade of a gas turbine with swirl-generating element and method for its manufacture
#244Gas turbine engine airfoil cooling circuit arrangement
#245Gas turbine engine component having platform cooling channel
#246Cooled component for the turbine of a gas turbine engine
#247Turbine vane
#248Passive thermostatic valve
#249TURBINE AIRFOIL TRAILING EDGE COOLING HOLE PLUG AND SLOT
#250Gas turbine engine airfoil with dirt purge feature and core for making same
#251Cooling assembly for a gas turbine system
#252Turbine cooling apparatus
#253Airfoil with improved internal cooling channel pedestals
#254Tapered thermal coating for airfoil
#255Turbine nozzle assembly methods
#256Turbine nozzle compartmentalized cooling system
#257Turbine rotor blade platform cooling
#258PIN-FIN ARRAY
#259WORKING A VANE ASSEMBLY FOR A GAS TURBINE ENGINE
#260Cooled airfoil in a turbine engine
#261Methods of fabricating a coated component using multiple types of fillers
#262Turbine blade and gas turbine
#263Integrated axial and tangential serpentine cooling circuit in a turbine airfoil
#264Turbine blade
#265TURBINE AIRFOIL VANE WITH AN IMPINGEMENT INSERT HAVING A PLURALITY OF IMPINGEMENT NOZZLES
#266AEROFOIL, AN AEROFOIL SUB-ASSEMBLY AND A METHOD OF MAKING THE SAME
#267Fluid transfer arrangement
#268Branched airfoil core cooling arrangement
#269Turbine blade with shielded tip coolant supply passageway
#270Turbine blade structure
#271Cooling system
#272Turbine vane for a stationary gas turbine
#273Gas turbine vane with improved cooling
#274Turbine blade with incremental serpentine cooling channels beneath a thermal skin
#275Turbine vane for gas turbine engine
#276Turbine blade cooling with a hollow airfoil configured to minimize a distance between a pin array section and the trailing edge of the air foil
#277Turbine blade
#278Cooled gas turbine vane assembly
#279Serpentine Microcircuit Vortex Turbulators for Blade Cooling
#280Aerofoil cooling arrangement
#281Aerofoil and method for making an aerofoil
#282Eccentric chamfer at inlet of branches in a flow channel
#283Turbine airfoil with near wall inflow chambers
#284Turbine airfoil with controlled area cooling arrangement
#285Chambered airfoil cooling
#286Radial split serpentine microcircuits
#287CMC vane insulator and method of use
#288Radial inner diameter metering plate
#289Dust hole dome blade
#290Cooling circuit flow path for a turbine section airfoil
#291Cooled turbine blade for a gas turbine and use of such a turbine blade
#292Reinforced airfoils
#293Blade for a gas turbine engine
#294Coated turbine blade
#295Insertable impingement rib
#296Turbine blade trip strip orientation
#297Air-cooled component
#298Airfoil with customized convective cooling
#299Integrated platform, tip, and main body microcircuits for turbine blades
#300Serpentine microcircuit vortex turbulatons for blade cooling