136864 ⎘
Stators; Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
TURBOMACHINE IMPINGEMENT COOLING MODULES
#2TRANSITION DUCT FOR GAS TURBINE ENGINE
#3COMBUSTOR HAVING SECONDARY FUEL INJECTOR
#4GAS TURBINE ENGINE
#5SEALING DEVICE WITH DISPLACEABLE ABUTMENT
#6Bolted joint of gas turbine engine
#7Fluid ducts including a rib
#8TRANSITION WITH UNEVEN SURFACE
#9Sealing member and gas turbine
#10Gas turbine engine with combustor section mounted modulated compressor air cooling system
#11Subassembly comprising means for compensating for a difference in expansion
#12ACOUSTIC LINER FOR A GAS TURBINE ENGINE
#13Impingement cooling apparatus support structure and method of manufacture
#14Impingement cooling apparatus for turbomachine
#15Gas turbomachine diffuser assembly with radial flow splitters
#16COMPONENT FOR A GAS TURBINE ENGINE
#17GEARED TURBOFAN ARCHITECTURE
#18Turbine stator vane, gas turbine, and method of producing turbine stator vane
#19Transition piece, combustor, and gas turbine engine
#20Transition piece, combustor, and gas turbine engine
#21Combustor assembly with moveable interface dilution opening
#22Combustor for a gas turbine engine
#23High-temperature seal having a clamping profile
#24Gas turbine component with fluid intake hole free of angled surface transitions
#25Component assembly for variable airfoil systems
#26COMPONENT ASSEMBLY FOR A COMBUSTION SECTION OF A GAS TURBINE ENGINE
#27Outlet seal, outlet seal set, and gas turbine
#28Flow channel forming plate, blade and gas turbine including this, and method of manufacturing flow channel forming plate
#29Transition piece, combustor, gas turbine, and gas turbine equipment
#30Methods and assemblies for attaching airfoils within a flow path
#31TURBOMACHINE WITH LOW LEAKAGE SEAL ASSEMBLY FOR COMBUSTOR-TURBINE INTERFACE
#32TURBOMACHINE WITH LOW LEAKAGE SEAL ASSEMBLY FOR COMBUSTOR-TURBINE INTERFACE
#33Method for manufacturing an engine component with a cooling duct arrangement and engine component
#34Transition system side seal for gas turbine engines
#35PRESSURE REGULATED PISTON SEAL FOR A GAS TURBINE COMBUSTOR LINER
#36Cooling system for recuperated gas turbine engines
#37Combustor assembly for a turbine engine
#38Transition Piece Cooling Holes for Gas Turbine Combustor
#39Combustor and gas turbine including the same
#40Ultra compact combustor
#41Liner cooling device, combustor including same, and gas turbine including same
#42Frame for a heat engine
#43Engine components with cooling holes having tailored metering and diffuser portions
#44Turbine nozzle compliant joints and additive methods of manufacturing the same
#45Transition system side seal for gas turbine engines
#46GAS TURBINE COMBUSTOR
#47Seal interface between a transition duct and a stage one vane structure
#48First-stage stator vane for gas turbine, gas turbine, stator vane unit for gas turbine, and combustor assembly
#49Transition piece, combustor provided with same, and gas turbine provided with combustor
#50Support structure for a turbine vane of a gas turbine engine
#51Reverse flow combustor
#52Combustor of gas turbine engine and method
#53Combustor and gas turbine including the same
#54TURBOMACHINE SEALING SYSTEM AND TURBOMACHINE INCLUDING THE SEALING SYSTEM
#55Conformal seal and vane bow wave cooling
#56Combustor with axial fuel staging system and gas turbine having the same
#57Systems and methods for manufacturing film cooling hole diffuser portion
#58Method and apparatus to enhance laminar flow for gas turbine engine components
#59Liner cooling structure with reduced pressure losses and gas turbine combustor having same
#60Pressure regulated piston seal for a gas turbine combustor liner
#61Gas turbine combustor
#62HGP component with effusion cooling element having coolant swirling chamber
#63GAS TURBINE ENGINE, CORRESPONDING SEAL SECTION AND INTEGRATED EXIT PIECE
#64Gas turbine stator vane and gas turbine provided with same
#65Diffuser case assembly
#66Turbine engine airfoil and method
#67Transition piece assembly, transition piece module, and combustor and gas turbine including transition piece assembly
#68COMBUSTION LINER AND GAS TURBINE ENGINE COMPRISING A COMBUSTION LINER
#69Conformal seal and vane bow wave cooling
#70Captured compliant coil seal
#71Cooled component for a gas turbine engine
#72TANGENTIAL ON BOARD INJECTOR NOZZLE WITH A FULL SWEEPING NOZZLE
#73Diffuser-deswirler for a gas turbine engine
#74Film-cooled multi-walled structure with one or more indentations
#75COMBUSTOR SLIDING JOINT
#76Seal assembly with ductile wear liner
#77Turbine blade and gas turbine
#78Turbine scroll assembly for gas turbine engine
#79Combustor assembly for a turbine engine
#80Fin-pin flow guide for efficient transition piece cooling
#81Flange stress-reduction features
#82COMBUSTOR-VANE INTERFACE FEATHER SEAL
#83Retention hardware
#84Blade profile tube nozzle for gas turbine
#85Gas turbine combustor
#86Transition piece
#87System and method for providing compressed air to a gas turbine combustor
#88Method and apparatus for mounting a transition duct in a gas turbine engine
#89Diffuser guide vane with deflector panel having curved profile
#90Ceramic matrix composite turbine vanes and vane ring assemblies
#91Gas turbine including first-stage stator vanes
#92First-stage stationary vane of gas turbine and gas turbine
#93Gas turbine component with platform cooling
#94Method for constructing impingement/effusion cooling features in a component of a combustion turbine engine
#95System with conduit arrangement for dual utilization of cooling fluid in a combustor section of a gas turbine engine
#96Flow control wall for heat engine
#97Cooling hole with shaped meter
#98Unitary flow path structure
#99Gas turbine engine architecture with nested concentric combustor
#100Airfoil fluid curtain to mitigate or prevent flow path leakage
#101REAR OUTER DISCHARGE NOZZLE
#102Methods and assemblies for attaching airfoils within a flow path
#103ANGLED IMPINGEMENT INSERTS WITH COOLING FEATURES
#104COOLING HOLE FOR A GAS TURBINE ENGINE COMPONENT
#105Curved seal with relief cuts for adjacent gas turbine components
#106Support ring with thermal heat shield for case flange
#107Seal assembly with shield for gas turbine engines
#108Seal assembly for gas turbine engine
#109Calcium-magnesium alumino-silicate (CMAS) resistant thermal barrier coatings, systems, and methods of production thereof
#110Combustor with flow guide in double pipe type liner, and gas turbine having same
#111Duct assembly and method of forming
#112Combustor with radially varying leading end portion of basket and gas turbine
#113Converging duct with elongated and hexagonal cooling features
#114Transition piece having cooling rings
#115System and method of measuring turbine vane cooling air consumption during engine operation
#116Inner cooling shroud for transition zone of annular combustor liner
#117Gas turbine combustor and transition piece assembly
#118Methods and features for positioning a flow path assembly within a gas turbine engine
#119Ultra compact combustor
#120Transition duct, turbine, and gas turbine engine
#121Methods and features for positioning a flow path inner boundary within a flow path assembly
#122COMBUSTION CHAMBER ARRANGEMENT
#123Intermediate casing of a turbine engine, provided with a sealing part at the arm/shroud interface
#124Triple bend finger seal and deflection thereof
#125Cooling hole for a gas turbine engine component
#126W501D5/D5A DF42 combustion system
#127Turbine shroud cooling
#128Flow channel for a turbomachine
#129GAS TURBINE ENGINE COMPONENT COOLING PASSAGE AND SPACE EATING CORE
#130Gas turbine engine cooling component
#131Combustor and gas turbine including the same
#132Combustor and gas turbine including the same
#133Aft frame assembly for gas turbine transition piece
#134Aft frame assembly for gas turbine transition piece
#135AFT frame assembly for gas turbine transition piece
#136Combustor and gas turbine including the same
#137ENGINE COMPONENT
#138Conjunction assembly and gas turbine comprising the same
#139Duct assembly including helicoidal structure and gas turbine combustor including the same
#140Transition piece support structure, gas turbine combustor including same, and method of installing same
#141Intersector sealing tab for an aircraft turbine engine
#142Air-collecting structure for enhancing cooling performance for transition piece and gas turbine combustor having same
#143Component for a turbine engine with a cooling hole
#144Conformal seal bow wave cooling
#145Cooling path structure for concentrated cooling of seal area and gas turbine combustor having the same
#146Gas Turbine
#147Conformal seal and vane bow wave cooling
#148DUCTED ENGINE COMPRESSOR BLEED VALVE ARCHITECTURE
#149Turbine engine thrust reverser stop
#150Combustor panel, combustor, combustion device, gas turbine, and method of cooling combustor panel
#151Lobed gas discharge fairing for a turbofan engine
#152Flow path forming plate, vane including this flow path forming plate, gas turbine including this vane, and manufacturing method of flow path forming plate
#153METHOD FOR FORMING A TURBINE COMPONENT
#154Cooling features for a gas turbine engine transition duct
#155Coated turbine component and method for forming a component
#156COATED CERAMIC MATRIX COMPOSITE OF METALLIC COMPONENT AND METHOD FOR FORMING A COMPONENT
#157Coated ceramic matrix composition component and a method for forming a coated ceramic matrix composition component
#158Systems and methods for manufacturing film cooling hole diffuser portion
#159Transition structure
#160Method of making a cooled airfoil assembly for a turbine engine
#161Seal member assembly structure and assembly method, seal member, and gas turbine
#162Interdigitated turbine engine air bearing and method of operation
#163Combustor, gas turbine including the same and method of distributing compressed air in combustor
#164Combustion cylinder, gas turbine combustor, and gas turbine
#165Joint cover with improved manifold block for duct leak detection system
#166Turbomachine coupling assembly
#167COMBUSTOR BASKET COOLING RING
#168Transition duct for a gas turbine engine
#169Gas turbine engine
#170Vane cooling system
#171ULTRA-LOW NOX EMISSION GAS TURBINE ENGINE IN MECHANICAL DRIVE APPLICATIONS
#172SYSTEM AND METHOD FOR ATTACHING A NON-METAL COMPONENT TO A METAL COMPONENT
#173Clad article and method for forming clad article
#174Diffuser-deswirler for a gas turbine engine
#175Combustor pipe, combustor, and gas turbine
#176SYSTEM AND METHOD FOR TRANSITION PIECE SEAL
#177System and method for transition piece seal
#178NON-AXIALLY SYMMETRIC TRANSITION DUCTS FOR COMBUSTORS
#179Component having active cooling and method of fabricating
#180Gas turbine engine vanes
#181Methods for assembling a unitary flow path structure
#182Methods and assemblies for attaching airfoils within a flow path
#183Methods and features for positioning a flow path assembly within a gas turbine engine
#184Flow path assembly with pin supported nozzle airfoils
#185Methods and features for positioning a flow path inner boundary within a flow path assembly
#186Combustor liner panel end rail with curved interface passage for a gas turbine engine combustor
#187Combustor liner panel with non-linear circumferential edge for a gas turbine engine combustor
#188Non-planar combustor liner panel for a gas turbine engine combustor
#189Non-planar combustor liner panel for a gas turbine engine combustor
#190Arrangement for a gas turbine combustion engine
#191COATED COMBUSTOR PANEL SHELL FOR A GAS TURBINE ENGINE COMBUSTOR
#192Apparatus with thermal break
#193Combustion can maintenance apparatus and method
#194Unitary flow path structure
#195Unitary flow path structure
#196Unitary flow path structure
#197Pneumatically-actuated bypass valve
#198Gas turbine combustor transition piece including inclined surface at downstream end portions for reducing pressure fluctuations
#199Gas turbomachine diffuser assembly with radial flow splitters
#200Method and system for ice tolerant bleed takeoff
#201Selective thermal coating of cooling holes with air flow
#202GAS TURBINE TRANSITION DUCT WITH LATE LEAN INJECTION HAVING REDUCED COMBUSTION RESIDENCE TIME
#203COMPONENT HAVING IMPINGEMENT COOLED POCKETS FORMED BY RAISED RIBS AND A COVER SHEET DIFFUSION BONDED TO THE RAISED RIBS
#204Turbine engine assembly with a component having a leading edge trough
#205TRANSITION DUCTS OF A GAS TURBINE COMBUSTOR
#206SELECTIVE THERMAL BARRIER COATING REPAIR
#207Engine door with burst seal
#208Annular wall of a combustion chamber with optimised cooling
#209Flash thermography photobox
#210Combustor seal for a gas turbine engine combustor
#211Turbine center frame having a connecting element
#212TRANSITION DUCT FORMED OF A PLURALITY OF SEGMENTS
#213Combustor device for a gas turbine engine and gas turbine engine incorporating said combustor device
#214Sealing device arrangement at the interface between a combustor and a turbine of a gas turbine and gas turbine with such a sealing arrangement
#215Combustor aft frame cooling
#216Component assembly for a gas turbine engine
#217Clamping device and an associated method thereof
#218Advanced seals with reduced corner leakage
#219Pressure-loaded seals
#220METHOD FOR TREATING COATED ARTICLE AND TREATED ARTICLE
#221Tool kit and method for decoupling cross-fire tube assemblies in gas turbine engines
#222Corner flow reduction seals
#223Gas turbine transition seal with hole through seal plate in groove of nozzle
#224Gas turbine transition duct
#225Combustor cooling panel, transition piece and combustor including the same, and gas turbine including combustor
#226Combustor finger seal
#227Static wear seals for a combustor transition
#228Transition Duct Exit Holder and Inlet Ring Support Arrangement
#229Sealing system for sealing against a non-cylindrical surface
#230Sealing arrangement on combustor to turbine interface in a gas turbine
#231Transition Duct Support Arrangement for a Gas Turbine Engine
#232Ducting arrangement with a ceramic liner for delivering hot-temperature gases in a combustion turbine engine
#233FORMING COOLING PASSAGES IN COMBUSTION TURBINE SUPERALLOY CASTINGS
#234Cooling hole with shaped meter
#235ELECTROSPARK DEPOSITION PROCESS FOR OXIDATION RESISTANT COATING OF COOLING HOLE
#236System and method for gas bearing support of turbine
#237Transition part assembly and combustor including the same
#238GAS TURBINE ENGINE
#239Turbine shroud with abradable layer having dimpled forward zone
#240TRANSITION PIECE, COMBUSTOR PROVIDED WITH SAME, AND GAS TURBINE PROVIDED WITH COMBUSTOR
#241Method and apparatus to enhance laminar flow for gas turbine engine components
#242Assembled turbine housing
#243System and method for sealing flow path components with front-loaded seal
#244Side seal with reduced corner leakage
#245Method and computer-readable model for additively manufacturing ducting arrangement for a gas turbine engine
#246Retention hardware
#247Engine components with cooling holes having tailored metering and diffuser portions
#248Method and Apparatus to Enhance Laminar Flow for Gas Turbine Engine Components
#249Gas turbine engine with an offtake
#250Feeder duct assembly with flexible end fittings
#251TRANSITION DUCT EXIT FRAME WITH INSERT
#252Mounting arrangement for mounting a fluid cooler to a gas turbine engine case
#253Gas turbine engine transition duct and turbine center frame
#254Combustor including a flow guide introduction portion connected to a flow guide main body portion, and a gas turbine
#255Heat shield with axial retention lock
#256Heat shield with axial retention lock
#257Seal member
#258Turboengine, and vane carrier unit for turboengine
#259TURBOMACHINE COMPONENT, PARTICULARLY A GAS TURBINE ENGINE COMPONENT, WITH A COOLED WALL AND A METHOD OF MANUFACTURING
#260Combustor and gas turbine
#261Combustor and gas turbine
#262Seal structure
#263TRANSITION-TO-TURBINE SEAL ASSEMBLY
#264Gas turbine engine having a heat shield
#265Transition duct assembly with late injection features
#266Transition duct assembly
#267Transition duct assembly
#268Transition duct assembly
#269Combustion liner cooling
#270Transition duct support and method to provide a tuned level of support stiffness
#271DUCTING ARRANGEMENT IN A COMBUSTION SYSTEM OF A GAS TURBINE ENGINE
#272Combustor and gas turbine
#273System having layered structure and method of making the same
#274Seal assembly between a transition duct and the first row vane assembly for use in turbine engines
#275MOVABLE INTERFACE FOR GAS TURBINE ENGINE
#276SUPERPLASTIC FABRICATION OF SUPERALLOY COMPONENTS FOR TURBINE ENGINES
#277Transition duct system with arcuate ceramic liner for delivering hot-temperature gases in a combustion turbine engine
#278Impingement cooling arrangement having a snap-in plate
#279Staged fuel and air injection in combustion systems of gas turbines
#280Staged fuel and air injection in combustion systems of gas turbines
#281Systems and methods for assessing strain of components in turbomachines
#282Coating methods
#283Combustor assembly lift systems
#284TRANSITION DUCT SYSTEM WITH A ROBUST CONVERGING FLOW JOINT AT AN INTERSECTION BETWEEN ADJACENT TRANSITIONS EXTENDING BETWEEN A COMBUSTOR AND A TURBINE ASSEMBLY IN A GAS TURBINE ENGINE
#285Cooling device, gas turbine installation provided with same, and method for operating cooling device
#286Converging flow joint insert system at an intersection between adjacent transitions extending between a combustor and a turbine assembly in a gas turbine engine
#287Gas turbine
#288Cooling patch for hot gas path components
#289Converging flow joint insert system at an intersection between adjacent transitions extending between a combustor and a turbine assembly in a gas turbine engine
#290Cylinder for combustor, combustor, and gas turbine
#291Turbine slotted arcuate leaf seal
#292Gas turbine engine with a transition duct and corresponding method of manufacturing a transition duct
#293COATING METHODS AND COATED ARTICLES
#294Gas turbine engine components, blade outer air seal assemblies, and blade outer air seal segments thereof
#295System for sealing between combustors and turbine of gas turbine engine
#296Wear pad system for turbine combustion systems and method for coupling wear pad into turbine combustion system
#297Sealing arrangement for gas turbine transition pieces
#298First stage turbine vane arrangement
#299Gas turbine engine combustor and method of forming same
#300Gas turbine