136845 ⎘
Blades; Blade-carrying members ; Heating, heat-insulating, cooling or antivibration means on the blades or the members; Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
Sub-classes:GAS TURBINE
#2TURBINE ENGINE WITH A BLADE ASSEMBLY HAVING COOLING CONDUITS
#3TURBINE ENGINE WITH A BLADE ASSEMBLY HAVING A DOVETAIL
#4TURBINE ENGINE WITH A BLADE ASSEMBLY HAVING A DOVETAIL
#5TURBINE ENGINE WITH A BLADE ASSEMBLY HAVING A DOVETAIL
#6TURBINE ENGINE WITH A BLADE ASSEMBLY HAVING A DOVETAIL
#7Turbine Engine Rotor Blade With Contoured Pocket Surface(S)
#8TURBINE ROTOR DOVETAIL STRUCTURE WITH SPLINES
#9HIGH PRESSURE TURBINE BLADE DOUBLE SCARF CUT
#10VARIABLE RIM WIDTH TURBINE BLADE ATTACHMENT
#11ROTOR DISK, ROTOR, AND METHOD FOR SERVICING A ROTOR DISK
#12TURBINE ENGINE HAVING A ROTATABLE DISK AND A BLADE
#13METHOD FOR MANUFACTURING A COMPOSITE BLADED DISK OR ROTOR
#14SYSTEM AND METHOD FOR ULTRASONIC PHASED ARRAY INSPECTION OF INTEGRAL SHROUD DRUM STAGE T-ROOT BLADES
#15Rotor assembly having protective core and gas turbine engine comprising same
#16Control of leakage for gas turbine engine compressor blades
#17TURBINE ROTOR AND PLATFORM FOR SUCH A ROTOR
#18TURBINE ROTOR COMPRISING A BLADE STOP RING CONFIGURED TO AID THE COOLING OF THE BLADE ROOTS
#19ASSEMBLY COMPRISING A FOIL MOUNTED ON A DISC OF A MOVING WHEEL
#20ANNULUS FILLER FOR A GAS TURBINE ENGINE
#21Turbine rotor dovetail structure with splines
#22Methods and apparatuses for blade locking
#23GAS TURBINE ENGINE WITH CLUTCH ASSEMBLY
#24BLADE SPACER
#25PROPULSION SYSTEM AND METHOD FOR OPERATION
#26FAN ASSEMBLIES WITH FAN DISK INSERTS AND METHODS OF ASSEMBLING THE SAME
#27MOVING BLADE FOR A TURBINE OF A TURBINE ENGINE, COMPRISING A STILT EQUIPPED WITH PROJECTIONS FOR RADIALLY RETAINING THE BLADE
#28BLADE FOR A ROTOR ASSEMBLY OF A TURBINE ENGINE
#29FOIL FOR A TURBINE ENGINE MOVING BLADE AND ROTOR ASSEMBLY COMPRISING SUCH A FOIL
#30TANDEM BLADE ROTOR DISK
#31Turbine airfoil attachment with serration profile
#32FOIL, ROTOR BLADE, ASSEMBLY FOR A TURBOMACHINE ROTOR AND ROTOR
#33ROTOR DISK, TURBINE BLADE, AND TURBINE BLADE ASSEMBLY EQUIPPED WITH THESE
#34T-fairing installation tooling assembly
#35Turbine engine including a composite airfoil assembly having a dovetail portion
#36COMPOSITE AIRFOIL ASSEMBLY HAVING A DOVETAIL PORTION
#37TURBINE ENGINE WITH A BLADE ASSEMBLY HAVING A DOVETAIL
#38FAN ASSEMBLY HAVING A FAN RETENTION MEMBER FOR SUPPORTING A BLADE PLATFORM
#39Rotor wheel for an aircraft turbine engine
#40ASSEMBLY FOR A TURBOMACHINE BLADE, COMPRISING A FASTENER, DEFINING A POCKET, AND A SHIM ADAPTED TO BE RECEIVED IN THE POCKET AT THE SAME TIME AS A ROOT OF THE BLADE
#41SYSTÈME PROPULSIF AÉRONAUTIQUE
#42AERONAUTICAL PROPULSION SYSTEM
#43Blade and slotted rotor wheel for a gas turbine engine
#44Blade and slotted rotor wheel for a gas turbine engine
#45Composite airfoil assembly having a dovetail portion
#46Aeronautical propulsion system
#47Aeronautical propulsion system
#48Fixing structure for turbine rotor blade
#49Machinable coating for CMC and metal interface in a turbine section
#50ASSEMBLY FOR A TURBOMACHINE BLADE, COMPRISING A FASTENER, DEFINING A POCKET, AND A SHIM ADAPTED TO BE RECEIVED IN THE POCKET AT THE SAME TIME AS A ROOT OF THE BLADE
#51Platform for an airfoil of a gas turbine engine
#52Method and system for protecting a rotatable shaft of a motor from excessive bending moments
#53Rotor with feather seals
#54TURBINE BLADE TIP COOLING HOLE SUPPLY PLENUM
#55Rotor blade and rotor blade assembly for a turbomachine
#56Blade with tip rail cooling
#57ADVANCE RATIO FOR SINGLE UNDUCTED ROTOR ENGINE
#58T-fairing installation tooling assembly
#59Airfoil ribs for rotor blades
#60Turbine rotor blade, turbine rotor blade assembly, gas turbine, and repair method for gas turbine
#61ROTOR BLADE FOR A GAS TURBINE
#62Rotor arrangement for a rotor of a gas turbine
#63Structure for assembling turbine blade seals and gas turbine including the same
#64T-fairing installation tooling assembly
#65Airfoil attachment for turbine rotor
#66System for protecting a rotatable shaft of a motor from excessive bending moments
#67BLADED DISC
#68Method for providing a gas turbine blade and rotor wear-protection system
#69DOVETAILED COMPOSITE OUTLET GUIDE VANE ASSEMBLY AND METHOD OF ASSEMBLING THEREOF
#70Turbine blade, and turbine and gas turbine including the same
#71Turbine rotor for a turbomachine and method for mounting the rotor
#72Low radius ratio fan blade for a gas turbine engine
#73Fan rotor with variable pitch blades and turbomachine equipped with such a rotor
#74Rotor for a turbomachine and turbomachine
#75BLADED DISC
#76Tandem blade rotor disk
#77Turbine blade and turbine
#78Glass viscous damper
#79Method for giving shroud interference to axial-entry blades in a rotary machine and rotary machine
#80A FIXING APPARATUS
#81Device for detecting cooling abnormalities for an aircraft turbine engine
#82Blade intake
#83Blade root receptacle for receiving a rotor blade
#84System with a rotor blade for a gas turbine with a blade root protective plate having a sealing section
#85Blade for a turbo machine, blade assembly, gas turbine, and method for manufacturing a blade for a turbo machine
#86Wrought root blade manufacture methods
#87Turbomachine moving blade with cooling circuit having a double row of discharge slots
#88Turbine blade tip cooling hole supply plenum
#89Rotor blade retention system for a gas turbine engine
#90Turbine rotor blade
#91Intermediate element for a blade/rotor disc connection in a rotor of a turbomachine, associated rotor for a turbomachine, and turbomachine
#92Ring fastener
#93Rotor blade with blade root contour having a straight portion provided in a concave contour portion
#94Turbine vane provided with a recess for embrittlement of a frangible section
#95Rotor and compressor
#96Airfoil tip rail and method of cooling
#97Airfoil attachment for turbine rotor
#98Rotor damping devices for a turbomachine
#99ROTOR DISK AND ROTOR BLADE FOR A GAS TURBINE COMPRESSOR OR TURBINE STAGE OF AN AEROENGINE
#100Gas turbine engine fan
#101Gas turbine blade and rotor wear-protection system
#102Device for attaching blades in a contra-rotating turbine
#103Turbomachine fan rotor
#104Tandem blade rotor disk
#105Production method for a component having integrated channels and component
#106Blade dovetail and retention apparatus
#107Rotor and turbo machine including same
#108Blade dovetail and retention apparatus
#109Blade dovetail and retention apparatus
#110WOUND RETAINING WIRE
#111Turbomachine assembly comprising fan blades with an extended trailing edge
#112Bladed rotor system and corresponding method of servicing
#113Blade with tip rail, cooling
#114Turbomachine rotor assembly
#115Layered fuselage shield
#116Rotor assembly
#117Rotor blade and disc of rotating body
#118Turbine blade cooling hole for side wall
#119Rotor comprising a rotor component arranged between two rotor disks
#120Composite fan blade root
#121Impeller and method of manufacturing the same
#122Holding system for the dismantling of a blade wheel
#123Turbine wheel
#124Extended root region and platform over-wrap for a blade of a gas turbine engine
#125Blade coupling structure and turbine system having the same
#126Gas turbine engine with clutch assembly
#127Gas turbine engine outlet guide vane assembly
#128Dovetail slot for use with rotor assemblies
#129Rotor assembly with internal vanes
#130Rotor assembly with internal vanes
#131Multi-disk bladed rotor assembly for rotational equipment
#132Trunnion retention for a turbine engine
#133Method of manufacturing a rotor disc for a turbine engine
#134Turbmachine fan disc
#135Damper stacks for turbomachine rotor blades
#136Pre-formed faceted turbine blade damper seal
#137Composite turbine disc rotor for turbomachine
#138System and method for control for unducted engine
#139Blade retention features for turbomachines
#140Mount for an airfoil
#141Rotor with centrifugally optimized contact faces
#142Flared fan hub slot
#143Fan blade attachment root with improved strain response
#144Composite blade and method for molding composite blade
#145Tandem blade rotor disk
#146Rotor with sealing element and ring seal
#147Multi-blade vane for a turbomachine rotor and rotor comprising same
#148Cooled attachment sleeve for a ceramic matrix composite rotor blade
#149TURBINE WHEEL ASSEMBLY WITH CERAMIC MATRIX COMPOSITE BLADES
#150Blade with tip rail cooling
#151BLADE FOR A GAS TURBINE ENGINE
#152Gas turbine rotor disk having scallop shield feature
#153Hybrid rotor blades for turbine engines
#154Turbine blade with ceramic matrix composite aerofoil and metallic root
#155Apparatus for circumferential separation of turbine blades
#156Airfoil tip rail and method of cooling
#157Turbine engine component and method of cooling
#158Method of forming an additively manufactured component
#159Fan comprising an inter-blade platform attached upstream by a ferrule
#160Rotor assembly with blade sealing tab
#161Turbine blade with radial support, shim and related turbine rotor
#162Turbine blade with radial support, shim and related turbine rotor
#163Turbine disk
#164TURBINE BLADE ASSEMBLY
#165Turbomachine blade
#166Rotor assembly with rotor disc lip
#167Turbine wheel assembly with offloaded platforms and ceramic matrix composite blades
#168Turbine blade of gas turbine having cast tip
#169Wrought root blade manufacture methods
#170System for protecting a rotatable shaft of a motor from excessive bending moments
#171Gas turbine engine with dove-tailed TOBI vane
#172Turbine blade comprising ceramic matrix composite materials
#173Second stage turbine blade
#174Variable pitch blade holder for gas turbine engine
#175Turbine, gas turbine, and method of disassembling turbine blades
#176Dovetail weight system for rotor balance
#177Fan blade attachment root with improved strain response
#178Turbine blade cooling system with channel transition
#179Fan platform wedge seal
#180Turbine wheel assembly with ceramic matrix composite blades
#181BLADE FOR A GAS TURBINE ENGINE
#182GAS TURBINE
#183Blisk bonded CMC airfoil having attachment
#184Method for producing a base body of a turbine blade
#185Method for measuring pre-twist amount of blade, and method for manufacturing rotor
#186TURBINE BLADE WITH ATTACHMENT-SUPPORTED PLATFORM FOR COMPOSITE MATERIAL CONSTRUCTION
#187Seal assembly with shield for gas turbine engines
#188Turbine disk with platforms coupled to disk
#189Platform for an airfoil of a gas turbine engine
#190Blade with inlet orifice on aft face of root
#191Seal assembly for gas turbine engine
#192Turbine disk with pinned platforms
#193COMPOSITE BLADE AND METHOD OF MANUFACTURING COMPOSITE BLADE
#194Method for disassembling/assembling gas turbine, seal plate assembly, and gas turbine rotor
#195Turbine blade assembly with mounted platform
#196Compressor rotor cooling apparatus
#197Method for disassembling/assembling gas turbine, gas turbine rotor, and gas turbine
#198Platform apparatus for propulsion rotor
#199Turbine rotor blade assembly
#200FAN DISC ASSEMBLY
#201FAN DISC ASSEMBLY
#202FAN DISC ASSEMBLY
#203Blade for a gas turbine engine
#204TURBINE ROTOR DISC HAVING MULTIPLE RIMS
#205Damping device
#206Machining device and method for machining a rotor arranged in a turbine housing which consists of two parts, thereby forming a joint, and method for repairing and/or retrofitting a turbine
#207Turbine blade cooling system with tip flag transition
#208Turbine blade cooling system with tip diffuser
#209Turbine blade cooling system with lower turning vane bank
#210Turbine blade cooling system with upper turning vane bank
#211Turbo engine rotor disc
#212Sealing system for a rotary machine and method of assembling same
#213System for rotating a fan of a turbojet engine
#214Steam turbine
#215Annulus filler
#216Modified J type cantilevered vane and gas turbine having the same
#217Connection assemblies between turbine rotor blades and rotor wheels
#218Compressor and gas turbine including the same
#219Rotor having improved structure, and turbine and gas turbine including the same
#220APPARATUS FOR CIRCUMFERENTIAL SEPARATION OF TURBINE BLADES
#221Trunnion retention for a turbine engine
#222Seal structure for gas turbine rotor blade
#223Turbine blade, turbine including same turbine blade, and gas turbine including same turbine
#224Contact interface for a composite component and methods of fabrication
#225Compressor rotor disk for gas turbine
#226Turbine blade axial retention and sealing system
#227Turbine rotor blade assembly
#228Turbine disk
#229Turbine disk
#230Knife-edge fastening with seal for a straightener blade
#231Turbine for a turbine engine
#232Turbine blade having an additive manufacturing trailing edge
#233Entrance and exit chip rings for balancing broach forces
#234Flexible damper for turbine blades
#235Blade with tip rail cooling
#236Rotary machines including a hybrid rotor with hollow and solid rotor blade sets
#237Turbine blade damper seal
#238Method and drive-out device for driving out a blade
#239Method for removing turbine blade, removal device for executing said method, and rotor set with said removal device
#240Methods and devices for turbine blade installation alignment
#241Ceramic matrix composite (CMC) blade and method of making a CMC blade
#242Ceramic matrix composite (CMC) turbine blades and methods of forming CMC turbine blades
#243Cantilevered vane and gas turbine including the same
#244Fastener cover for flowpath fasteners
#245Turbine wheel with clamped blade attachment
#246Vane ring assembly and compressor and gas turbine including the same
#247ROTOR DISK ASSEMBLY FOR A GAS TURBINE ENGINE
#248Ceramic matrix composite (CMC) turbine blade assembly, dovetail sleeve, and method of mounting CMC turbine blade
#249Composite blade and method of manufacture
#250Blade made of composite material with integrated platform for an aircraft turbine engine
#251Rotor blade tip
#252Wear-resistant shield for a rotating blade of a gas turbine
#253Airfoil platform cooling channels
#254GAS TURBINE BLADE ASSEMBLY HAVING RETAINER ASSEMBLING STRUCTURE, AND GAS TURBINE HAVING SAME
#255ENGINE COMPONENT WITH REPLACEABLE TIP ELEMENT
#256Retainer for gas turbine blade, turbine unit and gas turbine using the same
#257Tools and methods for cleaning grooves of a turbine rotor disc
#258Device for cooling a turbomachine rotor
#259Apparatus for axial locking of bucket and bucket assembly and gas turbine having the same
#260ENVIRONMENTAL SEVERITY MEASUREMENT TOOL
#261Thermal shielding in a gas turbine
#262Fan
#263Turbine blades having shank features
#264Turbine blade with ceramic matrix composite material construction
#265Damping inserts and methods for shrouded turbine blades
#266Staking tool
#267Enhanced superalloys by zirconium addition
#268Thermal shielding in a gas turbine
#269BLADE PLATFORM WITH CHAMFER
#270Gas turbine
#271Turbine blade and locking set
#272THREE-DIMENSIONALLY WOVEN CERAMIC MATRIX COMPOSITE TURBINE BLADE
#273Turbine blade with reinforced platform for composite material construction
#274Turbine rotor blade arrangement for a gas turbine and method for the provision of sealing air in a turbine rotor blade arrangement
#275Transfer of turbine blades to rotor wheel
#276Blade comprising a shank, provided with a depressed portion
#277ROTOR BLADE FOR A GAS TURBINE
#278Gas turbine engine with dovetail connection having contoured root
#279Turbomachine bucket with radial support, shim and related turbomachine rotor
#280Installation or removal of turbine blade at turbine blade base
#281Cooling structure for a turbine component
#282Combined balance weight and anti-rotation key
#283Steam turbine
#284TURBINE AIRFOIL ATTACHMENT WITH MULTI-RADIAL SERRATION PROFILE
#285Structure for cooling rotor of turbomachine, rotor and turbomachine having the same
#286Turbine wheel with circumferentially-installed inter-blade heat shields
#287Installation or removal of turbine blade at turbine blade base
#288Turbine blade with three-dimensional CMC construction elements
#289Rotary assembly of a turbomachine equipped with an axial retention system of a blade
#290GAS TURBINE ENGINE ROTOR
#291Turbine blade mounting structure
#292Rotor blade assembly comprising a ring segment shaped or disc segment shaped blade carrier and a radially inner reinforcement structure
#293Blade equipped with platforms comprising a retaining leg
#294Attachment system for a turbine airfoil usable in a gas turbine engine
#295Rotor disk comprising a variable thickness web
#296Fixture for restraining a turbine wheel
#297TURBINE BLADE ASSEMBLY ARRANGEMENT AND CORRESPONDING ASSEMBLY TOOL
#298Turbine rotor with air separation ferrules for cooling of blade and disk coupling portions, for a turbomachine
#299Intermittent tab configuration for retaining ring retention
#300ROTOR DISK HAVING SERRATIONS AND ROTOR