136880 ā
Preventing or minimising internal leakage of working-fluid, e.g. between stages; Sealing means between non relatively rotating elements; Sealing the gap between rotor blades or blades and rotor by spacer elements between the blades, e.g. independent interblade platforms
Reinforced Fan Inter-Blade Platforms
#2INSERTION OF CERAMIC MEMBERS FOR GAS PATH ENDWALL CONTOURING
#3ANNULUS FILLER FOR A GAS TURBINE ENGINE
#4ANNULUS FILLER FOR A GAS TURBINE ENGINE
#5ANNULUS FILLER FOR A GAS TURBINE ENGINE
#6Seal assembly and a turbine with the same
#7Turbine engine with a composite-airfoil assembly having a dovetail portion
#8FAN ASSEMBLY HAVING A FAN RETENTION MEMBER FOR SUPPORTING A BLADE PLATFORM
#9PLATFORM FOR A FAN ASSEMBLY
#10Deformable root spacer for a gas turbine engine rotor blade
#11Platform for an airfoil of a gas turbine engine
#12Rotor with feather seals
#13Rotor assembly for gas turbine engines
#14Platform for a fan rotor of an aircraft turbomachine
#15Composite platform for a fan of an aircraft turbine engine
#16Method for manufacturing a composite platform for an aircraft turbine engine fan
#17Turbine circumferential dovetail leakage reduction
#18Turbomachine assembly comprising fan blades with an extended trailing edge
#19PREFORM WITH ONE-PIECE WOVEN FIBROUS REINFORCEMENT FOR INTER-BLADE PLATFORM
#20Rotor assembly for gas turbine engines
#21Thermally isolated rotor systems and methods
#22Turbine circumferential dovetail leakage reduction
#23Fan blade platform seal and method for forming same
#24Turbine fan fairing platform with protective surface
#25Rotor blade pair for rotational equipment
#26Rotor blade sealing structures
#27Damper stacks for turbomachine rotor blades
#28Airfoil-mounted platforms of gas turbine engines
#29Gas turbine engine
#30Sealing arrangement between turbine shroud segments
#31Inserts for slotted integrally bladed rotor
#32Inter-blade platform seal
#33Fan comprising an inter-blade platform attached upstream by a ferrule
#34Air-fire seal and assembly comprising such a seal
#35COMBUSTOR-VANE INTERFACE FEATHER SEAL
#36Platform apparatus for propulsion rotor
#37Rotor assembly with structural platforms for gas turbine engines
#38Rotor assembly for gas turbine engines
#39Rotor assembly with rotor disc lip
#40Platform with axial attachment for blade with circumferential attachment
#41Fan platform wedge seal
#42Fan including a platform and a locking bolt
#43Turbine disk with platforms coupled to disk
#44Turbine disk with blade supported platforms
#45Gas turbine engine fan platform
#46Fan spacer for a gas turbine engine
#47Platform apparatus for propulsion rotor
#48Composite fan platform lug reinforcement
#49Sealing system for a rotary machine and method of assembling same
#50Fairing ring for a bladed wheel
#51Annulus filler
#52Detachable anti-wear cap for rectifier sector
#53Annulus filler
#54Turbine blade, turbine, and gas turbine having the same
#55Composite stator with integral platforms for gas turbine engines
#56Blade platform with damper restraint
#57Blade platform and a fan disk for an aviation turbine engine
#58Sealing system for a rotary machine and method of assembling same
#59Fiber blank woven as a single piece by three-dimensional weaving to make a closed box-structure platform out of composite material for a turbine engine fan
#60Compliant rotatable inter-stage turbine seal
#61Removable anti-wear part for blade tip
#62Shroud assembly for turbine systems
#63SEALING PART FOR A GAS TURBINE AND METHOD FOR MANUFACTURING SUCH A SEALING PART
#64I beam blade platform
#65Air-fire seal and assembly comprising such a seal
#66Fan platform with stiffening feature
#67Turbine blade with ceramic matrix composite material construction
#68Rotary assembly of an aeronautical turbomachine comprising an added-on fan blade platform
#69DISPOSABLE FAN PLATFORM FAIRING
#70BLADE PLATFORM WITH CHAMFER
#71Assembly of turbine engine parts comprising a fan blade having an integrated platform, and corresponding turbine engine
#72Damper with varying thickness for a blade
#73Turbine wheel with circumferentially-installed inter-blade heat shields
#74Method and system for improving flow characteristics in marine propellers
#75Integrally bladed fan rotor
#76Gas turbine engine
#77Rotor disk comprising a variable thickness web
#78Method for manufacturing a turbomachine blade made of composite material
#79Fitted platform for a turbine engine fan, and a method of fabricating it
#80Radial seal and assembly
#81Split line flow path seals
#82Turbomachine blade fitted with an elastomer gasket
#83Conical load spreader for composite bolted joint
#84Low profile fan platform attachment
#85Stator-vane structure and turbofan engine
#86Seal member
#87Intercomponent seal for a gas turbine engine
#88Rotor for turbine engine comprising blades with added platforms
#89Stator-vane structure and turbofan engine employing the same
#90Method and system for separable blade platform retention clip
#91Tool and method for installing turbomachine component
#92Airfoil platform having dual pin apertures and a vertical stiffener
#93Platform for an airfoil having bowed sidewalls
#94Fan platform for a gas turbine engine
#95Aviation turbine engine fan assembly including a fitted platform
#96Turbomachine fan frame comprising improved attachment means
#97Fan blade platform spacer mounting
#98Fan platform with stiffening feature
#99Blade or vane row and gas turbine
#100Non-integral blade and platform segment for rotor
#101Reversible blade rotor seal with protrusions
#102Rotor heat shield
#103Trailing edge platform seals
#104Split line flow path seals
#105COMPRESSED CHOPPED FIBER COMPOSITE FAN BLADE PLATFORM
#106BLADED WHEEL WITH SEPARABLE PLATFORM
#107Airfoil device for a gas turbine and corresponding arrangement
#108Fan blade platform seal with leading edge winglet
#109Gas turbine bucket shanks with seal pins
#110Faceted turbine blade damper-seal
#111Method for manufacturing a stage of a steam turbine
#112Fan rotor with integrated platform attachment
#113Rotary assembly for an aviation turbine engine, the assembly comprising a separate fan blade platform mounted on a fan disk
#114TURBINE BLADE AND GAS TURBINE
#115Blade tip clearance control system including BOAS support
#116Gas turbine engine with disk having periphery with protrusions
#117CMC blade with monolithic ceramic platform and dovetail
#118Additive manufactured inseparable platform damper and seal assembly for a gas turbine engine
#119Seal for gas turbine engine
#120Fan platform with leading edge tab
#121Flowpath boundary and rotor assemblies in gas turbines
#122FLOWPATH BOUNDARY AND ROTOR ASSEMBLIES IN GAS TURBINES
#123FLOWPATH BOUNDARY AND ROTOR ASSEMBLIES IN GAS TURBINES
#124Flowpath boundary and rotor assemblies in gas turbines
#125Bucket assembly for replacing old bucket provided with turbine and method for replacing the same
#126Trough seal for gas turbine engine
#127Mini blind stator leakage reduction
#128Bonded fan platform
#129Vibration damper
#130Platform of small hub-tip ratio
#131Rotor heat shield and method for securing the same into a rotor assembly
#132Turbine blade or vane having a stepped and beveled platform edge
#133Composite compressor blade and method of assembling
#134Assembly for plugging an aperture in a body
#135Composite annulus filler
#136Endwall contouring for airfoil rows with varying airfoil geometries
#137Fan platform
#138Panels of a fan of a gas turbine
#139Panels of a fan of a gas turbine
#140ROTOR BLADE WITH L-SHAPED FEATHER SEAL
#141Method for manufacturing composite fan annulus filler having nano-coating
#142Riffled seal for a turbomachine, turbomachine and method of manufacturing a riffled seal for a turbomachine
#143Segmented seal for a gas turbine engine
#144Gas turbine rotor blade and gas turbine rotor
#145Segmented rim seal spacer for a gas turbine engine
#146T-shaped platform leading edge anti-rotation tabs
#147Annulus filler
#148Electrically grounding fan platforms
#149Blisk with low stresses at blade root, preferably for an aircraft turbine engine fan
#150Bladed rotor
#151Platform for ceramic matrix composite turbine blades
#152Turbine engine blade made of composite material with a bulb-shaped root
#153Seal damper with improved retention
#154Injection mold core for making a part out of composite material, the part having a closed box
#155Gas turbine engine fan spacer platform attachments
#156Contoured flowpath surface
#157Injection molded composite fan platform
#158Vane array with one or more non-integral platforms
#159Low profile fan platform attachment
#160Mass offset for damping performance
#161Microchannel exhaust for cooling and/or purging gas turbine segment gaps
#162Fan blade root integrated sealing solution
#163Rotor blade arrangement and gas turbine
#164Turbine blade and non-integral platform with pin attachment
#165Belly band seal with circumferential spacer
#166ANNULUS FILLER
#167Annulus filler
#168Turbine blade or vane
#169Linear gasket for an inter-blade platform
#170Turbine seal system and method
#171Turbine seal system and method
#172Composite material reinforcing part of pi-shaped section, in particular a platform for a turbine engine fan, and its method of fabrication
#173Turbine engine wheel, in particular for a low pressure turbine
#174Turbomachine blade assembly
#175Turbine engine blade
#176Integral fan blade wear pad and platform seal
#177TURBINE BLADE WITH A PIN SEAL SLOT
#178TURBINE BLADE PIN SEAL
#179Fan spacer having unitary over molded feature
#180Steam turbine
#181Axial compressor and method for controlling stage-to-stage leakage therein
#182Low radius ratio fan for a gas turbine engine
#183Gas turbine engine nose cone attachment configuration
#184Non-integral fan blade platform
#185System for damping vibrations in a turbine
#186Damper pin
#187Reversible blade damper
#188SOLID SEAL WITH COOLING PATHWAYS
#189ANNULUS FILLER FOR AXIAL FLOW MACHINE
#190Turbomachine rotor with a means for axial retention of the blades
#191Fan blade platform flap seal
#192NOZZLE FOR TURBINE SYSTEM
#193Fairing assembly
#194INTERBLADE PLATFORM FOR A FAN, ROTOR OF A FAN AND ASSOCIATED MANUFACTURING METHOD
#195Fan blade platform
#196Airfoil and disk interface system for gas turbine engines
#197Detachable fan blade platform and method of repairing same
#198Method for damping a gas-turbine blade, and vibration damper for implementing same
#199Axial-flow machine
#200Annulus filler
#201SEAL ASSEMBLY FOR TURBINE COOLANT PASSAGEWAYS
#202Methods for the controlled reduction of turbine nozzle flow areas and turbine nozzle components having reduced flow areas
#203Near flow path seal with axially flexible arms
#204Composite airfoil assembly
#205Turbine wheel for a turbine engine
#206Thermal plug for turbine bucket shank cavity and related method
#207Strip seals
#208Turbine blade and non-integral platform with pin attachment
#209Metallic fan blade platform
#210Seal assembly retention method
#211INGESTION-TOLERANT LOW LEAKAGE LOW PRESSURE TURBINE
#212CHEVRON PLATFORM TURBINE VANE
#213Hybrid rotor disk assembly with ceramic matrix composites platform for a gas turbine engine
#214Ceramic matrix composite continuous āIā-shaped fiber geometry airfoil for a gas turbine engine
#215Turbine wheel for a turbine engine
#216METHOD FOR FUSION WELDING A MONOCRYSTALLINE WORKPIECE TO A POLYCRYSTALLINE WORKPIECE AND ROTOR
#217ANNULUS FILLER SYSTEM
#218Annulus filler system
#219Turbomachine rotor
#220Bladed rotor
#221ROTOR HAVING AN ANNULUS FILLER
#222Turbomachine rotor assembly and method
#223Damper pin
#224SEALING DEVICE AND METHOD FOR PROVIDING A SEAL IN A TURBINE SYSTEM
#225METHODS, SYSTEMS AND APPARATUS RELATING TO ROOT AND PLATFORM CONFIGURATIONS FOR TURBINE ROTOR BLADES
#226Annulus filler
#227Turbine blade assembly including a damper
#228Blade arrangement, especially stator blade arrangement
#229Annulus filler
#230ANNULAR FLOW CHANNEL SECTION FOR A TURBOMACHINE
#231ROTARY MACHINE HAVING SPACERS FOR CONTROL OF FLUID DYNAMICS
#232Rotor for turbomachinery
#233SEAL MEMBER FOR HOT GAS PATH COMPONENT
#234Seal for a platform in the rotor of a turbine engine
#235Stator stage for turbomachine compressor
#236Non-integral platform and damper for an airfoil
#237Structural and aerodynamic module for a turbomachine casing and casing structure comprising a plurality of such a module
#238Annulus filler assembly for a rotor of a turbomachine
#239Turbine engine airfoil and platform assembly
#240Modular turbine airfoil and platform assembly with independent root teeth
#241Annulus filler for a gas turbine engine
#242Annulus filler element for a rotor of a turbomachine
#243Turbine blade having a constant thickness airfoil skin
#244Rotor assembly for a gas turbine
#245Sealing assembly
#246Energy absorbing fan blade spacer
#247Annulus filler for a gas turbine engine
#248Annulus filler
#249Turbomachine rotor assembly and method
#250Fan blade anti-fretting insert
#251Fan blade platform
#252Non-integral turbine blade platforms and systems
#253Turbine blade assembly including a damper
#254Platform seal in a turbomachine rotor, method for improving the seal between a platform and a turbomachine blade
#255Rotor blade arrangement and gas turbine
#256Spacers and turbines
#257Turbine blade damper arrangement
#258Blade arrangement
#259Annulus filler
#260Blade arrangement
#261Turbine blade and gas turbine equipped with a turbine blade
#262Aeroengine fan assembly
#263Fan rotor for a turbomachine or a test engine
#264Platformless turbine blade
#265Annulus filler
#266Annulus filler
#267Platform and blade for a bladed wheel of a turbomachine, bladed wheel and compressor or turbomachine comprising such a bladed wheel
#268Damping and sealing system for turbine blades
#269Turbine airfoil with platform cooling
#270Seal assembly retention feature and assembly method
#271Nozzle guide vanes
#272Turbine blade and gas turbine equipped with a turbine blade
#273Gas turbine systems involving feather seals
#274Turbine rotor blade and method of assembling the same
#275Turbine rotor blade assembly and method of assembling the same
#276Turbomachine fan
#277Gap seal in blades of a turbomachine
#278Rotary assembly for a turbomachine fan
#279Turbine blade and gas turbine equipped with a turbine blade
#280Turbomachine fan
#281Locking and fixing device for a heat shield element for a rotor unit of a turbomachine
#282Fan blade for a gas turbine engine
#283Air seal unit adapted to be positioned adjacent blade structure in a gas turbine
#284High temperature seals and high temperature sealing systems
#285Thermally sprayed conformal seal
#286Annulus filler seal
#287Aerofoil stage and seal for use therein
#288Vane shroud through-flow platform cover
#289Segmented component seal
#290Segmented component seal
#291Separable blade platform
#292Cooling arrangement
#293Gas turbine blade or vane and platform element for a gas turbine blade or vane ring of a gas turbine, supporting structure for securing gas turbine blades or vanes arranged in a ring, gas turbine blade or vane ring and the use of a gas turbine blade or vane ring
#294Method of calibrating the mass of components intended to be mounted at the periphery of a rotor
#295Sealing arrangement, in particular for the blade segments of gas turbines
#296Gas turbine having a sealing structure
#297Sealing arrangement, in particular for the blade segments of gas turbines
#298Rotating blade body
#299Controlled leakage pin and vibration damper for active cooling and purge of bucket slash faces
#300Cooling system for a seal for turbine vane shrouds