145607 ⎘
Function; Preventing, counteracting or reducing vibration or noise by mistuning rotor blades or stator vanes with irregular interblade spacing, airfoil shape
GAS TURBINE ENGINE WITH ACOUSTIC SPACING OF THE FAN BLADES AND OUTLET GUIDE VANES
#2ROTOR SYSTEM FOR A TURBINE ENGINE
#3GAS TURBINE ENGINE WITH ACOUSTIC SPACING OF THE FAN BLADES AND OUTLET GUIDE VANES
#4GAS TURBINE ENGINE WITH ACOUSTIC SPACING OF THE FAN BLADES AND OUTLET GUIDE VANES
#5GAS TURBINE ENGINE WITH ACOUSTIC SPACING OF THE FAN BLADES AND OUTLET GUIDE VANES
#6GAS TURBINE ENGINE WITH ACOUSTIC SPACING OF THE FAN BLADES AND OUTLET GUIDE VANES
#7GAS TURBINE ENGINE WITH ACOUSTIC SPACING OF THE FAN BLADES AND OUTLET GUIDE VANES
#8GAS TURBINE ENGINE WITH ACOUSTIC SPACING OF THE FAN BLADES AND OUTLET GUIDE VANES
#9GAS TURBINE ENGINE WITH ACOUSTIC SPACING OF THE FAN BLADES AND OUTLET GUIDE VANES
#10NON-UNIFORM AND BI-TRI STATOR SPACING FOR SWIRL RECOVERY VANE (SRV) OPEN ROTOR ENGINES
#11GAS TURBINE ENGINE WITH ACOUSTIC SPACING OF THE FAN BLADES AND OUTLET GUIDE VANES
#12GAS TURBINE ENGINE WITH ACOUSTIC SPACING OF THE FAN BLADES AND OUTLET GUIDE VANES
#13GAS TURBINE ENGINE WITH ACOUSTIC SPACING OF THE FAN BLADES AND OUTLET GUIDE VANES
#14GAS TURBINE ENGINE WITH FORWARD SWEPT OUTLET GUIDE VANES
#15AIRFOIL ASSEMBLY
#16AIRFOIL ROTOR HUB SYSTEM HAVING INTENTIONAL FREQUENCY MISTUNING
#17ROTOR BLADE SYSTEM OF TURBINE ENGINES
#18AIRFOIL FOR A TURBOFAN ENGINE
#19Method for manufacturing impeller
#20ROTOR SYSTEM FOR A TURBINE ENGINE
#21MISTUNING ALTERNATE BLADES IN A GAS TURBINE ENGINE
#22GAS TURBINE AIRFOIL NOISE REDUCTION
#23OUTLET GUIDE VANE ASSEMBLY FOR A TURBOFAN ENGINE
#24AIRCRAFT ENGINE WITH STATOR HAVING VARYING PITCH
#25Rotor blade system of turbine engines
#26Airfoil for a turbofan engine
#27OUTLET GUIDE VANE ASSEMBLY FOR A TURBOFAN ENGINE
#28AIRFOIL ASSEMBLY
#29Biased passages for turbomachinery
#30Airfoil for a turbofan engine
#31Aircraft engine with stator having varying pitch
#32PORTABLE AND WEARABLE HAND-GRASP NEURO-ORTHOSIS
#33Rotor blade system of turbine engines
#34METHOD OF MANUFACTURING A MISTUNED ROTOR
#35Turbocharger
#36Airfoil assembly with a differentially oriented stage
#37STALL MARGIN IMPROVEMENT OF ROTOR FAN AND HOUSING FOR A VANEAXIAL BLOWER SYSTEM
#38Tailored material property tuning for turbine engine fan blades
#39Fan blade with internal shear-thickening fluid damping
#40FAN AND FAN BLADES
#41Fan and fan blades
#42Diffuser with non-constant diffuser vanes pitch and centrifugal turbomachine including said diffuser
#43A RETURN CHANNEL WITH NON-CONSTANT RETURN CHANNEL VANES PITCH AND CENTRIFUGAL TURBOMACHINE INCLUDING SAID RETURN CHANNEL
#44Split shroud for vibration reduction
#45Bladed rotor system and corresponding method of servicing
#46Turbomachine blade having a sweep law with high flutter margin
#47Profiled structure for an aircraft or turbomachine
#48GAS TURBINE ENGINE WITH PARTIAL INLET VANE
#49Geared gas turbine engine with reduced fan noise
#50Blade rotor and fluid working machine comprising such a rotor
#51Blade cutback distribution in rotor for noise reduction
#52Variable pitch bladed disc
#53High cycle fatigue design for gas turbine engines
#54Mistuning of turbine blades with one or more internal cavities
#55Biased passages for turbomachinery
#56Compressor rotor for supersonic flutter and/or resonant stress mitigation
#57Geared gas turbine engine with reduced fan noise
#58Stacking of rotor blade aerofoil sections to adjust resonant frequencies
#59GAS TURBINE ENGINE JET
#60Heat dissipation fan
#61Fan rotor with flow induced resonance control
#62Mistuned rotors and methods for manufacture
#63Mistuned airfoil assemblies
#64LOW-NOISE BLOWER
#65Fan rotor with flow induced resonance control
#66SNUBBERED BLADES WITH IMPROVED FLUTTER RESISTANCE
#67Shrouded blades with improved flutter resistance
#68Compressor rotor with coated blades
#69Rotor blade arrangement
#70Method and arrangement to minimize noise and excitation of structures due to cavity acoustic modes
#71Gas turbine engine having a mistuned stage
#72Flow channel for a turbomachine
#73Mistuned fan for gas turbine engine
#74Gas turbine engine with partial inlet vane
#75Bladed disk
#76Mistuned compressor rotor with hub scoops
#77Compressor rotor with coated blades
#78Mistuned rotor for gas turbine engine
#79Rotor with non-uniform blade tip clearance
#80Tuned airfoil assembly
#81Surface heat exchanger and acoustic treatment
#82Mistuned concentric airfoil assembly and method of mistuning same
#83Geared gas turbine engine with reduced fan noise
#84Rotor with subset of blades having a cutout leading edge
#85Rotary machines including a hybrid rotor with hollow and solid rotor blade sets
#86METHOD FOR GENERATING AND SELECTING A MISTUNING PATTERN OF A BLADED WHEEL OF A TURBOMACHINE
#87Variable nozzle mechanism and variable displacement type exhaust turbocharger
#88Gas turbine with a radial-to-axial intake, variable-angle inlet guide vane therefore, and method of operation
#89Axial fan with unbalanced blade spacing
#90Fan blade surface features
#91Fan rotor with flow induced resonance control
#92Fan rotor with flow induced resonance control
#93Fan rotor with flow induced resonance control
#94Fan
#95Fan
#96Mistuned bladed rotor and associated manufacturing method
#97Method for manufacturing a turbomachine fan having a reduced noise level at multiple rotational frequencies of said turbomachine
#98Turbine blade comprising a cavity with wall surface discontinuities and process for the production thereof
#99Airfoil structure having a shape memory alloy actuator
#100Supersonic single-stage turbofan engine
#101Mistuned laminate airfoil
#102Turbine engine air guide assembly with improved aerodynamic performance
#103Fan blade surface features
#104Variable turbomachine vane cascade
#105LOW ENERGY WAKE STAGE
#106Guide vane segment
#107Variable pitch bladed disc
#108Variable pitch bladed disc
#109Non uniform vane spacing
#110Compressor rotor for supersonic flutter and/or resonant stress mitigation
#111Turbine blade centroid shifting method and system
#112Gas turbine engine with short inlet and mistuned fan blades
#113Instrumented flow passage of a turbine engine
#114Guide vane segment for a turbomachine
#115Mistuned concentric airfoil assembly and method of mistuning same
#116Biased passages for turbomachinery
#117Gas turbine engine
#118Gas turbine engine
#119Compressor
#120Low-noise blower
#121Blade disk arrangement for blade frequency tuning
#122Removably attachable snubber assembly
#123Rotary machines including a hybrid rotor with an integrally bladed rotor portion
#124Pylon matched fan exit guide vane for noise reduction in a geared turbofan engine
#125Blade for a turbine engine propeller, in particular a propfan engine, propeller, and turbine engine comprising such a blade
#126Gas turbine engine stator vane mistuning
#127Gas turbine engine rotor mistuning
#128Modal noise reduction for gas turbine engine
#129Blade cutback distribution in rotor for noise reduction
#130Fan assembly
#131Axial compressor rotor incorporating non-axisymmetric hub flowpath and splittered blades
#132Gas turbine engine stator vane asymmetry
#133Alternating Vane Asymmetry
#134Blade or vane arrangement for a turbomachine
#135Compressor with stator vane configuration in vicinity of bleed structure, and gas turbine engine
#136Rotor blade with reduced acoustic response
#137Rotating body provided with blades
#138Geared gas turbine engine with reduced fan noise
#139Gas turbine engine with partial inlet vane
#140Endwall contouring for airfoil rows with varying airfoil geometries
#141Rotors with modulus mistuned airfoils
#142Turbomachine blade arrangement with first and second guides with respective movable first and second elements to reduce vibrational response
#143Blade cascade for a turbomachine
#144Gas turbine engine having a mistuned stage
#145Method for detuning a rotor-blade cascade
#146Gas turbine blade array with reduced acoustic output
#147Undulating stator for reducing the noise produced by interaction with a rotor
#148Rotor and gas turbine engine including a rotor
#149Shrouded turbine blade with cut corner
#150Components resistant to traveling wave vibration and methods for manufacturing the same
#151Device and method for controlling the pitch of blades
#152Method for designing a turbine
#153Mistuned airfoil assemblies
#154Blade cascade
#155Blade cascade
#156Airplane turbojet fan blade of cambered profile in its root sections
#157Array of flow-directing elements for a gas turbine compressor
#158Aerofoil array for a gas turbine with anti fluttering means
#159Wind turbine rotor blade with serrated extension
#160Guide blade ring for an axial turbomachine and method for designing the guide blade ring
#161Alternating nozzles for radial inflow turbine
#162Turbine blade with sectioned pins
#163Split damped outer shroud for gas turbine engine stator arrays
#164Low-noise blower
#165Noise attenuation in rotating blades
#166Probabilistic high cycle fatigue (HCF) design optimization process
#167Noise reducing vane
#168Low pressure turbine provided with splitters at the last stator array, in particular for a gas turbine engine
#169Turbomachinery stationary vane arrangement for disk and blade excitation reduction and phase cancellation
#170Blade cascade for turbo machine
#171Pylon matched fan exit guide vane for noise reduction in a geared turbofan engine
#172Gas turbine
#173GAS TURBINE ASYMMETRIC NOZZLE GUIDE VANES
#174Impeller and method for driving fluids using the same
#175Intentionally frequency mistuned turbine blades
#176Bladed rotor for a turbomachine
#177Static vane assembly for an axial flow turbine
#178GEARED GAS TURBINE ENGINE WITH REDUCED FAN NOISE
#179TURBOMACHINE INCLUDING FLOW IMPROVEMENT SYSTEM
#180TURBOMACHINE FLOW IMPROVEMENT SYSTEM
#181Blade cascade and turbomachine
#182Modal tuning for vanes
#183ALTERNATE SHROUD WIDTH TO PROVIDE MISTUNING ON COMPRESSOR STATOR CLUSTERS
#184AIRFOIL AIR SEAL ASSEMBLY
#185Aerodynamic coupling between two annular rows of stationary vanes in a turbine engine
#186ROTOR ASYMMETRY
#187ROTOR WITH ASYMMETRIC BLADE SPACING
#188Turbine blade with laterally biased airfoil and platform centers of mass
#189Blade disk arrangement for blade frequency tuning
#190Alternative partial steam admission arc for reduced noise generation
#191ROTARY MACHINE HAVING SPACERS FOR CONTROL OF FLUID DYNAMICS
#192Rotary machine having non-uniform blade and vane spacing
#193BLADE EXCITATION REDUCTION METHOD AND ARRANGEMENT
#194Turbine rotor assembly and steam turbine
#195Bypass duct of a turbofan engine
#196Compressor with asymmetric stator and acoustic cutoff
#197Fan assembly
#198Use of non-uniform nozzle vane spacing to reduce acoustic signature
#199Intentionally mistuned integrally bladed rotor
#200Diffuser for centrifugal compressor
#201Stator ring configuration
#202Steam turbine having stage with buckets of different materials
#203Stator cascade of turbo type fluid machine
#204Method of manufacturing a rotor for a gas turbine engine that includes identifying the frequency response of the rotor and adjusting the frequency response by providing a pressure gradient within the rotor
#205Multi-blade fan
#206Method for machining an integrally bladed rotor
#207Method of providing non-uniform stator vane spacing in a compressor
#208Gas turbine compression system and compressor structure
#209Mixed tuned hybrid blade related method
#210Methods and apparatus for assembling gas turbine engines
#211Gas turbine engine with acoustic spacing of the fan blades and outlet guide vanes
#212Gas turbine engine with acoustic spacing of the fan blades and outlet guide vanes
#213Gas turbine engine with acoustic spacing of the fan blades and outlet guide vanes
#214Open rotor with fixed guide vane/stator
#215Non-uniform and bi-tri stator spacing for swirl recovery vane (SRV) open rotor engines
#216Cooling fan
#217Low-noise blade for an open rotor