145377 ⎘
Components; Rotors for turbines
Aircraft with counter-rotating turbofan engines
#602Device for locally regulating the delivery of gas in response to environmental variables
#603Clutch assembly with integrated surface cooling
#604Compressor assembly for turbocharger burst containment
#605GAS TURBINE ENGINE WITH ANGULARLY OFFSET TURBINE VANES
#606Generating Power Using an Ion Transport Membrane
#607Blade tip clearance systems
#608Arrangement of a rotor and at least a blade
#609Counter-swirl doublet combustor with plunged holes
#610REVERSE CORE FLOW GAS TURBINE ENGINE
#611Device for protecting against oil leaks towards the rotors of a turbomachine turbine
#612Tip clearance control for turbine blades
#613GAS TURBINE ENGINE NON-ROTATING STRUCTURE WEDGE SEAL
#614Apparatus having engineered surface feature and method to reduce wear and friction between CMC-to-metal attachment and interface
#615Removable riveted balance ring
#616ELECTRICALLY COUPLED COUNTER-ROTATION FOR GAS TURBINE COMPRESSORS
#617Method for starting a steam turbine
#618Turbine engine assembly and method of manufacturing
#619Method to pilot using flexible profile
#620Pre-diffuser with multiple radii
#621Turbine airfoil platform segment with film cooling hole arrangement
#622Rotor heat shield and method for securing the same into a rotor assembly
#623Rotor disk assembly for a gas turbine engine
#624Fiber reinforced spacer for a gas turbine engine
#625Geared turbofan engine gearbox arrangement
#626Three spool turbofan engine with low noise intermediate turbine rotor
#627Frame segment for a combustor turbine interface
#628LOW NOISE TURBINE FOR GEARED TURBOFAN ENGINE
#629Fire extinction design for an auxiliary power unit compartment of an aircraft
#630AIRCRAFT
#631Angled Core Engine
#632Device and method for separating dirt particles from the working medium of a turbine
#633Turbocharger roller support system
#634Internally cooled turbine platform
#635GAS TURBINE AND HEAT SHIELD FOR A GAS TURBINE
#636Alternating Vane Asymmetry
#637Hybrid ram air turbine
#638Rotor for a thermal turbomachine
#639Split axial-centrifugal compressor
#640Turbofan engine front section
#641Split turbocharger bearing assembly
#642TURBINE AND METHOD FOR DETECTING RUBBING
#643Variable fan nozzle using shape memory material
#644Composite components for gas turbine engines
#645Gas turbine engine driving multiple fans
#646Gas turbine engine and frame
#647Turbine-end bearing support and cooling system
#648Bleed valve
#649Additive process for an abradable blade track used in a gas turbine engine
#650Mixed stator for an axial turbine engine compressor
#651Turbine blisk including ceramic matrix composite blades and methods of manufacture
#652LOW NOISE TURBINE FOR GEARED TURBOFAN ENGINE
#653Rotor for a turbine
#654Method of connecting an impeller to a shaft, connection arrangement and rotary machine
#655Compressor with stator vane configuration in vicinity of bleed structure, and gas turbine engine
#656Speed reduced driven turbocharger
#657Air separator for a turbine engine
#658Offset cores for gas turbine engines
#659Pulse energy enhanced turbine for automotive turbochargers
#660Compressor bleed air supply for an aircraft environmental control system
#661LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BETWEEN INLET AND FAN SIZE
#662Radially fastened fixed-variable vane system
#663Gas turbines engine support structures
#664Turbofan engine bearing and gearbox arrangement
#665Turbofan engine front section
#666Turbine blade tip shroud
#667Gas turbine hub
#668Reverse flow single spool core gas turbine engine
#669Rotor assembly for an open cycle engine, and an open cycle engine
#670Coating system including alternating layers of amorphous silica and amorphous silicon nitride
#671INSPECTION AND QUALIFICATION FOR REMANUFACTURING OF COMPRESSOR WHEELS
#672Coating system including oxide nanoparticles in oxide matrix
#673GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE
#674Turbine engine comprising a device for braking the fan rotor
#675COMPRESSOR AND TURBOCHARGER
#676Turbine wheel for a turbine engine
#677Bladed rotor arrangement including axial projection
#678Bladed rotor arrangement and a lock plate for a bladed rotor arrangement
#679GAS TURBINE ENGINE BLADE SLOT HEAT SHIELD
#680FAN DRIVE GEAR SYSTEM
#681Gas turbine engine blade outer air seal assembly
#682Geared turbofan engine with high compressor exit temperature
#683Endwall contouring for airfoil rows with varying airfoil geometries
#684Auxilliary power and thrust unit drive system
#685GAS TURBINE ENGINE WITH HIGH SPEED LOW PRESSURE TURBINE SECTION
#686GEARED TURBOFAN WITH THREE TURBINES WITH HIGH SPEED FAN DRIVE TURBINE
#687Decoupled gas turbine engine
#688Turbine wheel of an exhaust-gas turbocharger
#689Turbofan engine main bearing arrangement
#690GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE
#691Method for manufacturing composite fan annulus filler having nano-coating
#692Modulated turbine cooling system
#693Method for producing a rotor of a charging apparatus
#694Circulating lubricant through a turbine engine component with parallel pumps
#695LOW NOISE TURBINE FOR GEARED TURBOFAN ENGINE
#696Arcuate directionally solidified components and manufacture methods
#697Asymmetric double-entry turbine
#698LOW NOISE TURBINE FOR GEARED TURBOFAN ENGINE
#699A COMPACT ROTARY WASTEGATE VALVE
#700Turbine of a turbocompound engine with variable load and a controller thereof
#701GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE
#702GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE
#703Oil baffles in carrier for a fan drive gear system
#704Shaped rim cavity wing surface
#705TURBINE WHEEL OF AN EXHAUST GAS TURBOCHARGER AND ASSOCIATED PRODUCTION METHOD
#706Asymmetric fan nozzle in high-BPR separate-flow nacelle
#707Combined two engine cycle with at least one recuperated cycle engine for rotor drive
#708Electric rotor fit onto a turbomachine shaft
#709Multi-stage turbocharger system
#710Rotor and gas turbine engine including same
#711Multivariable feedforward control
#712TURBINE SECTION OF HIGH BYPASS TURBOFAN
#713TURBINE SECTION OF HIGH BYPASS TURBOFAN
#714Segmented seal for a gas turbine engine
#715Flow control structures for turbomachines and methods of designing the same
#716Geared turbofan architecture
#717Geared turbofan engine with high compressor exit temperature
#718Rotor balancing
#719Balanced rotor disc, and balancing method
#720TURBOCHARGER AND CASING
#721Gas turbine engine vapor cooled centrifugal impeller
#722GAS TURBINE ENGINE COMPONENT WITH EMBEDDED DATA
#723Recessable damper for turbine
#724Method for friction welding a blade onto a turbine engine rotor disc; corresponding integral blade disc
#725Aerofoil blade
#726Spinner for electrically grounding fan blades
#727Gas turbine engine
#728High pressure compressor thermal shield apparatus and system
#729Reduced fan containment threat through liner and blade design
#730GAS TURBINE ROTOR
#731Process for producing a turbine rotor
#732Blisk with low stresses at blade root, preferably for an aircraft turbine engine fan
#733Steam turbine with resonance chamber
#734Method for designing a turbine
#735Axial Flow Machine
#736Layered arrangement, hot-gas path component, and process of producing a layered arrangement
#737Turbine engine blade made of composite material with a bulb-shaped root
#738Group of blade rows
#739Thermal shields for gas turbine rotor
#740Geared turbofan engine gearbox arrangement
#741Turbofan engine main bearing arrangement
#742Turbine split ring retention and anti-rotation method
#743High pressure rotor disk
#744Shaped rim cavity wing surface
#745Airfoil having internal lattice network
#746Gas turbine engine driving multiple fans
#747Gas turbine engine component with diffusive cooling hole
#748GEARED TURBOFAN GAS TURBINE ENGINE ARCHITECTURE
#749Gas turbine engine with low stage count low pressure turbine
#750Generating power using an ion transport membrane
#751Gas turbine engine and frame
#752Separation resistant aerodynamic article
#753Variable fan nozzle using shape memory material
#754Compressor in an exhaust gas turbocharger of an internal combustion engine and method for operating the compressor
#755Turbocharger compressor with an auxiliary rotor wheel and magnetic clutch
#756Axial compressor rotor assembly
#757Turbine rotor dovetail structure with splines
#758Radial turbine assembly with intermediate blade bonding ring
#759Clocking balance weight rotor assembly for gas turbine engines
#760Turbine blade airfoil profile
#761Splined balance weight for rotating components in gas turbine engines
#762Rotor assembly for a gas turbine engine and method for assembling same
#763Tip shroud with exit surface for cooling passages
#764Apparatus and process of forming an integrally bladed rotor with cooled single crystal blades and an equiax nickel disk
#765Super-cooled ice impact protection for a gas turbine engine
#766Gas turbine engine
#767Platform for an airfoil of a gas turbine engine
#768Turbine wheel incorportating nickel-based alloy
#769Cast integrally bladed rotor with bore entry cooling
#770Apparatus and process of forming an integrally bladed rotor with cooled single crystal blades and an equiax nickel disk
#771Gas turbine engine airfoil frequency design
#772Gas turbine engine airfoil frequency design
#773Gas turbine engine airfoil frequency design
#774Gas turbine engine airfoil frequency design
#775Gas turbine engine airfoil frequency design
#776Gas turbine engine airfoil frequency design
#777Gas turbine engine airfoil frequency design
#778Gas turbine engine airfoil frequency design
#779Gas turbine engine airfoil frequency design
#780Housing for bearing cavity in a gas turbine engine
#781Generator system