LOW NOISE TURBINE FOR GAS TURBINE ENGINE

GAS TURBINE ENGINE WITH HIGH SPEED LOW PRESSURE TURBINE SECTION AND BEARING SUPPORT FEATURES

FLEXIBLE SUPPORT STRUCTURE FOR A GEARED ARCHITECTURE GAS TURBINE ENGINE

GAS TURBINE ENGINE FRONT SECTION

COMPRESSOR FOR A FUEL-CELL SYSTEM, AND FUEL-CELL SYSTEM HAVING SAME

LOW NOISE TURBINE FOR GEARED TURBOFAN ENGINE

SHORT IMPELLER FOR A TURBOMACHINE

TANDEM BLADE ROTOR DISK

MONOLITHIC SUPERSTRUCTURE FOR LOAD PATH OPTIMIZATION

BLADE FASTENING ASSEMBLY AND GAS TURBINE INCLUDING SAME

Centerbody insertion for improved CAC motor cooling

ROTOR ASSEMBLY FOR A TURBOMOLECULAR PUMP

Vacuum pump and rotating cylinder provided in vacuum pump

Energy-saving device for rapidly and infinitely compressing air

TURBOMOLECULAR VACUUM PUMP AND METHOD FOR MANUFACTURING A ROTOR

Compressor flowpath

Low noise turbine for geared turbofan engine

Vacuum pump and vacuum pump rotor blade

Pressurized airflow to rotate compressor during engine shutdown

GAS TURBINE ENGINE WITH HIGH SPEED LOW PRESSURE TURBINE SECTION AND BEARING SUPPORT FEATURES

Compressor flowpath

Tandem blade rotor disk

Gas turbine engine front section

Axial and downstream compressor assembly

Geared turbofan engine gearbox arrangement

Hydrogen centrifugal compressor

Tandem blade rotor disk

Integral superstructure for load path optimization

Flexible support structure for a geared architecture gas turbine engine

MECHANICALLY DRIVEN AIR VEHICLE THERMAL MANAGEMENT DEVICE

Reverse flow engine architecture

FLEXIBLE SUPPORT STRUCTURE FOR A GEARED ARCHITECTURE GAS TURBINE ENGINE

Outlet guide vane

Turbofan engine front section

Gas turbine engine with axial movable fan variable area nozzle

Vacuum pump, stator column, base, and exhaust system of vacuum pump

Ammonia plant synthesis gas compressor train

Turbomachine comprising an air collection circuit

Reinforced vacuum system component

Gas turbine engine with separable shaft and seal assembly

Compact aero-thermo model based engine power control

Geared turbofan engine gearbox arrangement

Tandem blade rotor disk

Gas turbine engine compressors having optimized stall enhancement feature configurations and methods for the production thereof

Flexible support structure for a geared architecture gas turbine engine

LOW NOISE TURBINE FOR GEARED TURBOFAN ENGINE

Rotor disk for gas turbine engine

Compressor flowpath

Flexible support structure for a geared architecture gas turbine engine

Nano-porous based thermal enclosure with heat removal

Turbomachine rotor rotating system and turbomachine rotor

LEADING EDGE COVER MEMBER, LEADING EDGE COVER MEMBER UNIT, COMPOSITE BLADE, METHOD OF MANUFACTURING LEADING EDGE COVER MEMBER, AND METHOD OF MANUFACTURING COMPOSITE BLADE

Housing with filter for purge valve protection

Compressor rotor, gas turbine rotor provided therewith, and gas turbine

BLEED TUBES

Retention clip for a blade outer air seal

BOOSTER COMPRESSOR WITH SPEED CHANGE SYSTEM

Reverse flow engine architecture

Methods for processing bonded dual alloy rotors including differential heat treatment processes

TURBINE BLADES AND VANES FOR GAS TURBINE ENGINE

Gas turbine engine with high speed low pressure turbine section and bearing support features

MAGNETIC SQUEEZE FILM DAMPER SYSTEM FOR A GAS TURBINE ENGINE

SHROUDED BLADE ASSEMBLIES

Method and system for elastic bearing support

Mini-disk for gas turbine engine

Flexible support structure for a geared architecture gas turbine engine

Flexible support structure for a geared architecture gas turbine engine

Turbine airfoil with passive morphing structure

FIRST STAGE TURBINE NOZZLE WITH EROSION COATING SURFACE FINISH

Gas turbine engine with vane having a cooling inlet

BOAS thermal protection

Rotor blade arrangement

Cross key anti-rotation spacer

Flared anti-vortex tube rotor insert

Telescoping bore basket for gas turbine engine

Pump arrangement, axial-flow machine and compressor comprising at least one rotor having permanent magnets and a stator having a multiplicity of teeth separated from each other wherein the tooth tip has a substantially rectangular-shaped cross section

Compressor bleed port structure

Radial cooling system for gas turbine engine compressors

TURBOCHARGER THRUST BEARING AND MANUFACTURING METHOD

Sealing system for a rotary machine and method of assembling same

Fairing ring for a bladed wheel

THREE SPOOL TURBOFAN ENGINE WITH LOW NOISE INTERMEDIATE TURBINE ROTOR

Multi-material turbine airfoil

Partially shrouded gas turbine engine fan

Turbofan engine bearing and gearbox arrangement

Structure for mitigating vibratory modes of counter-rotating engine rotors

Asymmetrical shroud for a compressor of a turbine engine

Shroud having elevations, for a turbomachine compressor

Compressor for turbine engine

Method for manufacturing a rotor for a turbine engine high-pressure compressor

Rotor disk assembly for gas turbine

Tuned retention ring for rotor disk

Gas turbine engine with axial movable fan variable area nozzle

Compact aero-thermo model based engine material temperature control

Bladed disk

Compact aero-thermo model based control system

Mistuned compressor rotor with hub scoops

Turbine engine seal for high erosion environment

Compressor rotor, compressor and gas turbine

HIGH YIELD STRENGTH NICKEL ALLOY WITH AUGMENTED PRECIPITATION HARDENING

Gas turbine rotor, gas turbine, and gas turbine equipment

Compact aero-thermo model based engine power control

Compact aero-thermo model base point linear system based state estimator

Compact aero-thermo model stabilization with compressible flow function transform

Fluid-cooled seal arrangement for a gas turbine engine

Rotary machines including a hybrid rotor with hollow and solid rotor blade sets

Cooling system for a turbine engine

AXI-CENTRIFUGAL COMPRESSOR

Methods for optimized engine balancing based on flight data

Method and system for compressor vane leading edge auxiliary vanes

Turbo compressor having an inner passage for cooling the motor

Pin to reduce relative rotational movement of disk and spacer of turbine engine

TURBOMACHINE WITH AN ADAPTIVE SEALING APPLIANCE

Compressor having reinforcing disk, and gas turbine having same

Nickel-base superalloy

Inter-shaft bearing connected to a compressor boost system

Bearing outer race retention during high load events

Rim seal

Compact aero-thermo model real time linearization based state estimator

Short impeller for a turbomachine

Turbine rotor with low over-speed requirements

Forced induction engine with electric motor for compressor

Contouring a blade/vane cascade stage

Disk assembly for gas turbine compressor

RADIAL VARIABLE INLET GUIDE VANE FOR AXIAL OR AXI-CENTRIFUGAL COMPRESSORS

METHOD OF REPAIRING A BLISK

LNG PLANT INCLUDING AN AXIAL COMPRESSOR AND A CENTRIFUGAL COMPRESSOR

Gas turbine seal

BLADED DISC AND METHOD OF MANUFACTURING THE SAME

HIGH EFFICIENCY SELF-CONTAINED MODULAR TURBINE ENGINE POWER GENERATOR

Gas turbine engine compressors having optimized stall enhancement feature configurations and methods for the production thereof

Reverse flow engine architecture

Multiple axle-sleeve driving bidirectional rotating wheel-shaped fan turbine and a bushing wheel-shaped fan compressor

Brush seal assembly and method

GAS TURBINE ENGINE TANGENTIAL ORIFICE BLEED CONFIGURATION

Monolithic superstructure for load path optimization

Rotor shaft architectures for a gas turbine engine and methods of assembly thereof

Seal assembly

Method and system for elastic bearing support

Deicing nose of an axial turbine engine compressor

Bearing housing with impingement cooling system

Sealing fin having an axially asymmetric tip portion

Coolant flow redirection component

Rotor stage for a turbomachine, rotor drum, and rotor

Tri-axial capacitance probe with case integrated housing

Fire containment coating system for titanium

Gas turbine engine with progressive stall recovery

Floating non-contact seal vertical lip

Floating, non-contact seal with at least three beams

Floating, non-contact seal with angled beams

Floating, non-contact seal with offset build clearance for load imbalance

Compressor rotor, compressor, and gas turbine

Gas turbine engine with axial movable fan variable area nozzle

Mechanically driven air vehicle thermal management device

Direct drive aft fan engine

Method and apparatus for active clearance control on gas turbine engines

Engine with face seal

Gas turbine engine with axial movable fan variable area nozzle

Assembly and method for influencing flow through a fan of a gas turbine engine

Rotary friction welding

STATIC HUB TRANSITION DUCT

Gas turbine engine with axial movable fan variable area nozzle

Singular stator vane control

THICKENED RADIALLY OUTER ANNULAR PORTION OF A SEALING FIN

Mini-disk for gas turbine engine

Engine bleed air system with waste gate valve for compressor surge management

BOOSTER COMPRESSOR WITH SPEED CHANGE SYSTEM

Axial flow compressor assembly

Axial compressor with radially outer annulus

Service routing configuration for a gas turbine engine diffuser system

Active core cooling system

Compression system for a turbine engine

Heat exchanger with decreased core cross-sectional areas

METHOD FOR MANUFACTURING A COMPRESSOR IMPELLER

AIRFLOW MANIPULATION DEVICE FOR COMPRESSOR

Abrasive blade tips with additive layer resistant to clogging

Organic matrix abradable coating resistant to clogging of abrasive blade tips

EFFICIENT LOW PRESSURE RATIO PROPULSOR STAGE FOR GAS TURBINE ENGINES

Heat exchanger with heat resistant center body

Piezoelectric damping rings

Downhole wet gas compressor processor

Rotary machine with gas bearings

Contra-flow strips, contra-flow seal segments, and methods for inhibiting leakage

COMPRESSOR SECONDARY FLOW AFT CONE COOLING SCHEME

BRAZE MATERIAL FOR HYBRID STRUCTURES

Shaft and a turbomachine

AXI-CENTRIFUGAL COMPRESSOR

Vane ring, inner ring, and turbomachine

Low hub-to-tip ratio fan for a turbofan gas turbine engine

Methods for processing bonded dual alloy rotors including differential heat treatment processes

Connection of rotatable parts

Real time rotation breakaway detection

Gas turbine engine with ring damper

FLEXIBLE SUPPORT STRUCTURE FOR A GEARED ARCHITECTURE GAS TURBINE ENGINE

Bearing outer race retention during high load events

Method for clearance control in a gas turbine engine

Floating, non-contact seal and dimensions thereof

Compressor rotor with anti-vortex fins

ROTOR-STATOR COMBINATION FOR AN AXIAL TURBOMACHINE AND AERO ENGINE

Method of balancing a gas turbine engine rotor

Compressor aft rotor rim cooling for high OPR (T3) engine

RIM FACE SCALLOP FOR INTEGRALLY BLADED ROTOR DISK

Lubrication device for a turbine engine

GRAPHENE ULTRA-CONDUCTIVE CASING WRAP

Systems and methods for a compressor diffusion slot

Method and system for improving structural characteristics of composite component corners

Method and system for centrifugal pump

LOW NOISE TURBINE FOR GEARED TURBOFAN ENGINE

Compressor and method for mounting of a compressor

Method and apparatus for active clearance control for high pressure compressors using fan/booster exhaust air

Gas turbine engine with short inlet and blade removal feature

Active high pressure compressor clearance control

Gas turbine combustion acoustic damping system

METHOD FOR METERING MICRO-CHANNEL CIRCUIT

Flywheel with Inner Turbine, Intermediate Compressor, and Outer Array of Magnets

Fastening assembly

Disk assembly and turbine including the same

Outer airseal for gas turbine engine

Turbine airfoil with passive morphing structure

De-oiler balance weights for turbomachine rotors and systems for removing excess oil from turbomachine rotors

Gas turbine engine with vane having a cooling inlet

Multistage compressor with aerofoil portion profiled in a spanwise direction

SYSTEM AND METHOD FOR APPLYING A TENSILE LOAD TO A COMPONENT

Self-contained lubrication cooling system with heat exchanger integrated with sump

Compressor

GAS TURBINE ENGINE WITH HIGH SPEED LOW PRESSURE TURBINE SECTION AND BEARING SUPPORT FEATURES

Geared gas turbine engine

Reduced stress rotor interface

SYSTEMS AND METHODS TO FACILITATE ENHANCING TURBINE OUTPUT USING AN AUXILIARY GENERATOR

ROTOR SEAL AND ROTOR THRUST BALANCE CONTROL

Gas turbine cooling apparatus

Containment for a continuous flow machine

FLOW GUIDING DEVICE AND TURBO-ENGINE WITH AT LEAST ONE FLOW GUIDING DEVICE

Compressor stator vane, axial flow compressor, and gas turbine

Method and system for modulated turbine cooling

Turbine engine advanced cooling system

Planet gearbox with cylindrical roller bearing with high density roller packing

DOUBLE ROW CYLINDRICAL ROLLER BEARING WITH HIGH LENGTH TO DIAMETER RATIO ROLLERS

Nickel-base superalloy

COUPLING FOR A GEARED TURBO FAN

Gas turbine engine with axial movable fan variable area nozzle

Composite booster spool with separable composite blades

Gas turbine engine with axial movable fan variable area nozzle

Gas turbine engine with axial movable fan variable area nozzle

Geared turbofan engine gearbox arrangement

Turbine cap for turbo-molecular pump

SYSTEM AND METHOD FOR MAINTAINING EMISSIONS COMPLIANCE WHILE OPERATING A GAS TURBINE AT TURNDOWN CONDITION

Magnetic squeeze film damper system for a gas turbine engine

Apparatus and method for water and ice flow management in a gas turbine engine

Axial flow compressor, gas turbine including the same, and stator blade of axial flow compressor

Perforated drum of a compressor of an axial turbine engine

Patch ring for a compressor

Rotor disc and rotor for a vacuum pump

Rotor structure for rotating machinery and method of assembly thereof

Surge free subsea compressor

High pressure compressor diffuser for an industrial gas turbine engine

Turbomachine component or collection of components and associated turbomachine

Supply of air to an air-conditioning circuit of an aircraft cabin from its turboprop engine

COOLED COMPRESSOR

FAN-DRIVE GEAR SYSTEM WITH SEPARATE SCAVENGE PUMP

Cantilevered stator vane and stator assembly for a rotary machine

Axial turbomachine compressor casing

Windmill and negative-G oil system for geared turbofan engines

Gas turbine engine

Pump for a turbine engine

Stator device for a continuous-flow machine with a housing appliance and multiple guide vanes

Stator device for a continuous-flow machine with a housing appliance and multiple guide vanes

Radial tie-bolt support spring

Auxiliary power unit with intercooler

TANDEM ROTOR BLADES WITH COOLING FEATURES

Airfoil, and method for manufacturing the same

Efficient power and thermal management system for high performance aircraft

ROTOR FOR A TURBOMACHINE AND COMPRESSOR

Turbomachine comprising a shaft sleeve and associated sleeve tube

Fire containment coating system for titanium

Oil-cooled gas compressor

Turbine engine with a turbo-compressor

Methods of washing gas turbine engines and gas turbine engines

GEARED TURBOFAN ENGINE WITH COUNTER-ROTATING SHAFTS

Internally cooled turbine blisk and method of manufacture

Supply of air to an air-conditioning circuit of an aircraft cabin from its turboprop engine

AXIAL COMPRESSOR AND USE OF AN AXIAL COMPRESSOR

Rotor disk having a centripetal air collection device, compressor comprising said disc and turbomachine with such a compressor

Blade outer air seal mount

Retention clip for a blade outer air seal

Supply of air to an air-conditioning circuit of an aircraft cabin from its turboprop engine

ROTOR DRUM FOR A TURBOMACHINE AND COMPRESSOR

Rotor arrangement for a turbomachine and compressor

Gas turbine engine integrally bladed rotor with asymmetrical trench fillets

ABRASIVELY MACHINED GAS TURBINE COMPONENTS

Control concept for closed loop Brayton cycle

Bladed gas turbine engine rotors having deposited transition rings and methods for the manufacture thereof

Noise reduction using IGV flow ejections

Adaptive turbomachine cooling system

System and method for operating a compressor

Process for testing a compressor or a combustor of a gas turbine engine using a large compressed air storage reservoir

Washing nozzles and gas turbine engines

Shroud assembly and shroud for gas turbine engine

Modular engine, such as a jet engine, with a speed reduction gear

Rotating labyrinth M-seal