MITIGATION STRATEGY FOR AIRFOIL CRACKS FOR INTEGRALLY BLADED ROTORS

Metallic Substrate Laser Treatment

ASSEMBLY FOR A TURBINE ENGINE

FLEXIBILITIES IN A GAS TURBINE ENGINE WITH SPEED REDUCER

TRANSFER OF POWER BETWEEN THE HIGH-PRESSURE SHAFT AND THE LOW-PRESSURE SHAFT OF A TURBOMACHINE

Rotor blade and gas turbine provided therewith

ROTOR OF A GAS TURBINE, AND METHOD FOR PRODUCING A ROTOR

Rotor bow mitigation

Bowed-rotor mitigation system for a gas turbine

CASE COMPRISING INTERNAL AND/OR EXTERNAL STIFFENERS

Turbine component with heated structure to reduce thermal stress

Airfoil ribs for rotor blades

Rotor having crack mitigator

Method and apparatus for cooling turbine blades

ROTOR BLADE FOR A GAS TURBINE

Airfoil for a turbomachine

SYSTEM AND METHOD FOR GAS TURBINE ENGINE ROTOR BOW MITIGATION

Rotor for a turbomachine and turbomachine

Turbine blade and turbine

Transition piece, combustor, and gas turbine engine

Method of reducing turbine wheel high cycle fatigue in sector-divided dual volute turbochargers

Blade intake

ASSEMBLY FOR A TURBINE ENGINE

Blade root receptacle for receiving a rotor blade

Turbine rotor blade

System for controlling the cyclic setting of blades

Thrust reverser with anti-buckling actuating system

Integrally repaired bladed rotor

Engine component with modification area for influencing crack propagation and method of manufacturing

ROTOR BLADE FOR A TURBOMACHINE, ASSOCIATED TURBINE MODULE, AND USE THEREOF

Rotor blade for a turbomachine, associated turbine module, and use thereof

Turbine vane provided with a recess for embrittlement of a frangible section

Gas turbine engine with pre-conditioned ceramic matrix composite components

Stiffened torque tube for gas turbine engine

Thermally isolated rotor systems and methods

Combustor and gas turbine including the same

Gas turbine engine operating schedules for optimizing ceramic matrix composite component life

Gas turbine combustor

Rounded radial snap configuration for a gas turbine engine cover plate

Fuel injector systems and support structures

Gas turbine engine with pre-conditioned ceramic matrix composite components

Impeller and rotary machine

Exhaust nozzle of a gas turbine engine

Exhaust nozzle of a gas turbine engine

Turbmachine fan disc

Steam turbine and method for operating same

GAS TURBINE COMBUSTOR

Engine with cooling passage circuit extending through blade, seal, and ceramic vane

Gas turbine engine airfoils having multimodal thickness distributions

Fan blade attachment root with improved strain response

Multi-blade vane for a turbomachine rotor and rotor comprising same

Methods for producing gas turbine engine rotors and other powdered metal articles having shaped internal cavities

Stiffened torque tube for gas turbine engine

Internally cooled turbine blade with creep reducing divider wall

Pre-diffuser for a gas turbine engine

BOAS and methods of making a BOAS having fatigue resistant cooling inlets

Turbine blade tip wall cooling

Continuous wedge vane arm with failsafe retention clip

Inter-component seals for ceramic matrix composite turbine vane assemblies

Stress reduction structure, gas turbine casing, and gas turbine

Reinforced axial diffuser

Turbine wheel assembly

Modified aircraft idle for reduced thermal cycling

Blade retainer for gas turbine engine

Variable pitch blade holder for gas turbine engine

Spigot assembly for rotating components

Fan blade attachment root with improved strain response

Mini-disk for gas turbine engine

Turbine shroud having ceramic matrix composite seal segment

Balance bracket

Reduced stress boss geometry for a gas turbine engine

GAS TURBINE

Jacket ring assembly for a turbomachine

Density gradient in blade to reduce centrifugal load

Airfoil for a turbomachine

Airfoil of axial flow machine

Shield for arranging between a bearing and a rotating seal element

Double bore basket

Guide vane airfoil for the hot gas flow path of a turbomachine

Shroud segment for disposition on a blade of a turbomachine, and blade

AIRCRAFT NOZZLE

Casing of a turbocharger and turbocharger

Blade for a gas turbine engine

Housing arrangement for a turbomachine as well as turbomachine arrangement having such a housing arrangement and method for manufacturing the housing arrangement

Combustor Assembly for a Turbine Engine

Fuel injector systems and support structures

System and method for rotor bow mitigation

Gas turbine engine vane attachment feature

SUPPORTING DEVICE FOR A CASING OF A TURBOMACHINE, CASING FOR A TURBOMACHINE, AND TURBOMACHINE

Thermal gradient attenuation structure to mitigate rotor bow in turbine engine

Turbine blade of a turbine blade ring

Turbine bucket with a cooling circuit having asymmetric root turn

Turbine housing

Blade and rotor for a turbomachine and turbomachine

Gas turbine disk

Combustor and gas turbine including the same

Impeller, rotary machine, and turbocharger

Bladed disk

CONTOURED CASE BOSSES FOR A GAS TURBINE ENGINE

MULTIDIRECTIONALLY DEFLECTABLE MOUNTING APPARATUS AND METHOD

Gas turbine

Blade for a turbomachine

Contact interface for a composite component and methods of fabrication

Compressor rotor disk for gas turbine

Turbine disk

Turbine disk

Turbine disk

Rectifier for aircraft turbomachine compressor, comprising air extraction openings having a stretched form in the peripheral direction

Turbine nozzle with stress-relieving pocket

Stator vane segment for a turbomachine

Aircraft component and gas turbine engine for aircraft

Guide vane segment with curved relief gap

Gas turbine engine hollow fan blade rib orientation

GAS TURBINE DISC

Expansion joint and methods of assembling the same

Aircraft engine lubrication circuit and method, using a non-return pressurisation valve with two plugs

Elliptical slot with shielding holes

COMPOSITE TURBOMACHINE COMPONENT AND RELATED METHODS OF MANUFACTURE AND REPAIR

Assembly of tube and structure crossing multi chambers

Turbine shroud assembly

Transient control to extend part life in gas turbine engine

ROTOR DISK ASSEMBLY FOR A GAS TURBINE ENGINE

Methods for producing gas turbine engine rotors and other powdered metal articles having shaped internal cavities

Support unit for power unit, and turbine having the same

Centrifugal impeller for a turbine engine

Mechanical flywheel for bowed rotor mitigation

Engine turning motor via pneumatic or hydraulic motor

Connecting element

Two-shaft tower shaft support

High temperature disk conditioning system

Turbine engine and method of manufacturing

VARIABLE NOZZLE MECHANISM AND VARIABLE CAPACITY TURBOCHARGER

Turbine engine exhaust casing with improved lifetime

Mount structure for an aircraft ancillary engine unit

SYSTEM AND METHOD FOR FAST STARTUP OF A COMBINED CYCLE POWER PLANT

Blade comprising a shank, provided with a depressed portion

SEALING SYSTEM FOR AN AXIAL TURBOMACHINE AND AXIAL TURBOMACHINE

Airfoil with retention pocket holding airfoil piece

Undercut on airfoil coversheet support member

Gas turbine engine airfoils having multimodal thickness distributions

Apparatus and system for marine propeller blade dovetail stress reduction

Component assembly for a gas turbine engine

Fan for aircraft turbomachine

Modular fan assembly

Positioning element with recesses for a guide vane arrangement

SHIM FOR GAS TURBINE ENGINE

Liner element for a turbine intermediate case

Borescope plug

Assembly for supporting an annulus

Radially connected cascade grids

Mini-disk for gas turbine engine

Component for a gas turbine engine

Contoured retaining ring

Blade with stress-reducing bulbous projection at turn opening of coolant passages

Gas turbine engine having a vane assembly

Creep resistant axial ring seal

Gas turbine engine with compliant layer for turbine vane assemblies

Heat shield with axial retention lock

Blade outer air seal with centrally mounted seal arc segments

Bowed rotor start using direct temperature measurement

Bowed rotor prevention system using waste heat

Thermal stress relief of a component

TURBINE BLADE AND TURBINE

Turbine engine airfoil with cooling

Turbine blade attachment curved rib stiffeners

Exhaust frame

Vane, gas turbine, ring segment, remodeling method for vane, and remodeling method for ring segment

Rotary machine, method of assembling rotary machine, and method of performing maintenance of rotary machine

Rotor for gas turbine engine

Converging flow joint insert system at an intersection between adjacent transitions extending between a combustor and a turbine assembly in a gas turbine engine

Reduced stress rotor interface

Turbine blade

Gas turbine disk

FLOW PATH TRENCHES AND METHODS OF FORMING THE SAME

Shafting arrangement for a gas turbine engine

Combustor assembly for a turbine engine

Combustor assembly for a turbine engine

Control system for managing steam turbine rotor stress and method of use

Turbine band anti-chording flanges

Heat exchanger for cooled cooling air

Turbine shroud having ceramic matrix composite seal segment

Composite fan

Composite fan and method of manufacture

Article, airfoil component and method for forming article

Diffuser part for a gas turbine

Seal segment for a gas turbine engine

Method and system for interfacing a ceramic matrix composite component to a metallic component

Turbine component thermal barrier coating with depth-varying material properties

Turbine component thermal barrier coating with crack isolating engineered groove features

Igniter assembly for a gas turbine engine

Reduced stress boss geometry for a gas turbine engine

Fan blade attachment root with improved strain response

Trailing edge platform seals

Sheet-metal turbine housing

Composite airfoil metal patch

Rotary blade manufacturing method

Intermittent grooved soft abradable material to reduce blade tip temperature

Compliant attachment for an organic matrix composite component

BLADE

Turbine bucket cooling

Compressor system and airfoil assembly

BLADE/DISK DOVETAIL BACKCUT FOR BLADE/DISK STRESS REDUCTION FOR A SECOND STAGE OF A TURBOMACHINE

PROTECTIVE BEARING, BEARING UNIT, AND VACUUM PUMP

Heat shields for air seals

Coupling part structure for vane and jet engine including the same

Rotating labyrinth M-seal

Turbine housing

Hybrid nozzle segment assemblies for a gas turbine engine

Cooling passages for a mid-turbine frame

COOLING SYSTEM FOR A GAS TURBINE

Turbine engine combustor heat shield with multi-angled cooling apertures

Brushing retention of threaded fastener

Compound fillet varying chordwise and method to manufacture

Turbocharger turbine assembly

Inner diffuser case for a gas turbine engine

Compound fillet for a gas turbine airfoil

Method and system for a ceramic matrix composite shroud hanger assembly

Machined film holes

Rotor disc

Forward-swept impellers and gas turbine engines employing the same

Turbine blade, set of turbine blades, and fir tree root for a turbine blade

Guide vane ring for a turbomachine

Radially connected cascade grids

Gas turbine engine control for rotor bore heating

Turbomachine flow path having circumferentially varying outer periphery

Gas turbine engine truncated airfoil fillet

Shielding pockets for case holes

Turbine blade platform undercut with decreasing radii curve

Intergrated seal supports

Gas turbine vane

Slots for turbomachine structures

Rotating blade for a gas turbine

Rotor disk assembly for a gas turbine engine

HYBRID BONDED TURBINE ROTORS AND METHODS FOR MANUFACTURING THE SAME

BLISK rim face undercut

Single-piece blisk for turbomachine fan comprising an upstream and/or downstream recess making its blades more flexible

Fairing for a mixer of a nozzle of a dual-flow turbomachine

Gas turbine engine and frame

Turbine rotor nut and bolt arrangement with improved fatigue resistance under centrifugal load

Stator assembly with pad interface for a gas turbine engine

Composite component

Turbine engine comprising a device for braking the fan rotor

Stator assembly for a gas turbine engine

Combustor arrangement with fastening system for combustor parts

Methods and apparatus to validate translated guest code in a dynamic binary translator

Methods for producing gas turbine engine rotors and other powdered metal articles having shaped internal cavities

Integrally bladed rotor

Fan hub design

Shield for arranging between a bearing and a rotating seal element

AXIAL FLOW COMPRESSOR AND GAS TURBINE EQUIPPED WITH AXIAL FLOW COMPRESSOR

Rotor blade with a conic spline fillet at an intersection between a platform and a neck

High temperature disk conditioning system

Fan blade damping device

Turbomachine component with a stress relief cavity

Gas turbine spindle bolt structure with reduced fretting fatigue

Turbocharger

Rotor and gas turbine engine including same

Reduced vibratory response rotor for a gas powered turbine

Mount with deflectable tabs

Gas turbine engine components having sealed stress relief slots and methods for the fabrication thereof

Panel connection system and a method of using the same

Rotor shaft with cooling bore inlets

High durability turbine exhaust case

Structural configurations and cooling circuits in turbine blades

Methods and apparatus to validate translated guest code in a dynamic binary translator

Gas turbine case and reinforcement strut for same

High durability turbine exhaust case

Rotor of rotary machine and rotary machine

Gas turbine engine rotors including intra-hub stress relief features and methods for the manufacture thereof

SEAL SYSTEM

Waste gate valve

High durability turbine exhaust case

Method and system for relieving turbine rotor blade dovetail stress

Actuator support system and apparatus

Disc axis adjusting mechanism in gas turbine

Method for repairing wear marks on a rotor supporting the fan of a bypass engine

Turbine blade and turbine with improved sealing

Damping device for being situated between a housing wall and a casing ring of a housing of a thermal gas turbine

Compliant intermediate component of a gas turbine engine

Panel attachment system and a method of using the same

Igniter for a gas turbine

Connection structure of exhaust chamber, support structure of turbine, and gas turbine

Gas turbine engine support strut assembly

Labyrinth disk for a turbomachine

Device and method for preventing leakage of air between multiple turbine components

Rotor blade support structure

Turbine nozzles with slip joints and methods for the production thereof

Rotor blade for a turbomachine and turbomachine

Turbomachine blade reinforcement

Exhaust case for a turbomachine with a flexible hub

Mid-turbine frame with tensioned spokes

Turbine component, turbine blade, and turbine component fabrication process

Flexible connection between a wall and a case of a turbine engine

Gas turbine engine turbine diaphragm with angled holes

Gas turbine engine preswirler with angled holes

Process for producing a turbine housing and turbine housing

LAST STAGE BLADE INCLUDING A PLURALITY OF LEADING EDGE INDENTATIONS

Axial retention of a platform seal

Turbomachine monitoring system and method

TWO-PIECE DUCT ASSEMBLY