Trip strip restagger

Fluid injector for cooling a gas turbine engine component

Mid-turbine frame assembly

Insert and standoff design for a gas turbine engine vane

Turbine vane with load shield

Flow splitting first vane support for gas turbine engine

Cooling passages for a mid-turbine frame

Cooling passages for a mid-turbine frame

Tie rod for a mid-turbine frame

Cooling passages for a mid-turbine frame

Cooling passages for a mid-turbine frame

Cooling passages for a mid-turbine frame

Cooling passages for a mid-turbine frame

Turbine exhaust cylinder/turbine exhaust manifold bolted full span turbine exhaust flaps

Leakage air systems for turbomachines

Gas turbine engine diffuser cooling and mixing arrangement

Tangential on-board injection vanes

Variable area turbine arrangement with secondary flow modulation

Multi-function boss for a turbine exhaust case

Cooling for gas turbine engine components

Turbo machine having a sealing unit, maintenance method, and associated maintenance device

Gas turbine engine component providing prioritized cooling

Turbomachine auxiliary lead-through device

Baffle for gas turbine engine vane

Diffuser case mixing chamber for a turbine engine

Intergrated seal supports

Compliant seal assembly and method of operating

Airfoil profile-shaped seals and turbine components employing same

Gas turbine engine mid-turbine frame tie rod arrangement

Pre-diffuser strut for gas turbine engine

Reversible flow blade outer air seal

Cooling of engine components

Gas turbine engine forward bearing compartment architecture

Inner diffuser case cone and skirt

Turbine airfoil platform segment with film cooling hole arrangement

Moment accommodating fastener assembly

Cooling system of a stator assembly for a gas turbine engine having a variable cooling flow mechanism and method of operation

Hot gas components with compound angled cooling features and methods of manufacture

Sealing interface for a case of a gas turbine engine

Fully integrated air guide element

Supply duct for cooling air from gas turbine compressor

Oil distributor

Gas turbine engine

Vane assembly for a gas turbine engine

Vane assembly for a gas turbine engine

Cooled component

Corrugated mid-turbine frame thermal radiation shield

Gas turbine engine with dove-tailed TOBI vane

Power turbine cooling air metering ring

Power turbine heat shield architecture

Cooled component

Internal cooling of engine components

Cooled component

Diffuser case strut for a turbine engine

Gas turbine engine

Turbine engine diffuser assembly with airflow mixer

Plate for metering flow

Gas turbine nozzles with embossments in airfoil cavities

Film hole with in-wall accumulator

Air guiding device and aircraft engine with air guiding device

Double-jet film cooling structure and method for manufacturing same

Beveled coverplate

Structural frame integrated with variable-vectoring flow control for use in turbine systems

Article and process for producing an article

CERAMIC MATRIX COMPOSITE COMPONENTS WITH INSERTS

Ducting platform cover plate

Engine mid-turbine frame transfer tube for low pressure turbine case cooling

Guide blade for a gas turbine

High temperature disk conditioning system

Multi-lobed cooling hole

Additive manufacturing baffles, covers, and dies

TURBULATING COOLING STRUCTURES

Gas turbine engine component having shaped pedestals

Cooled composite sheets for a gas turbine

Method and apparatus for collecting pre-diffuser airflow and routing it to combustor pre-swirlers

Method and apparatus for handling pre-diffuser airflow for use in adjusting a temperature profile

Method and apparatus for handling pre-diffuser flow for cooling high pressure turbine components

Method and apparatus for handling pre-diffuser airflow for cooling high pressure turbine components

Intermediate casing for a turbofan engine

Cleaning system for a turbofan gas turbine engine

Cooling hole for a gas turbine engine component

Gas turbine engine component cooling channels

Additive manufacturing method for the addition of features within cooling holes

Instrumentation transfer strut

Method and apparatus for selectively collecting pre-diffuser airflow

Method and apparatus for handling pre-diffuser airflow for cooling high pressure turbine components

Gas turbine engine component paired film cooling holes

Half-spoolie metal seal integral with tube

Gas turbine engine composite airfoil trailing edge

Cooling hole for a gas turbine engine component

Gas turbine engine component with combined mate face and platform cooling

Gas turbine engine component having curved turbulator

Multi-segment adjustable stator vane for a variable area vane arrangement

Split airfoil cluster and method therefor

Multi-airfoil split and rejoin method

Mid-frame for a gas turbine and gas turbine having such a mid-frame

Multi-circuit lubrication system for a turbine engine

Fluid collection gutter for a geared turbine engine

Cooling passages for inner casing of a turbine exhaust

Engine systems and methods for removing particles from turbine air

Plug assembly with retaining element

Flapper seal apparatus and system

EXHAUST FRAME COOLING VIA STRUT COOLING PASSAGES

Multi-airfoil split and rejoin method to produce enhanced durability coating

Frame junction cooling holes

Instrumented flow passage of a turbine engine

Heat shield for a casing

Heated inlet guide vane

Vane support systems

Double tube connecting device

Cooling structure for stationary blade

Cooling systems for gas turbine engine components

Angled cut to direct radiative heat load

Cooling architecture for turbine exhaust case

Scupper channelling in gas turbine modules

Turbine nozzles and cooling systems for cooling slip joints therein

Fluid system

Geared turbofan gas turbine engine architecture

Turbine exhaust case architecture

Heat shield for cooling a strut

Multi-purpose gas turbine seal support and assembly

Distributor device for cooling air within an engine

Bifurcation fairing

Shrouded conduit for arranging a fluid flowpath

Blade cooling circuit feed duct, exhaust duct, and related cooling structure

Stator vane formed by a set of vane parts

Method of reducing manufacturing variation related to blocked cooling holes

Turbomachine thermal management

Heat shield based air dam for a turbine exhaust case

Integrated heat exchangers for low fan pressure ratio geared turbofan

Cooling system with a bearing compartment bypass

Air stream mixing inner diameter (ID) cavity

Gas turbine engine forward bearing compartment architecture

Gas turbine engine turbine vane platform cooling

Method of supporting a tool and an apparatus for supporting a tool in an assembled apparatus

Turbine vane with cooled fillet

Inner diffuser case struts for a combustor of a gas turbine engine

Gas turbine duct casing

MODULAR TURBOMACHINE INNER AND OUTER CASINGS WITH MULTI-STAGE STEAM EXTRACTION SITES

Split-zone flow metering T-tube

Air supply device for aircraft engine turbines

Baffle with flow augmentation feature

Seal assembly for a static structure of a gas turbine engine

Method of operating a gas turbine assembly and the gas turbine assembly

Ceramic pedestal and shield for gas path temperature measurement

Fluid transport system having divided transport tube

Turbine nozzle and method for cooling a turbine nozzle of a gas turbine engine

Steam turbine and methods of assembling the same

Nozzle endwall film cooling with airfoil cooling holes

Supporting structure for a gas turbine engine

Multi-orifice plate for cooling flow control in vane cooling passage

Drain pipe arrangement and gas turbine engine comprising a drain pipe arrangement

Cooled airfoil trailing edge and method of cooling the airfoil trailing edge

Aircraft engine driveshaft vessel assembly and method of assembling the same

Annular cover delimiting a turbomachine lubrication chamber

Gas turbine airfoil

Bracket for mounting a stator guide vane arrangement to a strut in a turbine engine

Turbine and power generation system

Arrangement for cooling a component in the hot gas path of a gas turbine

Coolant bridging line for a gas turbine, which coolant bridging line can be inserted into a hollow, cooled turbine blade

Method and system for providing cooling for turbine components

Internally cooled airfoil

Internally cooled airfoil

Disc axis adjusting mechanism in gas turbine

Thermal isolating service tubes and assemblies thereof for gas turbine engines

Fixed turbine engine receiver part comprising an assembly for holding ancillary systems in position inside a fixed hollow shaft

Impingement cooling of turbine blades or vanes

Fluid cooling arrangement for a gas turbine engine and method

Cooled turbine guide vane or blade for a turbomachine

Gas turbine with high-pressure turbine cooling system

Cooling hole with curved metering section

Hollow-blade turbine vane made from composite material, turbine or compressor including a nozzle or guide vane assembly formed by such blades, and turbomachine comprising same

Interface device between two turbomachine elements

Gas turbine engine combustor with integrated combustor vane having swirler

Turbine nozzles and methods of manufacturing the same

Turbine blade

Strut for a gas turbine engine

Gas turbine engine cooling arrangement

Gas turbine outer case active ambient cooling including air exhaust into sub-ambient cavity

Turbine blade

Modular turbomachine inlet assembly and related inlet transition section

Cooled ceramic matrix composite airfoil

Gas turbine engine diffuser system for a high pressure (HP) compressor

Axial-flow turbine and power plant including the same

Chamber fluid removal system

Bifurcated inlet scoop for gas turbine engine

Flow diverter to redirect secondary flow

Mid-turbine frame vane assembly support with retention unit

Multi-lobed cooling hole

Gas turbine engine vane embedded beam interrupt optical tip-timing probe system

Purge and cooling air for an exhaust section of a gas turbine assembly

Multiple piece shroud feedthru enclosure

Fuel-cooled bladed rotor of a gas turbine engine

Component retention with probe

Gas turbine engine including a pre-diffuser heat exchanger

Anti-ice supply system for inlet guide vanes

Turbomachine

Full ring inner air-seal with locking nut

Turbine engine drive shaft device

Film cooling channel array with multiple metering portions

Temperature control within a cavity of a turbine engine

Film cooling channel array having anti-vortex properties

Turbine stator airfoil assemblies and methods for their manufacture

Turbomachine with bleed valves located at the intermediate case

Method for assembling a nozzle and an exhaust case of a turbomachine

Threaded full ring inner air-seal

Forward compartment service system for a geared architecture gas turbine engine

Closed loop cooling system for a gas turbine

Seal apparatus of turbine and thermal power system

Vane insertable tie rods with keyed connections

Airfoil cooling arrangement

Corrugated mid-turbine frame thermal radiation shield

Mid-turbine frame thermal radiation shield

FLOW METERING ANTI-ROTATION OUTER DIAMETER (OD) HEX NUT

Cooling apparatus for a mid-turbine frame

Gas turbine engine component with discharge slot having oval geometry

Cooled component for the turbine of a gas turbine engine

Cooling for a turbine airfoil trailing edge

Heat shield for a low-pressure turbine steam inlet duct

Nacelle bifurcation for gas turbine engine

Self-sealing tube for a gas turbine secondary air system

Method and device for modifying a secondary air system in a gas turbine engine

Shield system for gas turbine engine

TURBINE AIRFOIL TRAILING EDGE BIFURCATED COOLING HOLES

Turbomachine thermal management

Oil discharge device and turbomachine comprising such a device

Gas turbine frame stiffening rails

Gas turbine engine bearing support strut

Turbine frame fairing for a gas turbine engine

Gas turbine

Gas turbine engine buffer cooling system

Gas turbine engine component with multi-lobed cooling hole

Gas turbine engine component with compound cusp cooling configuration

GAS TURBINE ENGINE COMPONENT WITH CUSPED, LOBED COOLING HOLE

Multiple diffusing cooling hole

Cooling hole with enhanced flow attachment

Gas turbine engine component with cusped cooling hole

Gas turbine engine component with diffusive cooling hole

Manufacturing methods for multi-lobed cooling holes

EDM method for multi-lobed cooling hole

Cooling hole with crenellation features

Multi-lobed cooling hole and method of manufacture

Gas turbine engine component with impingement and lobed cooling hole

Gas turbine engine component with impingement and diffusive cooling

Cooling hole with asymmetric diffuser

Cooling hole with curved metering section

Multi-lobed cooling hole and method of manufacture

Tri-lobed cooling hole and method of manufacture

Cooling hole with thermo-mechanical fatigue resistance

Customer bleed air pressure loss reduction

Method and apparatus to control part-load performance of a turbine

Internal manifold for turning mid-turbine frame flow distribution

Geared turbofan gas turbine engine architecture

TURBINE EXHAUST DIFFUSER SYSTEM MANWAYS

Oil purge system for a mid turbine frame

Start system for gas turbine engines

GAS TURBINE EXHAUST DIFFUSER HAVING PLASMA ACTUATOR

Casing for an aircraft turbofan bypass engine

Impingement cooling system for use with contoured surfaces

Turbine nozzle compartmentalized cooling system

Turbine to operate at part-load

High pressure turbine vane cooling hole distribution

Ambient air cooling arrangement having a pre-swirler for gas turbine engine blade cooling

Use of multi-faceted impingement openings for increasing heat transfer characteristics on gas turbine components

Steam turbine arrangement of a three casing supercritical steam turbine

EXHAUST GAS DIFFUSER

Offset counterbore for airfoil cooling hole

Air system architecture for a mid-turbine frame module

Gas turbine

Method and apparatus for segregated oil supply and scavenge in a gas turbine engine

Airfoil including trench with contoured surface

Gas turbine and turbine stationary blade for same

STRUT, A GAS TURBINE ENGINE FRAME COMPRISING THE STRUT AND A GAS TURBINE ENGINE COMPRISING THE FRAME

Gas turbine engine systems involving I-beam struts

Flowpath insert and assembly

Turbine nozzle slashface cooling holes

Gas turbine engine compressor case mounting arrangement

Method of reducing asymmetric fluid flow effects in a passage

Method of supporting a tool and an apparatus for supporting a tool in an assembled apparatus

Gas-turbine balancing device

Rear hub cooling for high pressure compressor

Method for producing a component with at least one element arranged in the component

METHOD FOR COOLING TURBINE STATORS AND COOLING SYSTEM FOR IMPLEMENTING SAID METHOD

Load limited actuator

CMC turbine nozzle adapted to support a metallic turbine internal casing by a radial contact

CMC turbine nozzle adapted to support a metallic turbine internal casing by an axial contact

Communicating structure between adjacent combustors and turbine portion and gas turbine

System for cooling and purging exhaust section of gas turbine engine

Process for the vapor phase aluminization of a turbomachine metal part and donor liner and turbomachine vane comprising such a liner

Gas turbine engine

Steam seal dump re-entry system

STRUT AIRFOIL DESIGN FOR LOW SOLIDITY EXHAUST GAS DIFFUSER

SYSTEM AND METHOD FOR A GAS TURBINE EXHAUST DIFFUSER

LEADING EDGE AIRFOIL-TO-PLATFORM FILLET COOLING TUBE

Axial compressor and associated operating method

Steam turbine nozzle assembly having flush apertures

Endwall component for a turbine stage of a gas turbine engine

Turbine exhaust plenum

Gas turbine engine havinga rotatable off-take passage in a compressor section

Device for spray lubrication of a wind turbine transmission