System and method for converting turbine cooling nozzle

Airfoil edge cooling channels

Flow arrangement for placing in a hot gas duct of a turbomachine

Turbomachine airfoil

Air inlet for a gas turbine engine

HYDROSTATIC NON-CONTACT SEAL WITH SEAL CARRIER ELIMINATION

AIR GUIDING SYSTEM IN AN AIRCRAFT TURBO ENGINE

Insert assembly, airfoil, gas turbine, and airfoil manufacturing method

Non-contact seal assembly for rotational equipment

Turbine engine component with an insert

Fluid cooling systems for a gas turbine engine

Oil jet for turbine engine with housing including sealing membrane

Additively manufactured hollow body component with interior curved supports

Debris filter apparatus for preventing clogging of turbine vane cooling holes

Assemblies and methods for cooling flowpath support structure and flowpath components

Systems and methods for manufacturing film cooling hole diffuser portion

Plenum for cooling turbine flowpath components and blades

Turbomachine including a cooling and turbine clearance control system having an air supply scoop

Flow modulating airfoil apparatus

Turbine engine with variable effective throat

Cored airfoil platform with outlet slots

Method of making a cooled airfoil assembly for a turbine engine

COOLING SYSTEM AND COOLING METHOD IN A GAS TURBINE

Engine component with insert

Adaptively opening backup cooling pathway

Adaptive cover for cooling pathway by additive manufacture

Adaptive cover for cooling pathway by additive manufacture

Gas turbine and component-temperature adjustment method therefor

Nozzle airfoil decoupled from and attached outside of flow path boundary

Passively-driven bleed source switching

Bleed flow safety system

Masking fixture

Compliant seal assembly and method of operating

GAS TURBINE ENGINE WITH FILM HOLES

Strut assembly for bearing compartment

Gas turbine engine components with air-cooling features, and related methods of manufacturing the same

Turbomachine thermal management

Intermediate case for an aircraft turbomachine comprising a lubricant passage end-piece connected to a case vane by a connection piece

FORWARD FACING TANGENTIAL ONBOARD INJECTORS FOR GAS TURBINE ENGINES

Turbine vane and gas turbine including the same

Repaired Airfoil with Improved Coating System and Methods of Forming the Same

Sealing assembly for a gas turbine

Vane cooling system

Cooled cooling air to blade outer air seal passing through a static vane

Flow diverter case attachment for gas turbine engine

Guide vane arrangement for gas turbine engine

Engine component with flow enhancer

Vane cooling system

Device for measuring the characteristics of an air flow

Cooled cooling air for blade air seal through outer chamber

Scavenge tube for a gas turbine engine

Blockage-resistant vane impingement tubes and turbine nozzles containing the same

High temperature disk conditioning system

Outlet guide vane for aircraft turbomachine, with improved lubricant cooling function

Gas turbine engine vanes

METHOD OF CONVERTING THE ENERGY OF A GASEOUS WORKING FLUID AND APPARATUS FOR THE IMPLEMENTATION THEREOF

Gas turbine engine component with flow separating rib

Integrated heat exchangers for low fan pressure ratio geared turbofan

Thermally compliant heatshield

Method of repairing turbine component using ultra-thin plate

Airflow straightening assembly having improved aerodynamic performances

Airfoil cooling structure

Threaded fitting for tube

Fitting for multiwall tube

Apparatus with thermal break

Gas turbine and gas turbine operating method

Multiwall tube and fitting for bearing oil supply

Airfoil turn caps in gas turbine engines

HOT GAS PATH COMPONENT WITH METERING STRUCTURE INCLUDING CONVERGING-DIVERGING PASSAGE PORTIONS

Turbine spider frame with additive core

Gas turbine engine forward bearing compartment architecture

Gas turbine engine forward bearing compartment architecture

Apparatus for supplying cooling air to a turbine

Internally cooled engine components

Trailing edge pressure and flow regulator

Component and method for forming a component

Turbine engine exhaust casing with improved lifetime

Method and system for ice tolerant bleed takeoff

Controlling tip clearance in a turbine

Blade, cut-back of blade or vane and gas turbine having the same

Thermal shielding in a gas turbine

GAS TURBINE WITH SECONDARY AIR SYSTEM

Gas turbine blade

Composite turbine vane with three-dimensional fiber reinforcements

Gas turbine

Dual wall airfoil with stiffened trailing edge

Cooling pocket for turbomachine nozzle

Airfoil trailing edge segment

Turbine vane assembly

INTEGRATED CASTING CORE-SHELL STRUCTURE FOR MAKING CAST COMPONENT WITH NON-LINEAR HOLES

Integrated casting core-shell structure for making cast component with cooling holes in inaccessible locations

INTEGRATED CASTING CORE-SHELL STRUCTURE FOR MAKING CAST COMPONENTS HAVING THIN ROOT COMPONENTS

Additive manufactured case with internal passages for active clearance control

Components having separable outer wall plugs for modulated film cooling

Gas turbine engine forward bearing compartment architecture

IMPINGEMENT INSERT FOR A GAS TURBINE ENGINE

Propulsion assembly comprising a duct for feeding the gas generator in an inter-duct casing

Turbine cooling system

Airfoil with sealed baffle

Gas turbine engine component with degradation cooling scheme

Gas turbine engine

Airfoil with dual profile leading end

Airfoil with ceramic airfoil piece having internal cooling circuit

Method for making ceramic turbine engine article

Dual-wall airfoil with leading edge cooling slot

Methods and apparatuses using cast in core reference features

Airfoil leading edge impingement cooling

Double impingement slot cap assembly

Airfoil endwall with partial integral airfoil wall

Turbine engine unit for lubricating a bearing holder

Seal assembly

Additively manufactured component for a gas powered turbine

Turbine airfoil trailing edge coolant passage created by cover

Partially wrapped trailing edge cooling circuits with pressure side impingements

Partially wrapped trailing edge cooling circuit with pressure side serpentine cavities

Turbine airfoil coolant passage created in cover

Turbine vane cooling arrangement

Mid turbine frame including a sealed torque box

Integrated inner case heat shield

Casing with suction arm for axial turbine engine

Seal arrangement for a mid turbine frame of a gas turbine

Dual-walled components for a gas turbine engine

Gas turbine component with cooling aperture having shaped inlet and method of forming the same

Supplemental cooling air for turbine exhaust components and surfaces

Flow directing cover for engine component

Dual walled component for a gas turbine engine

Air-film cooled component for a gas turbine engine

Embedded electric machine

ENGINE COMPONENT WITH POROUS HOLES

Engine component with porous trench

Modulated turbine component cooling

Impingement system for an airfoil

Systems for removing heat from turbine components

Impingement system for an airfoil

Inter-stage cooling for a turbomachine

Turbofan engine comprising a fairing being located in the secondary flow channel and having a separate end element

Air metering baffle assembly

Turbine engine air guide assembly with improved aerodynamic performance

Cooling hole with enhanced flow attachment

GAS TURBINE ENGINE WITH HEAT PIPE FOR THERMAL ENERGY DISSIPATION

Gas turbine engine turbine vane baffle and serpentine cooling passage

Intermediate case for an aircraft turbomachine made from a single casting with a lubricant duct

Turbine vane with coupon having corrugated surface(s)

Blade with corrugated outer surface(s)

Turbine rotor blade with coupon having corrugated surface(s)

Heat pipe temperature management system for wheels and buckets in a turbomachine

Assembly for supporting an annulus

Turbomachine component having impingement heat transfer feature, related turbomachine and storage medium

Manufacturing methods for multi-lobed cooling holes

Cooling hole with shaped meter

Stator vane arrangement and a method of casting a stator vane arrangement

Service routing configuration for a gas turbine engine diffuser system

Ceramic matrix composite component cooling

Impingement cooling system for a gas turbine engine

Impingement insert for a gas turbine engine

Split-zone flow metering T-tube

Multiple nozzle configurations for a turbine of an environmental control system

Method and system for bowed rotor start mitigation using rotor cooling

Internal cooling of stator vanes

Engine component assembly

Engine components with cooling holes having tailored metering and diffuser portions

Vane for turbomachinery, such as an aircraft turbojet or turbofan engine or an aircraft turboprop engine

Sector for the assembly of a stage of a turbine and corresponding manufacturing method

Intermediate central passage spanning outer walls aft of airfoil leading edge passage

Service tube for a turbine engine

System and method for cooling components of a gas turbine engine

Gas turbine engine turbine vane baffle and serpentine cooling passage

Gas turbine engine transition duct and turbine center frame

Air bypass system for rotor shaft cooling

Gas turbine engine service tube mount

IMPINGEMENT PLATE WITH STRESS RELIEF FEATURE

Output director vane for an aircraft turbine engine, with an improved lubricant cooling function using a heat conduction matrix housed in an inner duct of the vane

Blade outer air seal with flow guide manifold

Internal cooling system with insert forming nearwall cooling channels in midchord cooling cavities of a gas turbine airfoil

Gas turbine exhaust diffuser with air injection

Apparatus, turbine nozzle and turbine shroud

Sump housing for a gas turbine engine

Connection system for housing elements of a turbine intermediate casing

Turbine frame cooling systems and methods of assembly for use in a gas turbine engine

Air shredder insert

Thermal stress relief of a component

Impingement holes for a turbine engine component

Gas turbine engine trailing edge ejection holes

Gas turbine

Modulated turbine vane cooling

CENTRIFUGAL COMPRESSOR

Exhaust frame

Core component having toroidal structures

Outlet guide vane for aircraft turbine engine, presenting an improved lubricant cooling function

Cooled CMC wall contouring

Flow exchange baffle insert for a gas turbine engine component

Gas turbine engine case flow blocking covers

Turbine airfoil trailing edge cooling passage

Turbine vane, turbine, and turbine vane modification method

Turbine blade with optimised cooling at the trailing edge of same comprising upstream and downstream ducts and inner side cavities

Assembly for turbine machine with open rotor contra-rotating propellers, comprising a small duct for the passage of ancillaries

Method and system for combination heat exchanger

Staged fuel and air injection in combustion systems of gas turbines

Impingement cooling baffle

Crossover hole configuration for a flowpath component in a gas turbine engine

Turbine rotor coolant supply system

Article and method of forming an article

Article and method of cooling an article

CLOSED LOOP COOLING METHOD FOR A GAS TURBINE ENGINE

OGV heat exchangers networked in parallel and serial flow

Casing for use in a turbofan engine and method of scavenging fluid therefrom

Instrumented flow passage of a turbine engine

Multiple diffusing cooling hole

Thermal management of CMC articles having film holes

Gas turbine engine with rotor centering cooling system in an exhaust diffuser

Cooling of turbine blades and method for turbine blade manufacture

Turbine assembly with detachable struts

Turbine airfoil cooling system with spanwise extending fins

Vane unit and steam turbine

Gas turbine engine having a flow control surface with a cooling conduit

Ceramic matrix composite component and process of producing a ceramic matrix composite component

Cooling hole patterned surfaces

Turbine engine and particle separators therefore

Multi-piece shroud hanger assembly

Multiple spoke cooling system and method

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

Cooling passages in a turbine component

Mid-turbine frame spoke cooling system and method

Module for a gas turbine

Turbine cavity sealing assembly

Nozzle for a gas turbine engine

BLADE FOR FLUID FLOW MACHINE, TURBO FAN ENGINE AND METHOD FOR MANUFACTURING A BLADE

Spiral cooling of combustor turbine casing aft plenum

Cooling hole with curved metering section

Staggered crossovers for airfoils

METHOD OF CREATING HEAT TRANSFER FEATURES IN HIGH TEMPERATURE ALLOYS

Mixed flow turbocore

Non-contact seal assembly for rotational equipment

Impingement structure for jet engine mid-turbine frame

Turbine assembly and corresponding method of operation

Turbine component surface cooling system with passive flow modulation

Overlapping herringbone filmhole patterned surfaces

Bladed gas turbine rotor

Cooling structure for hot-gas path components with methods of fabrication

Gas turbine engine frame assembly

Nozzle guide vane and method for forming such nozzle guide vane

Ply, method for manufacturing ply, and method for manufacturing article with ply

Cooling device with small structured rib-dimple hybrid structures

Turbo machine

Cooling system for a turbine engine

Turbine stator vane assembly for a turbomachine

Integrated strut-vane nozzle (ISV) with uneven vane axial chords

Cooling structure for stationary blade

Thermally compliant heatshield

Guide vane of a gas turbine engine, in particular of an aircraft engine

Axial transfer tube

Gas turbine blade

Internal manifold for turning mid-turbine frame flow distribution

Guide arm for elements having an elongated shape, in particular for a turbomachine

Monolithic ceramic rods to enable cooling holes in CMC

Pre-skewed capture plate

Gas turbine engine cooling fluid composite tube

Gas turbine engine component with diffusive cooling hole

Turbomachine comprising a ventilation system

Tie rod connection for mid-turbine frame

Angled impingement inserts with cooling features

Heat shield, systems and methods

Flow splitting baffle

Overlapping herringbone filmhole patterned airfoil

Gas turbine, gas turbine control device, and gas turbine cooling method

Mid turbine frame including a sealed torque box

Flow directing cover for engine component

Multiple injector holes for gas turbine engine vane

Nozzle insert rib cap

Asymmetric diffuser opening for film cooling holes

Compressor rim thermal management

Cutouts in gas turbine structures for deflection control

Method for providing coolant to a movable airfoil

Shim to maintain gap during engine assembly

Heat pipe temperature management system for a turbomachine

Tri-tab lock washer

Airfoil contour for low-loss on-boarding of cooling air through an articulating spindle

System for cooling a turbine engine

Fan drive gear system manifold radial tube filters

Cooling passages for a mid-turbine frame

Cooling passages for a mid-turbine frame

Turbine engine component with diffuser holes

Engine component with film hole

Cooling passages for a mid-turbine frame

Secondary air system with venturi

Integrated inner case heat shield

Vane assembly for a gas turbine engine

Baffle inserts

Vane for jet engine mid-turbine frame

Gas powered turbine component including serpentine cooling

Systems and methods for axial compressor with secondary flow

Gas turbine engine airfoil

Engine component

Engine component

Gas turbine engine mid-turbine frame configuration

Thermally compliant fitting for high temperature tube applications

Clinch nut bolt hole geometry

Mid-turbine frame assembly for a gas turbine engine

Cooling passages for a mid-turbine frame

Airfoil with skin core cooling