Airfoil having endwall panels

Airfoil having panels

Transition manifolds for cooling channel connections in cooled structures

Heat exchanger with integral bleed air ejector

Combustor liner panel with a multiple of heat transfer augmentors for a gas turbine engine combustor

COMBUSTOR WALL ELEMENT AND METHOD FOR MANUFACTURING THE SAME

Combustor aft frame cooling

Circular heatsink

Flange heat shield

Wall panel assembly for a gas turbine engine

Engine heat exchanger and method of forming

Combustion bypass passive valve system for a gas turbine

Multi-circuit buffer system for a gas turbine engine

Mechanically driven air vehicle thermal management device

Impingement system for an airfoil

Components having outer wall recesses for impingement cooling

Gas turbine engine with thermoelectric system

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

Combustor assembly for a turbine engine

System and method of cooling a turbine engine

Fuel injector with heat pipe cooling

Gas turbine engine and method to cool a gas turbine engine case assembly

Split-zone flow metering T-tube

Turbine engine and method of cooling

Method and system for bowed rotor start mitigation using rotor cooling

Core assemblies and gas turbine engine components formed therefrom

COMBINED CYCLE POWER PLANT WITH ABSORPTION REFRIGERATION SYSTEM

Airfoil with variable slot decoupling

Power electronics module

Gas-turbine combustion chamber with impingement-cooled bolts of the combustion chamber tiles

Cooled component having effusion cooling apertures

Light weight housing for internal component with integrated thermal management features and method of making

Panel for heat exchange and improved noise reduction for a turbomachine

Rotation enhanced turbine blade cooling

Method of making light weight component with internal metallic foam and polymer reinforcement

Light weight component and method of making

CLOSURE OF COOLING HOLES WITH A FILING AGENT

Method and system for modulated turbine cooling as a function of engine health

Bowed rotor prevention system using waste heat

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

Methods and systems for cooling airflow

Hybrid propulsion system for a gas turbine engine including a fuel cell

Cooled wall of a turbine component and a method for cooling this wall

Variable thickness core for gas turbine engine component

Methods of cooling a fluid using an annular heat exchanger

Heat exchanger for cooling medium temperature reduction

ENGINE COMPONENT ASSEMBLY

Method and system for a combined air-oil cooler and fuel-oil cooler heat exchanger

METHOD AND SYSTEM FOR COMPRESSOR AND TURBINE COOLING

SYSTEM AND METHOD OF SOAKBACK MITIGATION THROUGH PASSIVE COOLING

Core compartment ventilation devices for nacelles of gas turbine engines for cooling a core compartment of a gas turbine engine

Method and system for combination heat exchanger

Combustion chamber with fences for directing cooling flow

Active high pressure compressor clearance control

METHOD AND SYSTEM FOR STALL MARGIN MODULATION AS A FUNCTION OF ENGINE HEALTH

Staged fuel and air injection in combustion systems of gas turbines

Staged fuel and air injection in combustion systems of gas turbines

Cooling air heat exchanger scoop

Gas turbine engine airfoil cooling circuit arrangement

Heat exchange system for a power gear box, a power gear box and a turbo engine with a power gear box

System and method for cooling turbine shroud

Heat exchange system for power gear box, a power gear box and a turbo engine with a power gear box

Segmented micro-channel for improved flow

Coating methods

Method and apparatus for cooling gas turbine engine component

Cooling circuit for a multi-wall blade

Multi-source turbine cooling air

TURBULATORS FOR IMPROVED COOLING OF GAS TURBINE ENGINE COMPONENTS

Gas turbine engine turbine cooling system

Surface cooler and an associated method thereof

Gas turbine engine fluid cooling systems and methods of assembling the same

Turbine component including mixed cooling nub feature

Particle separators for turbomachines and method of operating the same

Aircraft with a propulsion unit comprising a fan at the rear of the fuselage

Heat exchange module for a turbine engine

Cooling an aperture body of a combustor wall

Shroud assembly for a gas turbine engine

ANGLED IMPINGEMENT INSERT WITH DISCRETE COOLING FEATURES

Turbine nozzle with inner band and outer band cooling

Exhaust plume cooling using periodic interruption of exhaust gas flow to form ambient air entraining vortices

Method and system for modulated turbine cooling

CMC ARTICLES HAVING SMALL COMPLEX FEATURES FOR ADVANCED FILM COOLING

CMC articles having small complex features for advanced film cooling

Turbine engine advanced cooling system

Phase change material cooling system for a vehicle

Mixing chambers for turbine wheel space cooling

Apparatus and method for air extraction at a gas turbine engine combustor

ENGINE LUBRICATION SYSTEM USING DE-OXYGENATED FUEL

Article and manifold for thermal adjustment of a turbine component

Internally cooled spoke

Turbine component surface cooling system with passive flow modulation

Gas turbine cooling systems and methods

First stage turbine vane arrangement

Seal segment for a gas turbine engine

Film cooling a combustor wall of a turbine engine

METHOD AND APPARATUS FOR GENERATING LATENT HEAT AT LOW TEMPERATURES USING EXOTHERMIC SALT CRYSTALLIZATION

Seals for gas turbine engine nacelle cowlings

Preloaded AFT vent area for low pressure fan ducts

Core assembly for gas turbine engine

Aircraft propulsion assembly with fire extinguishing system

Efficient power and thermal management system for high performance aircraft

Internal manifold for turning mid-turbine frame flow distribution

SYSTEMS AND METHODS FOR PASSIVELY PROVIDING ONE OR MORE FLOWS OF COOLING FLUID TO A HOT CAVITY WITHIN A COOLING CIRCUIT OF A GAS TURBINE ENGINE

Manufacture of component with cavity

Method of starting a gas turbine engine including a cooling phase

Brackets for gas turbine engine components

Turbofan bypass air cooled oil cooler fairings

Turbocooled vane of a gas turbine engine

Method for cooling a gas turbine and gas turbine for conducting said method

Thermal Barrier Coating with Lower Thermal Conductivity

METHOD FOR CONTROLLING THE TEMPERATURE OF A GAS TURBINE DURING A SHUTDOWN

System and method for improving exhaust energy recovery

GAS TURBINE ENGINE COMPONENT WITH SEPARATION RIB FOR COOLING PASSAGES

Systems for thermoelectric cooling for jet aircraft propulsion systems

Centrifugal airfoil cooling modulation

Hyperjet superconducting turbine blisk propulsion and power generation

Cooling a quench aperture body of a combustor wall

HEAT PIPE COOLING SYSTEM FOR A TURBOMACHINE

Transition duct assembly

Coated cooling passage

Cooling passages for a mid-turbine frame

Gas turbine engine wall assembly with offset rail

Bonded multi-piece gas turbine engine component

Diversion of fan air to provide cooling air for gas turbine engine

Self-cooled gas bottle

Orientation feature for swirler tube

Gas turbine, gas-turbine control device, and gas turbine operation method

Micro gas turbine systems and uses thereof

Mid-turbine frame assembly for a gas turbine engine

Cooling passages for a mid-turbine frame

High-flow-capacity centrifugal hydrogen gas compression systems, methods and components therefor

Mid-turbine frame assembly

Enhanced heat sink availability on gas turbine engines through the use of coolers

Overcooled air cooling system with annular mixing passage

Hydrocarbon film protected refractory carbide components and use

Gas turbine engine thermal management system

Cooling passages for a mid-turbine frame

Cooling passages for a mid-turbine frame

Gas turbine engine wall assembly with support shell contour regions

Controller cooling arrangement

Gas turbine engine thermal management system

Variable area turbine arrangement with secondary flow modulation

Gas turbine engine component providing prioritized cooling

Cooling having tailored flow resistance

Method and assembly for reducing secondary heat in a gas turbine engine

REVERSE CORE FLOW GAS TURBINE ENGINE

COOLING SYSTEM FOR AN ENERGY STORAGE SYSTEM AND METHOD OF OPERATING THE SAME

AIRCRAFT

Tail cone generator with integral speed increasing gearbox

Thermal management system for a gas turbine engine with an integral oil tank and heat exchanger in the nacelle

Compressor bleed air supply for an aircraft environmental control system

Tooling production method

Diffuser case strut for a turbine engine

Gas turbine system with cooling fluid generator

TURBINE COMPONENTS WITH STEPPED APERTURES

SYSTEM AND METHOD FOR PROVIDING A FILM TREATMENT TO A SURFACE USING COOLING DEVICES

Combined cycle power plant thermal energy conservation

Turbine bucket

Gas turbine rotors

SYSTEMS AND APPARATUS RELATING TO GAS TURBINE COMBUSTORS

Gas turbine engine cooling fluid metering system

Heat storage mechanism of heat exchanger

Environmental control generator system and apparatus

Gas turbine engine with axial compressor with internal cooling pathways

Gas turbine engine axial compressor rear hub

Method and an apparatus for producing cooling apertures in a combustion chamber head

GAS TURBINE ENGINE COMPONENT WITH TWISTED INTERNAL CHANNEL

Turbocharger

Through flow ventilation system for a power generation turbine package

Integrated thermal management with nacelle laminar flow control for geared architecture gas turbine engine

Gas turbine and operating method thereof

Gas turbine and operating method thereof

Gas turbine and operating method thereof

Acoustic treatment to mitigate fan noise

Thermally isolated turbine section for a gas turbine engine

Frame junction cooling holes

Cooling systems and methods using pressurized fuel

Heat shield for a casing

Two spool gas generator with improved air porting

Starter/generator combination with all variable frequency drives

Cooling architecture for turbine exhaust case

Scupper channelling in gas turbine modules

Gas generator with mount having air passages

Heat shield for cooling a strut

Rotor and gas turbine engine including a rotor

Turbine cooling system using an enhanced compressor air flow

Variable vane segment

MICRO GAS TURBINE SYSTEMS AND USES THEREOF

Gas turbine engine oil tank

GAS TURBINE INLET HAVING INTEGRATED COILS AND MIST REDUCING VANES

Gas turbine engine buffer system

Gas turbine engine component arrangement

Flow deflector arrangement

Dual filtration particle separator

Gas turbine engine

Directly communicated turbocharger

Cooling arrangement for a gas turbine

Modular power plant and an aircraft provided with a lift rotor

System for ventilating a gas turbine enclosure

Seal assembly with cooling feature

Repair methods for cooled components

Exhaust-gas turbocharger

HEAT SHIELD WITH A SUPPORTING STRUCTURE AND METHOD FOR COOLING THE SUPPORTING STRUCTURE

Aero boost—gas turbine energy supplementing systems and efficient inlet cooling and heating, and methods of making and using the same

Air supply device for aircraft engine turbines

Baffle with flow augmentation feature

Gas turbine engine configuration interface

Electric probe assembly, gas turbine engine having same and method of cooling same

Microcircuit cooling for gas turbine engine combustor

Gas turbine engine forward bearing compartment architecture

ANNULAR WALL FOR TURBOMACHINE COMBUSTION CHAMBER COMPRISING COOLING ORIFICES CONDUCIVE TO COUNTER-ROTATION

Gas turbine device using supercritical fluid as cooling fluid

Integrated electrical power and thermal management system

Exhaust plume cooling using periodic interruption of exhaust gas flow to form ambient air entraining vortices

Components with multi-layered cooling features and methods of manufacture

Surface cooler support mechanism

Cooling system with compressor bleed and ambient air for gas turbine engine

Gas turbine engine lubrication system

Steam turbine forced air cooling system, equipment, and steam turbine equipped with it

Gas turbine engine with a fire wall and an off-take device

METHOD OF COOLING A GAS TURBINE ENGINE

Method and system for providing cooling for turbine components

Method of recovering energy in a steam-cooled gas turbine

Axial flow machine cooling system

Heat transfer assembly and methods of assembling the same

Gas Turbine with Primary and Secondary Lubricating Oil Cooler

Cooling chamber for upstream weld of damping resonator on turbine component

Cooled wall

METHOD FOR DETERMINING AT LEAST ONE FIRING TEMPERATURE FOR CONTROLLING A GAS TURBINE AND GAS TURBINE FOR PERFORMING THE METHOD

Turbine engine nacelle fitted with a heat exchanger

Gas turbine engine thermal management system

Gas turbine engine heat exchanger system

Intercooled gas turbine with closed combined power cycle

Heat exchange arrangement

Multi-circuit buffer system for a gas turbine engine

Turbomachine inlet bleed heating assembly

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

Gas turbine engine lubrication system

Heat exchanger integrated with a gas turbine engine and adaptive flow control

Compressor air provided to combustion chamber plenum and turbine guide vane

Combustion chamber heat shield and seal assembly and a method of manufacturing a combustion chamber heat shield and seal assembly

Axial-flow turbine and power plant including the same

Film cooling structure and turbine blade

Heat shield manifold system for a midframe case of a gas turbine engine

Oil and fuel circuits in a turbine engine

Bore cavity thermal conditioning system

HEAT EXCHANGE MODULE FOR A TURBINE ENGINE

Engine cowl incorporating an equipment ventilation circuit

GAS TURBINE ENGINE COMPONENT COOLING ARRANGEMENT

Gas turbine engine heat exchangers and methods of assembling the same

Gas turbine engine buffer system

Internally coolable component for a gas turbine with at least one cooling duct

Aircraft propulsion system comprising an AFT pylon fairing with lateral walls that are profiled for injecting cool air along a thermal protection floor

Components with porous metal cooling and methods of manufacture

Closure of cooling holes with a filing agent

Heated rigid electrical harness for a gas turbine engine

System for controlling a cooling flow from a compressor section of a gas turbine

Cooled combustor seal

External cooling fluid injection system in a gas turbine engine

Turbine nozzle guide vane assembly in a turbomachine

Gas turbine thermal control and related method

Method for operating a gas turbine with sequential combustion and gas turbine for conducting said method

Part load performance improvement using deformable bore plugs

Combustor transition

BURNER FOR A GAS TURBINE

Air cooling design for tail-cone generator installation

System and method for operating a gas turbine engine

Discharge system of a separated twin-flow turbojet for an aircraft, corresponding turbojet and associated design method

Gas turbine engine buffer system

Nacelle scoop inlet

Method of operation of a downhole gas generator with multiple combustion chambers

Downhole gas generator with multiple combustion chambers

Method of cooling a downhole gas generator

Gas turbine apparatus

Assembly for a jet engine of an aircraft

Thermal barrier coating method, masking pin and combustor transition piece

Method and apparatus for gas turbine engine temperature management

Cooling device for a jet engine

Method and apparatus for generating motive power

Electrical raft with map

Gas turbine engine oil tank

Turbine component cooling system

Thermal management system for a gas turbine engine

METHOD AND SYSTEM FOR CONTROLLING A SECONDARY FLOW SYSTEM

Electrical structure having a grounding plane

Fluid flow machine especially gas turbine penetrated axially by a hot gas stream

Effusion cooled shroud segment with an abradable system

Turbine bypass system

Internal thermal management for motor driven machinery

TURBINE NOZZLE SEGMENT AND CORRESPONDING GAS TURBINE ENGINE

Gas turbine engine bearing support strut

Fuel air heat exchanger

Gas turbine engine thermal management system

Internally cooled spoke

Gas turbine engine buffer system

Multi-circuit buffer system for a gas turbine engine

Internal manifold for turning mid-turbine frame flow distribution

Gas turbine engine in-board cooled cooling air system

Gas turbine engine forward bearing compartment architecture

Electrical connectors