TURBINE ENGINE WITH A BLADE ASSEMBLY HAVING COOLING CONDUITS

GEARED GAS TURBINE ENGINE

Internal core profile for a turbine nozzle airfoil

Outlet guide vane assembly in gas turbine engine

Geometrically segmented abradable ceramic thermal barrier coating with improved spallation resistance

Turbine blade airfoil profile

Intercooled cooling air with auxiliary compressor control

Turbine nozzle airfoil profile

Measuring device and method for an aircraft engine and an aircraft engine

Gas turbine blade

Independently controllable wheel for a turbine section of a gas turbine engine

BOAS retention assembly with interlocking ring structures

Passive blade tip clearance control system for gas turbine engine

GEARED GAS TURBINE ENGINE

System and method for selectively modulating the flow of bleed air used for high pressure turbine stage cooling in a power turbine engine

Airfoil shape for turbine rotor blades

FAILURE DETECTION SYSTEM OF A COOLING AIR SUPPLY SYSTEM AND A FAILURE DETECTION METHOD FOR A COOLING AIR SUPPLY SYSTEM OF A HIGH-PRESSURE TURBINE

Geometrically segmented abradable ceramic thermal barrier coating with improved spallation resistance

Heat pipe in turbine engine

Blade structure for turbomachine

First-stage stationary vane of gas turbine and gas turbine

Gas turbine engine with dove-tailed TOBI vane

First stage turbine nozzle

Turbocooled vane of a gas turbine engine

Intercooled cooling air with auxiliary compressor control

Necked debris separator for a gas turbine engine

ROTOR OF A FLUID FLOW MACHINE

Turbine shroud block segment with near surface cooling channels

Airfoil cooling system

Trip strip configuration for gaspath component in a gas turbine engine

CMC nozzle with interlocking mechanical joint and fabrication

Gas turbine engine flow modulation in a rotating vane

Turbine vane for gas turbine engine

Fan spacer for a gas turbine engine

Intercooled cooling air tapped from plural locations

First-stage turbine vane supporting structure and gas turbine including same

METHOD FOR DETERMINING A LOCAL HOT GAS TEMPERATURE IN A HOT GAS DUCT, AND DEVICES FOR CARRYING OUT THE METHOD

Turbine engine and components for use therein

Compressor turbine vane airfoil profile

Power turbine vane airfoil profile

Vane assembly of a gas turbine engine

Blade and gas turbine provided with same

Gas turbine engine with diversion pathway and semi-dimensional mass flow control

Turbine support structure

Method of assembling and disassembling gas turbine and gas turbine assembled thereby

Cool core gas turbine engine

Gas turbine with axially moveable outer sealing ring with respect to housing against a direction of flow in an assembled state

Airfoil shape for a turbine rotor blade

Airfoil shape for a turbine rotor blade

Particle removal device for gas turbine and gas turbine including the same

Resupply hole of cooling air into gas turbine blade serpentine passage

Intercooled cooling air with dual pass heat exchanger

Gas turbine combustor transition piece including inclined surface at downstream end portions for reducing pressure fluctuations

Thermal isolation structure for rotating turbine frame

Component assembly for a gas turbine engine

Intercooled cooling air with dual pass heat exchanger

Gas turbine and method of attaching a turbine nozzle guide vane segment of a gas turbine

Impingement system for an airfoil

Impingement system for an airfoil

Turboengine, and vane carrier unit for turboengine

ENGINE HOT SECTION COMPONENT AND METHOD FOR MAKING THE SAME

Cooling device for cooling platforms of a guide vane ring of a gas turbine

Intercooled cooling air with auxiliary compressor control

System for sealing between combustors and turbine of gas turbine engine

Turbocooled vane of a gas turbine engine

Intercooled cooling air tapped from plural locations

Intercooled cooling air with plural heat exchangers

Intercooled cooling air with dual pass heat exchanger

TURBINE AIRFOIL

Gas turbine engine having section with thermally isolated area

Turbo-compressor with geared turbofan

Turbine blade having film cooling hole arrangement

Mounting apparatus for low-ductility turbine nozzle

Vane assembly of a gas turbine engine

Blade or vane for a turbomachine and axial turbomachine

MODIFIED BUCKET PLATFORMS OF TURBINE BUCKETS AND METHODS FOR MODIFYING BUCKET PLATFORMS OF TURBINE BUCKETS

Turbine arrangement

Air separator for a turbine engine

Gas turbine engine with dove-tailed TOBI vane

Method for manufacturing composite fan annulus filler having nano-coating

Gas turbine engine airfoil leading edge cooling

Power turbine blade airfoil profile

Gas turbine

Gas turbine

System for sealing between combustors and turbine of gas turbine engine

Cooling system for gas turbine

Method for disassembly and assembly of a rotor of a gas turbine

Gas turbine

Gas turbine engine turbine blade airfoil profile

TURBINE BLADE

High-pressure turbine nozzle for a turbojet

Sealing arrangement and gas turbine engine with the sealing arrangement

Engine hot section component and method for making the same

Gas turbine engine systems and related methods involving vane-blade count ratios greater than unity

Method for controlling a gas turbine and gas turbine for implementing the method

Seal assembly for use with turbine nozzles

Gas turbine

GAS TURBINE

Cooling arrangement

Crenelated turbine nozzle

Gas Turbine Seal

Compressor turbine blade airfoil profile

Airfoil core shape for a turbine nozzle

COOLED GAS TURBINE GUIDE BLADE FOR A GAS TURBINE, USE OF A GAS TURBINE GUIDE BLADE AND METHOD FOR OPERATING A GAS TURBINE

External profile for turbine blade airfoil

Turbine blade

Cooled airfoil component

Compound nozzle cooled engine

Cantilevered framework support for turbine vane

HP turbine vane airfoil profile

HP turbine blade airfoil profile

Airfoil for a first stage nozzle guide vane

Method and apparatus for assembling turbine nozzle assembly

Device for ventilating turbine disks in a gas turbine engine

Variable motive nozzle ejector for use with turbine engines

Cooled gas turbine guide blade for a gas turbine, use of a gas turbine guide blade and method for operating a gas turbine

Counterflow film cooled wall

Rotor blade for a first phase of a gas turbine

Airfoil profile with optimized aerodynamic shape

High efficiency rotor for the first phase of a gas turbine

High efficiency stator for the first phase of a gas turbine

Ni-base superalloy having a thermal barrier coating system

Turbine blade inner rib profile

Turbine blade inner rib profile

Surface profiles for tip rails of turbine blade tip shroud

Turbine blade cooling hole arrangement

Turbine blade airfoil profile

Gas turbine engine airfoil frequency design