TURBINE ENGINE WITH A BLADE ASSEMBLY HAVING COOLING CONDUITS

INTERMEDIATE SHAFT COVER, AND GAS TURBINE PROVIDED WITH SAME

COMPONENT WITH COOLING PASSAGE FOR A TURBINE ENGINE

MANIFOLD FOR TURBINE BLADE OF GAS TURBINE ENGINE

Rotor assembly for a gas turbine

Heat-protection element for a bearing chamber of a gas turbine

Component with cooling passage for a turbine engine

Anti-vortex tube retaining ring and bore basket

Pressure gain for cooling flow in aircraft engines

Inertial particle separator for a turbine section of a gas turbine engine

Gas turbine engine rotor assembly and method of using same

Turbine blade trailing edge cooling feed

Anti-vortex tube retaining ring and bore basket

Speed-controlled conditioning valve for high pressure compressor

Rotor assembly

Pre-swirl nozzle carrier and method of manufacturing the same

Rotor including replaceable self-locking sealing assembly, turbine, and gas turbine including the same

Vented tangential on-board injector for a gas turbine engine

Monolithic body including an internal passage with a generally teardrop shaped cross-sectional geometry

Propulsion engine thermal management system

TANGENTIAL ON-BOARD INJECTOR (TOBI) ASSEMBLY

Serpentine turn cover for gas turbine stator vane assembly

Turbine blade having an improved structure

Mini-disk for gas turbine engine

COMPONENT FOR A TURBINE ENGINE WITH A COOLING HOLE

Intercooled cooling air fleet management system

Compressor rotor cooling apparatus

Rotor, in particular blisk of a gas turbine, having a broken-up rim and method for producing the same

Radial cooling system for gas turbine engine compressors

Compressor cooling in a gas turbine engine

Gas turbine disk

Structure for cooling turbine blades and turbine and gas turbine including the same

Gas turbine rotor, gas turbine, and gas turbine equipment

GAS TURBINE DISC

Non-contact seal assembly for rotational equipment

Gas turbine and component-temperature adjustment method therefor

Interdigitated turbine engine air bearing cooling structure and method of thermal management

Air bearing and thermal management nozzle arrangement for interdigitated turbine engine

JET ENGINE WITH A COOLING DEVICE

Compressor having reinforcing disk, and gas turbine having same

Rotor disc sealing device, and rotor assembly and gas turbine including the same

Retainer for gas turbine blade, turbine unit and gas turbine using the same

Gas turbine unit

ARRANGEMENT FOR A GAS TURBINE

Turbine engine turbine rotor with ventilation by counterbore

Vented tangential on-board injector for a gas turbine engine

Turbine have a first and second rotor disc and a first and second cooling fluid conduit wherein the second cooling fluid conduit is extended through an annular axially extended bore having a radially outer extent defined by a radially innermost surface of the rotor discs

Turbine rotor blade arrangement for a gas turbine and method for the provision of sealing air in a turbine rotor blade arrangement

Rotor disc with passages

Heat pipe in turbine engine rotor

GAS TURBINE

Rotor with a locking plate for securing an antirotation lock against unscrewing

Blade platform cooling in a gas turbine

Mini-disk for gas turbine engine

Nozzle cooling system for a gas turbine engine

Turbine assembly of an aircraft turbine engine

Cooling structure for turbine, and gas turbine

Rotor wheel and impeller inserts

Gas turbine with two swirl supply lines for cooling the rotor

Compressor aft rotor rim cooling for high OPR (T3) engine

Compressor and method for mounting of a compressor

Turbopump with axially curved vane

Turbine discs and methods of fabricating the same

Turbine disc assemblies and methods of fabricating the same

TURBINE ROTOR FOR A LOW PRESSURE TURBINE OF A GAS TURBINE SYSTEM

Gas turbine disk

Non-contact seal assembly for rotational equipment

Turbine disc assembly

Cooled turbine runner for an aircraft engine

Flow inducer for a gas turbine system

Rotor disk having a centripetal air collection device, compressor comprising said disc and turbomachine with such a compressor

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

Directed cooling for rotating machinery

Integral metering feature, systems and methods

Rotor for a thermal turbomachine

Rotary assembly for a turbomachine

Gas turbine engine with compressor disk deflectors

Turbine bucket for control of wheelspace purge air

Turbine bucket for control of wheelspace purge air

Rotor for a thermal turbomachine

Mixing plenum for spoked rotors

Rotor for a thermal turbomachine

High pressure compressor rotor thermal conditioning using discharge pressure air

Gas turbine rotors

Thermally isolated turbine section for a gas turbine engine

Vented tangential on-board injector for a gas turbine engine

Rotor shaft with cooling bore inlets

Turbine airfoil cooling system with cooling systems using high and low pressure cooling fluids

Method and system for cooling rotor blade angelwings

Rotor shaft for a turbomachine

Turbine wheel in a turbine engine

Impingement-cooled turbine rotor

Flow diverter to redirect secondary flow

Flow inducer for a gas turbine system

Cooling air configuration in a gas turbine engine

Systems and methods to control flow in a rotor wheel

Cooling device for a jet engine

Apparatus and method for purging a gas turbine rotor

Gas turbine engine with improved cooling between turbine rotor disk elements

GAS TURBINE SYSTEM

SYSTEM AND METHOD FOR REDUCING STRESS IN A ROTOR

TURBINE COOLING SYSTEM

Turbine component cooling with closed looped control of coolant flow

Turbine blade cooling system with bifurcated mid-chord cooling chamber

Turbine rotor disk inlet orifice for a turbine engine

HOLE FOR ROTATING COMPONENT COOLING SYSTEM

VENTILATED COMPRESSOR ROTOR FOR A TURBINE ENGINE AND A TURBINE ENGINE INCORPORATING SAME

Inserts for turbine cooling circuit

Rotating component of a turbine engine

Cross-over purge flow system for a turbomachine wheel member

Turbine engine rotating cavity anti-vortex cascade

Turbine blade

Apparatus and methods for cooling platform regions of turbine rotor blades

Cooling circuit for a drum rotor

Gas turbine

Turbine disc cooling arrangement

Apparatus and methods for cooling platform regions of turbine rotor blades

Apparatus and methods for cooling platform regions of turbine rotor blades

Apparatus and methods for cooling platform regions of turbine rotor blades

AXIAL TURBOMACHINE ROTOR HAVING BLADE COOLING

Rotor assembly disk spacer for a gas turbine engine

Air-cooled turbocharger with optional internal pressure relief valve

Ventilation of a high-pressure turbine in a turbomachine

Gas turbine with securing plate between blade base and disk

Turbine rotor wheel

Rotor Disc

Turbine assemblies with impingement cooling

GAS TURBINE, DISK, AND METHOD FOR FORMING RADIAL PASSAGE OF DISK

Anti-vortex device for a gas turbine engine compressor

Turbine disk and gas turbine

Turbine engine rotating cavity anti-vortex cascade

Turbine engine rotating cavity anti-vortex cascade

Seal coating between rotor blade and rotor disk slot in gas turbine engine

Insert for through-holes and method therefor

Steam turbine

Turbine engine rotor disc with cooling passage

Labyrinth seal for turbine dovetail

Gas turbine and cooling air supply structure thereof

Gas turbine

Cooling circuit for use in turbine bucket cooling

Air cooled turbine blades and methods of manufacturing

Turbine blade with micro-turbine nozzle provided in the blade root

Rotor for an engine

Mounting arrangement for turbine blades

Turbine blade cooling system

Rotor for a steam turbine

Bearing scavenge pump incorporated into turbine disk cover plate

Component with cooling passage for a turbine engine

Turbocharger shafts with integrated cooling fans and turbochargers comprising the same

Cast integrally bladed rotor with bore entry cooling

Turbine airfoil with pressure side trailing edge cooling slots