INTEGRAL LUBRICATION TUBE AND NOZZLE COMBINATION

Gas turbine engine rotor tip clearance and shaft dynamics system and method

Bleeding of air via the diffuser of a centrifugal compressor of a turbine engine

Gas turbine engine vanes

Accessing a valve assembly of a turbomachine

Gas turbine engine airfoil integrated heat exchanger

Turbine engine spacer

Bypass duct of a turbofan engine

Rear hub cooling for high pressure compressor

DOUBLE FLOW LOW-PRESSURE STEAM TURBINE

Airfoil cooling hole flag region

AERODYNAMICALLY SHAPED SUPPORTING AND/OR FAIRING ELEMENT IN THE BYPASS DUCT OF A GAS-TURBINE ENGINE

Steam turbine

Axial-centrifugal compressor having system for controlling play

Turbine vane and gas turbine

Oil tube with integrated heat shield

Cooling air system for mid turbine frame

Cooling system for a gas turbine and corresponding operation method

Air cooled turbine component having an internal filtration system

Dirt particle separator device for use in a gas turbine engine

Turbine vane for a gas turbine engine having serpentine cooling channels

Gas turbine

STARTER/GENERATOR INTEGRATED INTO COMPRESSOR OF TURBINE ENGINE

Inlet connecting piece for an axial-flow compressor

MOISTURE REMOVAL PROVISIONS FOR STEAM TURBINE

Structure of exhaust section of gas turbine and gas turbine

COOLED GAS TURBINE STATOR ASSEMBLY

TURBOJET ENGINE FOR AIRCRAFT

Thermal system for a working member of a power plant

Temperature responsive fluid flow control device

OIL LINE INSULATION SYSTEM FOR MID TURBINE FRAME

Vapor cooled static turbine hardware

Turbojet engine for aircraft, propulsion unit comprising such a turbojet engine and aircraft comprising such a propulsion unit

Heat transfer system and method for turbine engine using heat pipes

Bypass duct of a turbofan engine

Retention structures and exit guide vane assemblies

Vane

Airfoil insert having a tab extending away from the body defining a portion of outlet periphery

Fluid conduit coupling with leakage detection

Connector for heater

GAS TURBINE ENGINE WITH EJECTOR

VANE ASSEMBLY CONFIGURED FOR TURNING A FLOW IN A GAS TURBINE ENGINE, A STATOR COMPONENT COMPRISING THE VANE ASSEMBLY, A GAS TURBINE AND AN AIRCRAFT JET ENGINE

Bypass air scoop for gas turbine engine

Integrated service tube and impingement baffle for a gas turbine engine

Split fairing for a gas turbine engine

Mid turbine frame system for gas turbine engine

FABRICATED ITD-STRUT AND VANE RING FOR GAS TURBINE ENGINE

Mid turbine frame for gas turbine engine

Turbine frame assembly and method for a gas turbine engine

Method of assembly and disassembly of a gas turbine mid turbine frame

Mid turbine frame system and radial locator for radially centering a bearing for gas turbine engine

MID TURBINE FRAME SYSTEM FOR GAS TURBINE ENGINE

Mid turbine frame system for gas turbine engine

Shaped cooling holes for reduced stress

Gas turbine engine with integrated electric starter/generator

Apparatus and method for cooling a turbine airfoil arrangement in a gas turbine engine

Device for regulating the flow rate of air feeding a turbine ventilation cavity of a turbomachine turbine section

Bearing support structure for turbine

Arrangement for a gas turbine engine

Flow splitter for gas turbine engine

Gas turbine ejector and method of operation

Steam turbine having bearing struts

Turbojet for aircraft

Strut for a gas turbine engine

Gas turbine engine with insulated cooling circuit

Gas turbine and cooling air supply structure thereof

Combined acoustic absorber and heat exchanging outlet guide vanes

Turbomachine with integral generator/starter

GAS TURBINE

TURBINE ENGINE INLET STRUT DEICING

Cooling air manifold splash plates and gas turbines engine systems involving such splash plates

Two-shaft gas turbine

Vapor phase lubrication system

Apparatus for cooling rotary components within a steam turbine

Deoiling device and turbomachine comprising this device

Turbine blade

Mounting tubes for pressurizing an internal enclosure in a turbomachine

METHOD AND APPARATUS FOR DISTRIBUTING FLUID INTO A TURBOMACHINE

Intermediate casing of a turbojet and a turbojet

Vane and a vane assembly for a gas turbine engine

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

Method of aluminization in the vapor phase on hollow metal parts of a turbomachine

Media mixing insert for turbine blade in turbine engine

Gas turbine engine compressor case mounting arrangement

Gas turbine component with reduced cooling air requirement

Pipe assembly

Seal for gas turbine engine component

Multi-pass cooling for turbine airfoils

Blade shroud with fluid barrier jet generation

Systems and methods involving aerodynamic struts

Turbine blade and gas turbine equipped with a turbine blade

Exhaust casing for a turbomachine

Turbine component

Acoustic flow straightener for turbojet engine fan casing

Inter-turbine casing with cooling circuit, and turbofan comprising it

Turbofan provided with a pre-cooler

Strut cavity pilot and fuel injector assembly

Cooled airfoil component

Airfoil leading edge end wall vortex reducing plasma

Bypass turbomachine with artificial variation of its throat section

GAS TURBINE GUIDE VANES WITH TANDEM AIRFOILS AND FUEL INJECTION AND METHOD OF USE

Oil scavenge system for a gas turbine engine

Dual interstage cooled engine

Compound turbine cooled engine

Variable geometry guide vane for a gas turbine engine

Radial vaned diffusion system with integral service routings

Turbine airfoil with endwall horseshoe cooling slot

Connector for heater

Turbofan jet engine with an ancillary-connecting arm, and the ancillary-connecting arm

Assembly comprised of a vane and of a cooling liner, turbomachine nozzle guide vanes assembly comprising this assembly, turbomachine and method of fitting and of repairing this assembly

Casing cover in a jet engine

Turbomachine with integral generator/starter

Turbine exhaust strut airfoil profile

Method of securing a component in an engine

Methods and apparatus for controlling cooling air temperature in gas turbine engines

Cooling layout for a turbine blade, turbine blade included therein, turbine and aircraft engine equipped therewith

Methods and apparatus for cooling combustion turbine engine components

Device for supporting and housing auxiliaries in a bypass turbojet

Structural turbine engine casing

Access port for dirt removal for gas turbine engine

Dirt separator for gas turbine air supply

Grommeted bypass duct penetration

Counterrotating turbofan engine

Gas turbine compression system and compressor structure

Turbine exhaust case and method of making

Vane coupling

Link device between an enclosure for passing cooling air and a stator nozzle in a turbomachine

Method and apparatus for distributing fluid into a turbomachine

Method for air circulation in a turbomachine compressor, compressor arrangement using this method, compression stage and compressor incorporating such a arrangement, and aircraft engine equipped with such a compressor

Link device between an enclosure for passing cooling air and a stator nozzle in a turbomachine

Turbine engine guide vane and arrays thereof

Secondary flow, high pressure turbine module cooling air system for recuperated gas turbine engines

Recuperator and turbine support adapter for recuperated gas turbine engines

Gas turbine engine frame with an integral fluid reservoir and air/fluid heat exchanger

Turbine exhaust case and method of making

Modulated flow turbine nozzle

Airfoil insert with castellated end

Turbojet engine comprising a connector arm for ancillary systems, and the connector arm for ancillary systems

Turbofan jet engine with ancillaries distribution support

Apparatus and method for bearing lubrication in turbine engines

Methods and apparatus for assembling gas turbine engines

Sealing device for connection of a pipe in a hole

Method and apparatus for distributing fluid into a turbomachine

Provision of sealing in a jet engine for bleeding air to the cabin using a tube with a double ball joint

Ventilation system for a convergent divergent exhaust nozzle

Split flow turbine nozzle

Arrangement for bleeding the boundary layer from an aircraft engine

Device for injecting cooling air into a turbine rotor

Turbine engine having a combustion section

Thermal management system for gas turbine engine with open propulsor

Turbomachine component with film-cooling hole with hood extending from wall outer surface

Method of restoring alloy depletion in an airfoil around cooling holes

Inlet protector for vane coupling hole

Cooling nozzle vanes of a turbine engine

Engine with pressure gain combustor and compressor discharge turbine cooling

Service tube locking device

Airfoil with thick wishbone fiber structure

Gas turbine intake for aircraft engine and method of inspection thereof

Service tube locking device

Offtake scoops for bleed pressure recovery in gas turbine engines

Cooling method and structure of vane of gas turbine

Turbine stator vanes having inserts and splitter plates

Airfoil with dual-wall cooling and angled cooling channels

Gas turbine engine with hollow rotor in fluid communication with a balance piston cavity

Mid-turbine frame with intermediary plenum

Heat exchanger and flow modulation system

Turbine shroud having ceramic matrix composite component mounted with cooled pin

Diffused cooling arrangement for gas turbine engine components

Gas turbine engine with liquid metal cooling

Small turbine stator vane with impingement cooling insert

Industrial turbine stator vane