AIRCRAFT WITH AN UNDUCTED FAN PROPULSOR

FORWARD LOAD REDUCTION STRUCTURES FOR AFT-MOST STAGES OF HIGH PRESSURE COMPRESSORS

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Forward load reduction structures for aft-most stages of high pressure compressors

Stator vane assembly for an aircraft turbine engine compressor

STATOR VANE FOR A GAS TURBINE ENGINE

Air turbine starter with shaped vanes

Flowpath assembly for gas turbine engine

Air turbine starter with shaped vanes

Variable-pitch stator vane for an aircraft turbine engine

Wheel of a fluid flow machine

Platform seal

Gas turbine engine airfoils having multimodal thickness distributions

Cooled airfoil, guide vane, and method for manufacturing the airfoil and guide vane

Turbomachine fan flow-straightener vane, turbomachine assembly comprising such a vane and turbomachine equipped with said vane or said assembly

Airfoils having tapered tip flag cavity and cores for forming the same

Guide vane cascade for a turbomachine

Inter-component seals for ceramic matrix composite turbine vane assemblies

UNIFIED BOAS SUPPORT AND VANE PLATFORM

Turbine distributor sector for an aircraft turbine engine

Stator vane for a turbine of a turbomachine

Modified J type cantilevered vane and gas turbine having the same

Stator vane assembly for a gas turbine engine

Turbine engine component with an insert

Turbine vane comprising a blade with a tub including a curved pressure side in a blade apex region

GAS TURBINE ENGINE COMPONENT HAVING TIP VORTEX CREATION FEATURE

Airfoil turn caps in gas turbine engines

Method of repairing turbine component using ultra-thin plate

Method of repairing turbine component

Method of manufacturing turbine airfoil and tip component thereof

Airfoil turn caps in gas turbine engines

Two-piece multi-surface wear liner

Variable nozzle unit and variable displacement-type turbocharger

Radially diffused tip flag

Gas turbine engine airfoils having multimodal thickness distributions

Method for Scaling Turbomachine Airfoils

Flow directing cover for engine component

Gas turbine exhaust assembly

Cooling circuit for a multi-wall blade

Airfoil for a turbine engine

Flow discourager and method of making same

Gas turbine engine airfoil

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

Propeller fan and blower unit

CONTOURED SURFACE ANNULAR SECTION OF A GAS TURBINE

Turbomachine blade and relative production method

Mounting of vanes at the periphery of a turbine engine disc

Turbine engine assembly for measuring the vibrations to which a rotating blade is subjected

Gas turbine engine with a vane having a cooling air turning nozzle

Turbine stator vane of ceramic matrix composite

Compressor system and airfoil assembly

Flow directing cover for engine component

TURBINE INTRUSION LOSS REDUCTION SYSTEM

ABRASIVE BLADE TIP WITH IMPROVED WEAR AT HIGH INTERACTION RATE

Blade tip cooling arrangement

COOLED AIRFOIL, GUIDE VANE, AND METHOD FOR MANUFACTURING THE AIRFOIL AND GUIDE VANE

Gas turbine axial compressor

Gas turbine engine component with abrasive surface formed by electrical discharge machining

Turbomachine including a vane and method of assembling such turbomachine

ENGINE CASING ELEMENT

Gas turbine engine component with rib support

MOUNTING ARRANGEMENT FOR AEROFOIL BODY

Device for deicing a separator nose of an aviation turbine engine

Maxmet Composites for Turbine Engine Component Tips

Anti-rotation nozzle sector and method for manufacturing such a sector

Gas turbine engine component having tip vortex creation feature

Group of blade rows

Complaint cantilevered airfoil

High order shaped curve region for an airfoil

Turbocharger with variable turbine geometry having grooved guide vanes

Turbine intrusion loss reduction system

Steam turbine stationary blade and steam turbine

Crack-resistant environmental barrier coatings

Airfoil components containing ceramic-based materials and processes therefor

Trailing edge or tip flag antiflow separation

High order shaped curve region for an airfoil

Honeycomb seal and method

Turbine of a turbomachine

GAS TURBINE ENGINE AIRFOIL TIP RECESSES

Airfoil seal

Turbine airfoil components containing ceramic-based materials and processes therefor

SYSTEM AND METHOD TO ELIMINATE A HARD RUB AND OPTIMIZE A PURGE FLOW IN A GAS TURBINE

Vane assembly having a vane end seal

Stator vane with localized reworking of shape, stator section, compression stage, compressor and turbomachine comprising such a vane

Open rotor variable pitch blade with retracting inboard trailing edge

Sealing variable guide vanes