TIE ROD-LOCKING NUT ASSEMBLY AND GAS TURBINE INCLUDING SAME

MULTI-CORE ACOUSTIC PANEL FOR AN AIRCRAFT PROPULSION SYSTEM

DEGASSING TUBE AND EJECTION CONE FOR A TURBINE ENGINE, AS WELL AS TOOL FOR ASSEMBLY THEREOF

Rotor balance weight system

CMC honeycomb base for abradable coating on CMC BOAS

ANGLED IMPINGEMENT INSERTS WITH COOLING FEATURES

Rotor balance weight system

SEAL

TURBINE COMPONENTS WITH NEGATIVE CTE FEATURES

Blade ring segment for turbine section, turbine section having the same, and gas turbine having the turbine section

VARIABLE TURBINE AND/OR COMPRESSOR GEOMETRY FOR AN EXHAUST GAS TURBOCHARGER

BLADE OF A TURBOMACHINE, INCLUDING A COOLING CHANNEL AND A DISPLACEMENT BODY SITUATED THEREIN, AS WELL AS A METHOD FOR MANUFACTURING

ABRADABLE STRUCTURE FOR A TURBOMACHINE, TURBOMACHINE HAVING AN ABRADABLE STRUCTURE, AND METHOD FOR MANUFACTURING AN ABRADABLE STRUCTURE

Pin to reduce relative rotational movement of disk and spacer of turbine engine

Degassing tube and ejection cone for a turbine engine, as well as tool for assembly thereof

Three dimensional auxetic structure, manufacturing method and tooling

Polyhedral-sealed article and method for forming polyhedral-sealed article

COMPONENT HAVING IMPINGEMENT COOLED POCKETS FORMED BY RAISED RIBS AND A COVER SHEET DIFFUSION BONDED TO THE RAISED RIBS

Gas turbine engine component with degradation cooling scheme

TURBINE COMPONENT THERMAL BARRIER COATING WITH VERTICALLY ALIGNED, ENGINEERED SURFACE AND MULTIFURCATED GROOVE FEATURES

Dual walled component for a gas turbine engine

TURBINE COMPONENT THERMAL BARRIER COATING WITH CRACK ISOLATING, CASCADING, MULTIFURCATED ENGINEERED GROOVE FEATURES

Turbomachine including clearance control system

Acoustic liner for gas turbine engine components

Heat-exchange and noise-reduction panel for a propulsion assembly

Sealing element for a turbo-machine, turbo-machine comprising a sealing element and method for manufacturing a sealing element

Belly band seal with anti-rotation structure

Angled impingement inserts with cooling features

Composite fan inlet blade containment

TURBINE COMPONENTS WITH NEGATIVE CTE FEATURES

Structural honeycomb panel

Variable turbine and/or compressor geometry for an exhaust gas turbocharger

Brush seal

Borescope assembly and method of installing borescope plugs

System for damping vibrations in a turbine

Structural element of an air vehicle air intake composed of an array of passages with a hexagonal cross section

Component lock for a gas turbine engine

COATING WITH ABRADABILITY PROPORTIONAL TO INTERACTION RATE

Turbine airfoil and method for cooling a turbine airfoil

Boundary layer energiser

Boundary layer energiser

SYSTEME D'ANTI GIVRAGE ET DE DEGIVRAGE DE NACELLE DE MOTEUR D'AERONEF A TAPIS RESISTIF

Ice protection system for a multi-segment aircraft component

Thermally conductive structure

System for regulating a cooling fluid within a turbomachine

TURBINE INLET AIR TREATMENT APPARATUS

Fan duct blade containment assembly

Flow laminarizing device

Seal in a gas turbine engine having a shim base and a honeycomb structure with a number of cavities formed therein