TURBINE ENGINE WITH A NOZZLE HAVING COOLING FEATURES

ENGINE COMPONENT

FAN ASSEMBLY

PROPULSOR WING TRAILING EDGE EXHAUST AREA CONTROL

Turbine rotor for a turbomachine

Turbocharger with vaned diffuser for the compressor

Articulating slider for nacelle

Variable area nozzle and method for operating same

Articulating slider for nacelle

MULTI-CORE ACOUSTIC PANEL FOR AN AIRCRAFT PROPULSION SYSTEM

BLADED DISC

Tube gallery for gas turbine engine

Variable gap between impeller rotor and static structure

Pin member for turbine

Propulsor wing trailing edge exhaust area control

Film cooling diffuser hole

Lubricant nozzle for a planetary gear set speed reducer of a turbomachine

Assembly comprising a lubricating wheel and lubricant nozzles for a planetary gear speed reducer of a turbomachine

CMC BOAS intersegment seal

ANGLED IMPINGEMENT INSERTS WITH COOLING FEATURES

Reduced stress boss geometry for a gas turbine engine

TURBINE ELEMENT FOR HIGH PRESSURE DROP AND HEAT TRANSFER

BOAS thermal protection

Cooling hole for a gas turbine engine component

Fluid collection gutter for a geared turbine engine

CERAMIC COMPONENT FOR COMBUSTION TURBINE ENGINES

Support rail truss for gas turbine engines

Frangible airfoil for a gas turbine engine

Strip seal axial assembly groove

Blade for a turbomachine

Turbine rotor blade assembly

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

Endwall cooling system

Ceramic matrix composite joints

Fan and air-conditioning apparatus equipped with fan

Spline for a turbine engine

SPLINE FOR A TURBINE ENGINE

Spline for a turbine engine

SPLINE FOR A TURBINE ENGINE

Oblong purge holes

Systems including rotor blade tips and circumferentially grooved shrouds

Turbine engine duct

COMBUSTOR LINER PANEL END RAIL MATCHING HEAT TRANSFER FEATURES

Asymmetric multi degree of freedom flutter damper

Engine component with flow enhancer

Turbine assembly

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

Dual walled component for a gas turbine engine

Gas turbine blade

Forming cooling passages in thermal barrier coated, combustion turbine superalloy components

Turbine shroud with abradable layer having dimpled forward zone

Method for repairing a fan casing

ANTI-BIRD STRIKE PROTECTION NET FOR AIRCRAFT JET ENGINE

Seal carrier for a turbomachine, in particular a gas turbine

Gas turbine with an air bleeder tube

Seal-plate anti-rotation in a stage of a gas turbine engine

COATED AND UNCOATED SURFACE-MODIFIED AIRFOILS FOR A GAS TURBINE ENGINE COMPONENT AND METHODS FOR CONTROLLING THE DIRECTION OF INCIDENT ENERGY REFLECTION FROM AN AIRFOIL

Gas turbine disk

AXIAL TURBO MACHINE

EXHAUST MIXER WITH OUTER LOBE CONSTRAINT BAND

Morphing vane

Gas turbine blade

Diffuser part for a gas turbine

Air-shielded fuel injection assembly to facilitate reduced NOemissions in a combustor system

Reduced stress boss geometry for a gas turbine engine

Angled impingement inserts with cooling features

Composite fan inlet blade containment

Gas turbine blade with corrugated tip wall

BOAS thermal protection

Blade tip cooling arrangement

SHIM SEAL ASSEMBLIES AND ASSEMBLY METHODS FOR STATIONARY COMPONENTS OF ROTARY MACHINES

Turbine bucket for control of wheelspace purge air

Large displacement high temperature seal

Shroud assembly for a turbine engine

Flowpath boundary and rotor assemblies in gas turbines

Blade or vane for a turbomachine and axial turbomachine

Cooling hole for a gas turbine engine component

Rotor and gas turbine engine including same

Rocket motors and their use

Borescope assembly and method of installing borescope plugs

Damping device for being situated between a housing wall and a casing ring of a housing of a thermal gas turbine

Panel attachment system and a method of using the same

System and method for reducing back pressure in a gas turbine system

Reheat burner arrangement having an increasing flow path cross-section

Cooling for a turbine airfoil trailing edge

SHIM SEAL ASSEMBLIES AND ASSEMBLY METHODS FOR STATIONARY COMPONENTS OF ROTARY MACHINES

Cable-actuated variable area fan nozzle with elastomeric seals

Mechanism for variable adjustment of blades for a system of contra-rotating propellers, and a system of contra-rotating propellers comprising at least one such mechanism

COMPLIANT PLATE SEAL ASSEMBLY FOR A TURBO MACHINE

Rocket propulsion device and method for assembling rocket propulsion device

METHOD OF FABRICATING A COMPONENT USING A TWO-LAYER STRUCTURAL COATING

Compressor blade of a gas-turbine engine with a self-sharpening leading-edge structure

Oiling nozzle for thrust bearing

Modular serpentine cooling systems for turbine engine components

COMPLIANT PLATE SEAL WITH SELF-CORRECTING BEHAVIOR

Counter-vortex film cooling hole design

Counter-vortex paired film cooling hole design

Propulsion unit for aircraft with heat exchanger having front inlet faces for cooling air flow and hot air flow

Turbine component

Compliant plate seals for turbomachinery

Aerofoil assembly

Compliant plate seal with an annular ring for turbomachinery and methods of assembling the same

Double padded finger seal

Ceramic matrix composite turbine engine components with unitary stiffening frame

Compliant plate seals for turbomachinery

Compliant plate seals for turbomachinery

Gas turbine blade shroud

Outlet nozzle for a jet engine, an aircraft comprising the outlet nozzle and a method for controlling a gas flow from the jet engine

Yaw control device for a nozzle having a rectangular outlet section

Reduced gain thrust control valve

Duct liner acoustic splice

Exhaust nozzle for an engine of a flying craft

High efficiency fan cooling holes for turbine airfoil

Bladeless conical radial turbine and method

Engine component

2D variable-area plug nozzle