TURBINE ENGINE WITH COMPONENT HAVING A COOLING HOLE WITH A LAYBACK SURFACE

TURBINE ENGINE WITH A NOZZLE HAVING COOLING FEATURES

RAM AIR TURBINE

RAM AIR TURBINE

Pump cell for mobile surfing facility including radial pump and diffusor

Inlet cone for an aircraft turbomachine

Device for centering and guiding a shaft of an aircraft turbine engine

Turbine engine with component having a cooling hole with a layback surface

ASYMMETRIC HEAT TRANSFER MEMBER FILLET TO DIRECT COOLING FLOW

Turbine blade and gas turbine including the same

Trailing edge fuel injection enhancement for flame holding mitigation

Guide vanes for fully reversible turbomachinery

Method for modifying blades of fan, compressor, and turbine of axial flow type, and blades obtained by the modification

GAS TURBINE ENGINE STATIONARY VANE WITH CONTOURED PLATFORM

Turbine rotor blade

Cylinder head with integrated turbocharger

Variable stiffness damper system

VACUUM PUMP AND CONNECTION PORT USED IN VACUUM PUMP

Compressor impeller with partially swept leading edge surface

Inserts for airfoils of gas turbine engines

Gas turbine engine inlet wall design

HYBRID ELLIPTICAL-CIRCULAR TRAILING EDGE FOR A TURBINE AIRFOIL

Airfoil for a turbine engine incorporating pins

Thermal anti-icing system with non-circular piccolo tube

Pogo effect correction system

Quench aperture body for a turbine engine combustor

Non-uniform spray pattern oil delivery nozzle

Oval Steam Turbine Casing

Turbine distributor sector for an aircraft turbine engine

ANGLED IMPINGEMENT INSERTS WITH COOLING FEATURES

Thimble assemblies for introducing a cross-flow into a secondary combustion zone

Double wall turbine gas turbine engine blade cooling configuration

Support rail truss for gas turbine engines

Frangible airfoil for a gas turbine engine

Turbine vane, turbine, and gas turbine including the same

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

Gas turbine blade

Blade, blade ring, blade ring segment and turbomachine

Rotor for a turbomachine

Rotor with subset of blades having a cutout leading edge

GAS TURBINE DISC

Elliptical slot with shielding holes

Waste-gate valve and turbocharger

Bushing arranged between a body and a shaft, and connected to the shaft

Oblong purge holes

Vane assembly and gas turbine including the same

Turbine airfoil with biased trailing edge cooling arrangement

Flight vehicle engine with finned inlet

Asymmetric multi degree of freedom flutter damper

Device for ventilation of a turbomachine turbine casing

Composite piston ring seal for axially and circumferentially translating ducts

Diffuser for a turbine engine and method of forming same

Nested article by additive manufacturing with non-removable internal supporting structure

Guide vane for a diffuser of a radial compressor

Turbine assembly

Compressor rotor of a fluid flow machine

Rotor disc with passages

Rotor blade for a turbomachine and method for the assembly of a rotor blade for a turbomachine

Gas turbine blade

Ventilator wheel and ventilator

Acoustic liners for use in a turbine engine

TURBOMACHINE COMPONENT HAVING A PLATFORM CAVITY WITH A STRESS REDUCTION FEATURE

Air blowing device

Turbine vane gusset

Rotor with overhang at blades for a locking element

Idler gear connection for multi-stage variable vane actuation

Gas turbine engine components with optimized leading edge geometry

SYSTEM AND METHOD FOR UTILIZING TARGET FEATURES IN FORMING INLET PASSAGES IN MICRO-CHANNEL CIRCUIT

Gas turbine engine component with a baffle insert

Cooling passages for a gas path component of a gas turbine engine

Variable nozzle unit and variable geometry turbocharger

Diffuser part for a gas turbine

Composite piston ring seal for axially and circumferentially translating ducts

Impingement cooled spline seal

Angled impingement inserts with cooling features

Fan cooling hole array

Thermal shielding in a gas turbine

Thermal shielding in a gas turbine

Hula seal

Flow inlet

Quench aperture body for a turbine engine combustor

Gas turbine blade with corrugated tip wall

Blade tip cooling arrangement

Turbine bucket for control of wheelspace purge air

Large displacement high temperature seal

Shroud assembly for a turbine engine

Counter-swirl doublet combustor with plunged holes

Gas turbine engine component with converging/diverging cooling passage

Guide vane

Gas turbine engine

Gas turbine engine

Turbojet engine nacelle including a thrust reversing device with doors, including inner flanks on the sides of an opening

Nacelle and compressor inlet arrangements

Aero engine with a bearing chamber and an appliance for introducing oil

Double-jet film cooling structure and method for manufacturing same

Split ring spring dampers for gas turbine rotor assemblies

Gas turbine engine end-wall component

Rotor blade with a conic spline fillet at an intersection between a platform and a neck

Low leakage multi-directional interface for a gas turbine engine

Turbocharger compressor with an elliptical diffuser wall

Fastback vorticor pin

Thermocouple with a vortex reducing probe

Device for sealing between the coaxial shafts of a turbomachine

Gas turbine engine inlet wall design

Rotating turbine component with preferential hole alignment

Cooled airfoil trailing edge and method of cooling the airfoil trailing edge

Gas turbine engine inlet wall design

Flattened nacelle of a turbojet engine

Closure bucket for turbo-machine

Bushing arranged between a body and a shaft, and connected to the body

Bushing arranged between a body and a shaft, and connected to the shaft

Lightweight shrouded fan blade

Elliptical air opening at an upstream end of a fuel injector shroud and a gas turbine engine combustion chamber

Turbomachine rotor disk

Gas turbine engine cooling hole with circular exit geometry

Suction side turbine blade tip cooling

Closed loop cooling system for a gas turbine

Turbocharger and method of manufacturing floating bush

Gas turbine engine component with discharge slot having oval geometry

Asymmetrically shaped trailing edge cooling holes

TURBINE AIRFOIL TRAILING EDGE BIFURCATED COOLING HOLES

Gas turbine engine components with film cooling holes having cylindrical to multi-lobe configurations

Combustor with non-circular head end

Airfoil with improved internal cooling channel pedestals

Gas turbine engine component with converging/diverging cooling passage

Fan blade attachment of gas turbine engine

Double-jet type film cooling structure

Torque frame and asymmetric journal bearing for fan drive gear system

Turbine rotor

Elliptical Sealing System

PROBE ASSEMBLY FOR USE IN TURBINE ENGINES AND METHOD OF ASSEMBLING SAME

Ring sector of turbomachine turbine

NON-CIRCULAR PINS FOR CLOSURE GROUP ASSEMBLY

Rotor for an axial-throughflow turbomachine and moving blade for such a rotor

Compressor impeller blade with variable elliptic connection

Joining mechanism with stem tension and interlocked compression ring

Hybrid Tesla-Pelton Wheel Disc Turbine

Peripheral tunnels propeller

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

Variable vane assembly

Aerofoil having a plurality cooling air flows

Shaped cooling holes for reduced stress

Method and system for cooling engine components

Cooling arrangement

Variable slope exhaust nozzle

High bypass-ratio turbofan jet engine

Swept fan ramp for pivot door thrust reverser

Variable geometry turbine

Particulate mitigating propellant management tank device

Arrangement for propelling an aircraft, aircraft and outlet nozzle for a jet engine

Blade assembly in a combustion turbo-machine providing reduced concentration of mechanical stress and a seal between adjacent assemblies

BLEED HOLES ORIENTED WITH GASPATH AND FLARED FOR NOISE REDUCTION

Integrated engine exhaust systems and methods for drag and thermal stress reduction

Method and device for reducing engine noise

Airfoil for a first stage nozzle guide vane

Turbomachine with variable stator

Rotor shaft, in particular for a gas turbine

Rotating machine

Method and device for reducing engine noise

Intake housing for axial fluid flow engines

Compressor blade with reduced aerodynamic blade excitation

Compressor wheel joint

Turbine blade with impingement cooling

Conical tip shroud fillet for a turbine bucket

Low pressure steam turbine exhaust hood

Conical tip shroud fillet for a turbine bucket

Nozzle airfoil profile with elliptical trailing edge

Scramjet isolator

Scramjet isolator

Additively manufactured bladed-disk having blades with integral tuned mass absorbers

Cast integrally bladed rotor with bore entry cooling

Supersonic elliptical ramp inlet