CIRCUMFERENTIALLY VARYING FAN CASING TREATMENTS FOR REDUCING FAN NOISE EFFECTS

SHROUD OF GAS TURBINE ENGINE AND METHOD OF MANUFACTURING THEREOF

CENTRIFUGAL HEAT DISSIPATION FAN

AIRFOIL FOR A TURBOFAN ENGINE

MIXER VANES

CIRCUMFERENTIALLY VARYING FAN CASING TREATMENTS FOR REDUCING FAN NOISE EFFECTS

Airfoil for a turbofan engine

Circumferentially varying fan casing treatments for reducing fan noise effects

Circumferentially varying fan casing treatments for reducing fan noise effects

Guide vane assembly for an aircraft turbine engine

Trailing edge fuel injection enhancement for flame holding mitigation

Airfoil for a turbofan engine

CENTRIFUGAL HEAT DISSIPATION FAN

Gas turbine engine article with serpentine groove for coating interlock

Gas turbine air bleed arrangement with an inlet

Auxetic three-dimensional structure utilized in additive manufacturing applications

Splined shaft

Mixer vanes having a waveform profile

TURBINE COMPONENT WITH A THIN INTERIOR PARTITION

Ring segment and turbomachine including same

Annular component for supporting a turbine engine bearing

Turbine engine separate flow mixer with lobes

Foils with serrations

Flush fluid inlet designs for aero-acoustic tone mitigation of aircraft

Profiled structure for an aircraft or turbomachine

Channeling furrow upstream of a blade

Turbine rotor blade with platform with non-linear cooling passages by additive manufacture

Erosion-resistant coating with patterned leading edge

Cooling passages for gas turbine engine component

Turbomachine with serrated-profile flow-splitter nose

Air cooler for gas turbine engine

Contoured endwall for a gas turbine engine

Turbine component and methods of making and cooling a turbine component

Airfoil leading edge cooling channels

Deflection seal system

Turbine component and methods of making and cooling a turbine component

Shroud for gas turbine engine

Deliberately mistuned bladed wheel

Turbine component with a thin interior partition

Nozzle of a turbomachine provided with chevrons with a non-axisymmetric inner face

Modulation of vane end serrations

CERAMIC COMPONENT FOR COMBUSTION TURBINE ENGINES

Frangible airfoil for a gas turbine engine

Turbine wheel for a turbine

Fan cowl with a serrated trailing edge providing attached flow in reverse thrust mode

Sealing assembly and gas turbine including the same

NON-CONTINUOUS ABRADABLE COATINGS

Gas turbine engine active clearance control system using inlet particle separator

Liquid bond coatings for barrier coatings

Centrifugal turbo machinery

Hub for propeller having variable-pitch blades, with radial and axial dimensioning variation

Surface heat exchanger and acoustic treatment

Turbine wheel, radial turbine, and supercharger

Airfoil edge cooling channels

Fan wheel, fan, and system having at least one fan

Inlet pre-swirl gas turbine engine

Turbine component assembly

Variable nozzle mechanism and variable displacement type exhaust turbocharger

Turbomachine cooling system

Turbine engine airfoil with a modified leading edge

ENGINE COMPONENT FOR A GAS TURBINE ENGINE

Gas turbine engine component with flow separating rib

Turbofan nacelle assembly with flow disruptor

Turbine engine components with cooling features

High stiffness shape memory alloy actuated aerostructure

Axial fan with grooved trailing edge and outdoor unit

Chamfered stator vane rail

Biomimetic airfoil bodies and methods of designing and making same

Seal device for turbine, turbine, and thin plate for seal device

Turbine vane with coupon having corrugated surface(s)

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

Blade with corrugated outer surface(s)

Turbine rotor blade with coupon having corrugated surface(s)

Turbine shroud with abradable layer having dimpled forward zone

Turbine component and methods of making and cooling a turbine component

Turbine component and methods of making and cooling a turbine component

Turbine component and methods of making and cooling a turbine component

Friction damper

Intermediate central passage spanning outer walls aft of airfoil leading edge passage

Damper ring

Low sound tubeaxial fan

Airfoil with variable slot decoupling

Contra-flow strips, contra-flow seal segments, and methods for inhibiting leakage

Turbine engine guide vane

Fan for smoke and vapor extraction system, in particular for kitchens and extraction system incorporating such a fan

Aerofoil

Gas turbine engine with a cooling fluid path

Airfoil assembly with leading edge element

Cooled CMC wall contouring

EXHAUST NOZZLE FOR GAS TURBINE ENGINE

Vane unit and steam turbine

Impeller for an exhaust gas turbocharger

Cooled turbine runner for an aircraft engine

Jet engine, flying object, and method of operating a jet engine

Containment casing

Article having cooling passage with undulating profile

Alignment of flanged components

Immersed core flow inlet between rotor blade and stator vane for an unducted fan gas turbine

Intermittent grooved soft abradable material to reduce blade tip temperature

Gas turbine guide vane element

Fuel injector device

Incident tolerant turbine vane gap flow discouragement

S-shaped trip strips in internally cooled components

Sliding seal

Non-axisymmetric fan flow path

Baffle for gas turbine engine vane

Mini blind stator leakage reduction

Annular cartridge seal

Cooling of engine components

Nozzle of a turbomachine provided with chevrons with a non-axisymmetric inner face

Tapered cooling channel for airfoil

Leading edge cooling channel for airfoil

Turbine rotor segmented sideplates with anti-rotation

Carriers for turbine components

Core cowl for a turbofan engine

Gas turbine engine end-wall component

COMPONENT

Undulating stator for reducing the noise produced by interaction with a rotor

Debris removal system

Segmented turbine shroud with seals

Acoustic treatment to mitigate fan noise

Aircraft nacelle comprising an improved air intake

Variable dual spring blade root support for gas turbines

Fuel manifold and fuel injector arrangement for a combustion chamber

Fastener

FIRST STAGE NOZZLE OR TRANSITION NOZZLE CONFIGURED TO PROMOTE MIXING OF RESPECTIVE COMBUSTION STREAMS DOWNSTREAM THEREOF BEFORE ENTRY INTO A FIRST STAGE BUCKET OF A TURBINE

Multi-orifice plate for cooling flow control in vane cooling passage

Variable immersion lobe mixer for turbofan jet engine exhaust and method of fabricating the same

Gas turbine engines with turbine rotor blades having improved platform edges

System and method for exhausting combustion gases from gas turbine engines

Noise attenuation in rotating blades

Blade cascade for turbo machine

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

Vortex generators for improved film effectiveness

Clearance control for gas turbine engine section

Airfoils for wake desensitization and method for fabricating same

Fan blade with composite core and wavy wall trailing edge cladding

Energy absorbent fan blade spacer

Turbomachinery seal

Turbine bucket platform leading edge scalloping for performance and secondary flow and related method

Turbine bucket platform shaping for gas temperature control and related method

Gas turbine engine component having wavy cooling channels with pedestals

Turbine component including airfoil with contour

Turbojet engine outlet lobe mixer with guiding protrusions, and method of mixing airflows

Airfoil including trench with contoured surface

Machine with Abradable Ridges and Method

Centering mechanisms for turbocharger bearings

Gas turbine stator vane

Turbomachine comprising an annular casing and a bladed rotor

Turbomachine flow path having circumferentially varying outer periphery

Prestressing device having circumferential activity

Ring diffuser for an axial turbomachine

Turbine and turbine rotor blade

Apparatus and methods for cooling platform regions of turbine rotor blades

SEALING ASSEMBLY FOR USE IN TURBOMACHINES AND METHOD OF ASSEMBLING SAME

Combustor liner assembly with enhanced cooling system

Method and apparatus for enhancing compressor performance

Airfoil having reduced wake

System and method for enhanced turbine wake mixing via fluidic-generated vortices

Ring diffuser for an axial turbomachine

Apparatus for cooling a platform of a turbine component

Variable shape rotor blade

Blade for a turbo device with a vortex-generator

Turbine blade and gas turbine

TURBOFAN GAS TURBINE ENGINE AERODYNAMIC MIXER

Fan

Internally damped blade

Dirt particle separator device for use in a gas turbine engine

DUAL-FLOW TURBINE ENGINE FOR AIRCRAFT WITH LOW NOISE EMISSION

High stiffness shape memory alloy actuated aerostructure

Airfoil Having an Improved Trailing Edge

Centering mechanisms for turbocharger bearings

Bypass duct of a turbofan engine

WALL OF A ROCKET ENGINE

Method for the manufacture of an ejector nozzle tube

Turbine bucket angel wing compression seal

Wall of turbo machine and turbo machine

Stator assembly for a gas turbine engine

Serpentine cooling circuit and method for cooling tip shroud

Component structure

Centering mechanisms for turbocharger bearings

Metering sheet and iso-grid arrangement for a non axi-symmetric shaped cooling liner within a gas turbine engine exhaust duct

Fluted chevron exhaust nozzle

Rotary airfoils and method for fabricating same

Device for suspending guide blades

Turbine blade with an impingement cooling insert

Turbine blade with micro-turbine nozzle provided in the blade root

Tone noise reduction in turbomachines

Moving blade for a turbomachine

Turbomachine nozzle cover provided with triangular patterns having a point of inflexion for reducing jet noise

Exhaust dust flow splitter system

Centering mechanisms for turbocharger bearings

Axial compressor blading

Expansion joint and method of assembling same

Turbine nozzle with trailing edge convection and film cooling

Turbomachine