AIRFOIL ROTOR HUB SYSTEM HAVING INTENTIONAL FREQUENCY MISTUNING

COMPLIANT SHROUD DESIGNS WITH VARIABLE STIFFNESS

LOW-FREQUENCY ACOUSTIC CENTER BODY

Compliant shroud designs with variable stiffness

Turbine engine with a flow splitter having a profile with inclined serrations

Mixer vanes

Compliant shroud designs with variable stiffness

Stator blade for a centrifugal compressor

Profiled structure for an aircraft or turbomachine

Gas turbine engine components having interlaced trip strip arrays

Angular sector for turbomachine blading with improved sealing

Erosion-resistant coating with patterned leading edge

Free-tipped axial fan assembly

Cooling passages for gas turbine engine component

Turbomachine with serrated-profile flow-splitter nose

Turbine engine with a flow splitter having a profile with inclined serrations

Turbine component and methods of making and cooling a turbine component

Method of forming a cure tool and method of forming a textured surface using a cure tool

COOLING HOLE GEOMETRY FOR GAS TURBINE ENGINE COMPONENTS

Airfoil leading edge cooling channels

Turbine component and methods of making and cooling a turbine component

TURBINE ELEMENT FOR HIGH PRESSURE DROP AND HEAT TRANSFER

Trip strips for augmented boundary layer mixing

Trip strip configuration for gaspath component in a gas turbine engine

COMPRESSOR BLADE SURFACE PATTERNING

Impingement cooling features for gas turbines

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

Modulation of vane end serrations

First-stage turbine vane supporting structure and gas turbine including same

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

BLADE OR VANE FOR A GAS TURBINE ENGINE

NON-CONTINUOUS ABRADABLE COATINGS

Turbine airfoil with turbulating feature on a cold wall

Airfoil edge cooling channels

Variable nozzle mechanism and variable displacement type exhaust turbocharger

GAS TURBINE ENGINE COMPONENT HAVING TIP VORTEX CREATION FEATURE

Three dimensional auxetic structure, manufacturing method and tooling

AIRFOIL IMPINGEMENT CAVITY

Turbine engine bearing assembly and method for assembling the same

Turbine engine airfoil with a modified leading edge

Outlet guide vane for aircraft turbomachine, with improved lubricant cooling function

Method for manufacturing blisk, and blisk intermediate product

Turbine blade with ultrasonic wave scattering feature

Undulating tip shroud for use on a turbine blade

Airfoil trailing edge segment

Multi-ply seal

Free-tipped axial fan assembly

Axial fan with grooved trailing edge and outdoor unit

Biomimetic airfoil bodies and methods of designing and making same

Combustor cooling panel, transition piece and combustor including the same, and gas turbine including combustor

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

Crack stopper for welds

Damper ring

Axial Turbine Engine Compressor De-Icing Blade

Turbine engine guide vane

Turbofan and indoor unit for air conditioning apparatus

Internal cooling system with insert forming nearwall cooling channels in midchord cooling cavities of a gas turbine airfoil

Internal cooling system with insert forming nearwall cooling channels in an aft cooling cavity of an airfoil usable in a gas turbine engine

Turbine airfoil having near-wall cooling insert

Aerofoil

Turbine abradable layer with compound angle, asymmetric surface area ridge and groove pattern

Impeller for an exhaust gas turbocharger

Vehicle cooling fan with aerodynamic stator struts

Turbine abradable layer with inclined angle surface ridge or groove pattern

Tapered land thrust bearing device and turbocharger provided with the bearing device

Rotating labyrinth M-seal

Incident tolerant turbine vane gap flow discouragement

Air-blowing device

Gas turbine engine with seal having protrusions

Turbulator structure on combustor liner

Baffle for gas turbine engine vane

Blade

Mini blind stator leakage reduction

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

Multi-stage-type compressor and gas turbine equipped therewith

Core cowl for a turbofan engine

Debris removal system

Gas turbine engine component having tip vortex creation feature

Variable dual spring blade root support for gas turbines

Method and apparatus for cooling tower fan mounting for removal from inside the tower

Turbine abradable layer with zig zag groove pattern

Interwoven channels for internal cooling of airfoil

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

Thermo-acoustic protection structure for a rotating machine

Transition duct assembly with modified trailing edge in turbine system

Hollow component manufacture

Turbojet fan blade

Noise attenuation in rotating blades

Housing section of a turbine engine compressor stage or turbine engine turbine stage

Cooling system including wavy cooling chamber in a trailing edge portion of an airfoil assembly

Fan containment system

Nozzle with guiding devices

Airfoil with variable trip strip height

Cooling system in a turbine airfoil assembly including zigzag cooling passages interconnected with radial passageways

Vortex generators for improved film effectiveness

Convolution seal for transition duct in turbine system

Shark-bite tip shelf cooling configuration

Cooling hole with crenellation features

Turbofan engine mixer assembly

Turbine Shroud Impingement System with Bellows

Trailing edge cooling system in a turbine airfoil assembly

CHEVRON PLATFORM TURBINE VANE

Machine with Abradable Ridges and Method

Interface between a combustor basket and a transition of a gas turbine engine

Gas turbine blade for a turbomachine

Film cooled component wall in a turbine engine

METHOD FOR OPTIMIZING THE CONTACT SURFACES OF SHROUD SEGMENTS, WHICH ABUT AGAINST ONE ANOTHER, OF ADJACENT BLADES OF A GAS TURBINE

Gas turbine engine exhaust mixer including circumferentially spaced-apart radial rows of tabs extending downstream on the radial walls, crests and troughs

Charging device

Shroud for rotating blades of a turbo machine, and turbo machine

Internally damped blade

Shroud and rotary vane wheel of propeller fan and propeller fan

WALL OF A ROCKET ENGINE

Method for the manufacture of an ejector nozzle tube

THERMALLY BALANCED AERO STRUCTURES

THERMALLY BALANCED MATERIALS

Fan casing assembly

External fan duct casing in a turbomachine

Serpentine cooling circuit and method for cooling tip shroud

Sensor for quantifying widening reduction wear on a surface

Fluted chevron exhaust nozzle

Inspection tool for measuring bucket Z notch position

Wind turbine blade with anti-noise devices

Device for suspending guide blades

Turbine blade trip strip orientation

METHODS AND APPARATUS FOR LOAD TRANSFER IN ROTOR ASSEMBLIES

Turbine blade tip shroud

Gas exhaust nozzle for a bypass turbomachine having an exhaust or throat section that can be varied by moving the secondary cowl

Shroud and rotary vane wheel of propeller fan and propeller fan

Spacing arrangement

Device for reducing the jet noise of a turbomachine

Turbomachine

7FAstage 1 abradable coatings and method for making same