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

GAS TURBINE ENGINE WITH FORWARD SWEPT OUTLET GUIDE VANES

NOZZLE SECTOR

LOW-FREQUENCY ACOUSTIC CENTER BODY

TURBINE ENGINE HAVING A COMPRESSOR WITH AN INDUCER

OUTLET GUIDE VANES AND AN ACCESSORY DRIVE GEARBOX FOR A GAS TURBINE ENGINE

Low-frequency acoustic center body

Turbine engine having a compressor with an inducer

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

Fuel assembly for a gas turbine engine

GAS TURBINE ENGINE

Turbine wheel

FAN BLADE WITH ZERO TIP DIHEDRAL AT THE HEAD

PORTABLE AND WEARABLE HAND-GRASP NEURO-ORTHOSIS

RADIAL LIFT SEAL

Stator vane for a turbomachine

Air turbine starter with shaped vanes

Radial lift seal

Reverse-flow gas turbine engine

Blade set and blisk

GAS TURBINE ENGINE STATIONARY VANE WITH CONTOURED PLATFORM

Turbocharger turbine housing

Low-frequency acoustic center body

Evaporative cooling pack with same direction flutes designed to prevent nesting

Turbocharger turbine housing scroll passage

Turbomachine turbine having a CMC nozzle with load spreading

COMPONENT ASSEMBLY FOR A COMBUSTION SECTION OF A GAS TURBINE ENGINE

Air turbine starter with shaped vanes

Coolant delivery via an independent cooling circuit

Bypass duct fairing installation

ENGINE COMPONENT ASSEMBLY

Air intake of an aircraft turbojet engine nacelle comprising ventilation orifices for a de-icing flow of hot air

Impeller and axial fan

Ceiling fan

Reverse-flow gas turbine engine

Geared gas turbine engine with reduced fan noise

Wheel of a fluid flow machine

Reverse-flow gas turbine engine

COMPRESSOR HAVING EXTENDED RANGE AND STABILITY

Turbomachine nozzle with an airfoil having a curvilinear trailing edge

Impeller and axial fan

Turning vanes and heat exchangers and methods of making the same

Geared gas turbine engine with reduced fan noise

BLADE FOR A GAS TURBINE ENGINE

Fan system

High performance wedge diffusers for compression systems

Wheel of a fluid flow machine

High efficiency ducted heat exchanger systems

Single ply having plurality of fiber angles

Guide vane airfoil for the hot gas flow path of a turbomachine

ANGLED VANE SLOT

Recuperator for gas turbine engine

Support ring with fluid flow metering

Steam turbine

Gas turbine

Rotatable torque frame for gas turbine engine

Geared gas turbine engine with reduced fan noise

Gas turbine engine hollow fan blade rib orientation

Two spool gas turbine engine with interdigitated turbine section

Turbine wheel for a turbine of an exhaust gas turbocharger

Dimensioning of the skeleton angle of the trailing edge of the arms crossing the by-pass flow of a turbofan

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

FILM HOLE ARRANGEMENT FOR A TURBINE ENGINE

Interdigitated counter rotating turbine system and method of operation

Diffuser for a turbine engine and method of forming same

Full-span forward swept airfoils for gas turbine engines

Reverse-flow gas turbine engine

Gas turbine engine airfoil with showerhead cooling holes near leading edge

Erosion resistant and hydrophobic article

Modular annular heat exchanger

Film-cooled gas turbine component

Engine component assembly

Oil chamber wall

Gas turbine engine airfoil

Turbocharger compressor and method

Gas turbine engine

Multistage compressor with aerofoil portion profiled in a spanwise direction

Converging flow joint insert system at an intersection between adjacent transitions extending between a combustor and a turbine assembly in a gas turbine engine

Power transmission device

Compressor

Engine components with impingement cooling features

Turbine housing

Blade or vane row and gas turbine

Gas turbine

Electroformed nickel-chromium alloy

Turbocompound unit

Fan cooling hole array

Coated cooling passage

Forward-swept impellers and gas turbine engines employing the same

Rotating turbine vane bearing cooling

Blade track assembly with turbine tip clearance control

Blade with metallic leading edge and angled shear zones

Hot gas components with compound angled cooling features and methods of manufacture

Rotor blade with edge protection

Ceiling fan blade

Geared gas turbine engine with reduced fan noise

Compressor inlet recirculation system for a turbocharger

Methods and apparatus to validate translated guest code in a dynamic binary translator

Rotors with stall margin and efficiency optimization and methods for improving gas turbine engine performance therewith

V-shaped gearbox for driving turbomachine equipment

Gas turbine engine airfoil

Rotor assembly for gas turbine

Turbomachine rotor blade, turbomachine rotor disc, turbomachine rotor, and gas turbine engine with different root and slot contact face angles

Frame junction cooling holes

Angled impingement insert

Reduced length transition ducts

Heat exchanger for a turbo engine

Rotor for a turbo-machine and a related method

Drive gearbox on a turbomachine, consisting of a drive train with gear lines extending into non-parallel planes

Methods and apparatus to validate translated guest code in a dynamic binary translator

Water cooled turbine housing

Gas turbine blade

Thermo-acoustic protection structure for a rotating machine

Turbomachine rotor blade

Bleed duct assembly for a gas turbine engine

Gas turbine compressor stator vane assembly

Turbomachine rotor blade

Blade with an S-shaped profile for an axial turbomachine compressor

Centrifugal fluid machine

Stator vane row

Attaching the blades of an axial turbocompressor to the compressor drum

Seal assembly including grooves in an aft facing side of a platform in a gas turbine engine

Seal assembly including grooves in a radially outwardly facing side of a platform in a gas turbine engine

Trailing edge and tip cooling

Propulsion device having unducted counter-rotating and coaxial rotors

Oil deflector

Gas turbine engine preswirler with angled holes

Combustor transition duct assembly with inner liner

Variable blade outer air seal

Shroud for a rotary machine and methods of assembling same

Ladder seal system for gas turbine engines

Turbine engine stator and method of assembly of the same

Axial compressor

Method of Joining at Least Two Components, a Method for Rendering a Component Resistant to Eroision, and a Turbine Blade

Erosion resistant and hydrophobic article

Seals for rotary devices and methods of producing the same

GEARED GAS TURBINE ENGINE WITH REDUCED FAN NOISE

Retrofittable interstage angled seal

FILM COOLED TURBINE COMPONENT

TURBINE BUCKET FOR USE IN GAS TURBINE ENGINES AND METHODS FOR FABRICATING THE SAME

ACOUSTIC LINER

Turbine and turbine rotor blade

Spring loaded seal assembly for turbines

Skewed tip hole turbine blade

First stage impulse steam turbine nozzle axially tangential holes matrix

Angled brush seal and gas turbine engine component combination

Variable bleed valves with inner wall controlled-flow circuits