HYBRID TRANSMISSION COMPONENT FOR A GAS TURBINE ENGINE

Vacuum pump and rotating cylinder provided in vacuum pump

Face sheet of acoustic liner having streamlined holes with elongated edges

Long-arm flange design for connecting and supporting thin-walled parts subject to high bending and thermal loads

Exhaust collector conversion system and method

Variable gap between impeller rotor and static structure

Aircraft propulsion system with variable area inlet assembly

Turbine blade, manufacturing method for turbine blade, and gas turbine

Exhaust collector conversion system and method

Turbine shaft, turbocharger, and manufacturing method of turbocharger

SELF-CENTERING SEAL AND METHOD OF USING SAME

BOUNDARY LAYER TURBOMACHINE

Turbine blade tip wall cooling

Ribbed pin fins

RETENTION OF A ROTOR OF AN ELECTRONICALLY-CONTROLLED TURBOMACHINE

Control ring for a stage of variable-pitch vanes for a turbine engine

Vacuum pump and rotating cylindrical body included in vacuum pump

Gas turbine engine vane attachment feature

Liquid propellant rocket engine turbopump drain

Contacting dry face seal with tapered carbon nose

Turbine rotor blade assembly

Turbine for a turbine engine

Intershaft seal assembly with multi-axis stepped grooves

Coated turbine component and method for forming a component

Tapered composite backsheet for use in a turbine engine containment assembly

Connecting element

ENGINE COMPONENT FOR A GAS TURBINE ENGINE

RING FOR CONTROLLING A STAGE OF VARIABLE-SETTING VANES FOR A TURBINE ENGINE

Airfoil containment structure including a notched and tapered inner shell

Alignment apparatus for coupling diaphragms of turbines

Variable nozzle unit and variable displacement-type turbocharger

Inducer and pump

Blast fan

Airfoil with stepped spanwise thickness distribution

Chamfered stator vane rail

Turbine components and method for forming turbine components

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

Turbine shroud with abradable layer having dimpled forward zone

Blade or vane row and gas turbine

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

Integral instrumentation in additively manufactured components of gas turbine engines

Bidirectional axial fan device

Rotor assembly with wear member

Boundary layer turbomachine

Seal housing pre-taper

Seal for turbofan engine

Tapered cooling channel for airfoil

Leading edge cooling channel for airfoil

Airfoil with stepped spanwise thickness distribution

Electric submersible pump assembly bearing

Partially coated blade

Blade outer air seal having partial coating

Components with cooling channels and methods of manufacture

Knife edge with increased crack propagation life

Assembly

Fastback vorticor pin

Blade cooling circuit feed duct, exhaust duct, and related cooling structure

Fan blade composite cover with tapered edges

Rotor blade and guide vane airfoil for a gas turbine engine

Turbine airfoil with local wall thickness control

ATR axial V-groove

Integrated nozzle and plug

ATR full ring sliding nacelle

ATR guide pins for sliding nacelle

Bearings for a turbomachine having an electric motor

Acoustically treated thrust reverser track beam

Tapered-land thrust bearing for turbochargers

Turbomachine rotor blade

Adjustable gib shim

Variable displacement turbocharger and assembly method of variable nozzle mechanism

Rotor assembly

Inner turbine shell axial movement

Ceramic core tapered trip strips

Gas turbine engine comprising a tension stud

Turbine airfoil and method for thermal barrier coating

Blade and method for manufacturing blade

Method for manufacturing aircraft engine cases with bosses

Components with cooling channels and methods of manufacture

Blade outer air seal having partial coating

PLUG ASSEMBLY FOR BLADE OUTER AIR SEAL

Curved Passages for a Turbine Component

Turbine combustion system transition piece side seals

Turbine combustion system cooling scoop

Belted toroid pressure vessel and method for making the same

Gas turbine engine air intake in a nacelle

Turbine engine compressor stator

Axially angled annular seals

Gas turbine engine sealing structure

Ceramic core tapered trip strips

Cooled blade for a gas turbine, method for producing such a blade, and gas turbine having such a blade

Turbocharger

turbine engine component for adaptive cooling

Airfoil incorporating tapered cooling structures defining cooling passageways

Castings, Casting Cores, and Methods

Fastback turbulator structure and turbine nozzle incorporating same

Rotating body

Chamfer rail pockets for turbine vane shrouds

Turbine blade platform

Device and method for connecting a blade to a rotor shaft of a continuous flow machine

DIFFUSER ARRANGEMENT

Floatable unit for evacuation purposes

Turbocharger with improved charge pressure regulating flap configuration

Actuator

Actuator

Turbo engine

Impingement cooling arrangement

Airfoil with tapered radial cooling passage

Gas turbine nozzle seals for 2000° F. gas containment

Method of friction welding

AXIAL BLADE SLOT PRESSURE FACE WITH UNDERCUT

Method to prevent brinelling wear of slot and pin assembly

Aerofoil configuration

Apparatus and method for active gap monitoring for a continuous flow machine

Cantilevered nozzle with crowned flange to improve outer band low cycle fatigue

Crowned rails for supporting arcuate components

Cooling arrangement for a tapered turbine blade

System and method for aligning and sealing a turbine shell assembly

Curved variable pitch wedge retention in vane outer base

Tip ramp turbine blade

Bell-shaped fan cooling holes for turbine airfoil

Fan frame

Wedge repair of mechanically retained vanes

Mechanical coupling for a rotor shaft assembly of dissimilar materials

Skewed tip hole turbine blade

Adjustment assembly

Method to augment heat transfer using chamfered cylindrical depressions in cast internal cooling passages

Turbine airfoil with weight reduction plenum

High pressure turbine disk hub with reduced axial stress and method

Damper cooled turbine blade

Blunt tip turbine blade

Rotor assembly with cooling air deflectors and method

Compressor blade with a chamfered tip

Cooling arrangement

Stress defender holes

Bore and shaft assembly

Bore and shaft assembly

Turbine nozzle with trailing edge convection and film cooling

Flow restrictors for aircraft inlet acoustic treatments, and associated systems and methods

Fluid Flow Channels in Bladeless Compressors, Turbines and Pumps

Aerofoil containment structure

Rotor assembly with cooling air deflectors and method

Method for manufacturing aircraft engine cases with bosses

Braided wire damper for segmented stator/rotor and method

Turbine case reinforcement in a gas turbine jet engine

Bore and shaft assembly

Device and method for detachably connecting an impeller to a shaft

Variable vane arm/unison ring attachment system

High-efficiency jet ejector and propulsive jet

Method of installing stationary blades of a turbine and turbine structure having a radial loading pin

Cooled gas turbine engine vane

Exhaust diffuser assembly with tunable velocity profile