TURBOMACHINE HAVING AN IMPROVED OIL-RECOVERY DEVICE

COOLING FEATURES FOR A COMPONENT OF A GAS TURBINE ENGINE

ENGINE COMPONENT WITH ABRADABLE MATERIAL AND TREATMENT

MULTISTAGE CENTRIFUGAL PUMP FOR PUMPING FLUID, AN IMPELLER/ SHAFT ASSEMBLY AND A METHOD FOR ASSEMBLING AN IMPELLER/ SHAFT ASSEMBLY

Pump assembly

Turbine stator vane and steam turbine

RADIAL LIFT SEAL

Rotor having crack mitigator

Engine component with abradable material and treatment

Radial lift seal

Turbine blade, and turbine and gas turbine including the same

Turbine vane provided with a recess for embrittlement of a frangible section

ROTOR DISK AND ROTOR BLADE FOR A GAS TURBINE COMPRESSOR OR TURBINE STAGE OF AN AEROENGINE

Turbine blade having gas film cooling structure with a composite irregular groove and a method of manufacturing the same

Torque transmission device with reduced friction

Connection between a ceramic matrix composite stator sector and a metallic support of a turbomachine turbine

Dual density abradable panels

System and method for removably inserting a sensor assembly into a compressor casing

Rotary machine with cooling jacket including helical groove

Fan blade attachment root with improved strain response

Rotor for a turbocharger

Enhanced film cooling system

Stator blades in turbine engines and methods related thereto

Dual-wall airfoil with leading edge cooling slot

Fan blade attachment root with improved strain response

Seal coating

Method and arrangement to minimize noise and excitation of structures due to cavity acoustic modes

COMPRESSOR BLADE SURFACE PATTERNING

Rotary machine

Lever connection of a guide vane adjustment for turbomachinery

Shredding assembly for a grinder pump and centrifugal grinder pump

Liquid propellant rocket engine turbopump drain

3-D measurement of features, including cut-outs and/or grooves

Enhanced film cooling system

BLADE OR VANE FOR A GAS TURBINE ENGINE

Gas turbine

Turbine rotor blade assembly

Liquid bond coatings for barrier coatings

Stress-relieving pocket in turbine nozzle with airfoil rib

Geometry optimized blade outer air seal for thermal loads

Seal fin, seal structure, and turbo machine

Slotted ceramic coatings for improved CMAS resistance and methods of forming the same

Hybrid thermal barrier coating

Systems including rotor blade tips and circumferentially grooved shrouds

GAS TURBINE ENGINE COMPONENT HAVING TIP VORTEX CREATION FEATURE

Turbine engine airfoil with a modified leading edge

Flow control structures for turbomachines and methods of designing the same

Airfoil containment structure including a notched and tapered inner shell

Method of manufacturing a coated turbine blade and a coated turbine vane

Tip leakage flow directionality control

Self retaining face seal design for by-pass stator vanes

Blade comprising a shank, provided with a depressed portion

Dual-wall airfoil with leading edge cooling slot

Fan for aircraft turbomachine

TURBINE COMPONENT THERMAL BARRIER COATING WITH VERTICALLY ALIGNED, ENGINEERED SURFACE AND MULTIFURCATED GROOVE FEATURES

Biomimetic airfoil bodies and methods of designing and making same

Engine component with porous trench

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

TURBINE COMPONENT THERMAL BARRIER COATING WITH CRACK ISOLATING, CASCADING, MULTIFURCATED ENGINEERED GROOVE FEATURES

Turbine shroud with abradable layer having dimpled forward zone

Heat shield with axial retention lock

Fan motor

Intercomponent seal for a gas turbine engine

Turbine rotor blade

Riblets for a flowpath surface of a turbomachine

Gas turbine engine blade casing

Cooled CMC wall contouring

GAS-TURBINE SYSTEM

Reversible spiral groove journal bearing for use on standard and reverse rotation turbochargers

Apparatus and method for air particle separation in a gas turbine engine

Bearing housing

Engine component for a gas turbine engine

Turbine component thermal barrier coating with depth-varying material properties

Turbine abradable layer with inclined angle surface ridge or groove pattern

Turbine component thermal barrier coating with crack isolating engineered groove features

Fan blade attachment root with improved strain response

Disk lug cooling flow trenches

Turbine blade damper system having pin with slots

Rotor blade having a flared tip

Centrifugal multiblade blower

Multi-stage inter shaft ring seal

Turbine blade platform undercut with decreasing radii curve

Water removal device for steam turbine and method for forming slit

Cooling of engine components

Water removal device for steam turbine

Centrifugal compressor and turbocharger

Methods and system for fluidic sealing in gas turbine engines

Rotor disk blade with friction-held root, rotor disk, turbomachine and associated assembly method

Stator assembly for a gas turbine engine

Core cowl for a turbofan engine

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

Riffled seal for a turbomachine, turbomachine and method of manufacturing a riffled seal for a turbomachine

Serrated outer surface for vortex initiation within the compressor stage of a gas turbine

Brush seal

Edge treatment for gas turbine engine component

Gas turbine engine component external surface micro-channel cooling

Exhaust liner flange cooling

Gas turbine engine component having tip vortex creation feature

Gas turbine rotor blade and gas turbine rotor

Tip leakage flow directionality control

Components resistant to traveling wave vibration and methods for manufacturing the same

Turbine abradable layer with zig zag groove pattern

Gas turbine engine

Turbocharger with variable turbine geometry having grooved guide vanes

ATR axial V-groove

Integrated nozzle and plug

ATR full ring sliding nacelle

ATR guide pins for sliding nacelle

Variable geometry system turbocharger and method of manufacturing housing for variable geometry system turbocharger

Thermal management article and method of forming the same, and method of thermal management of a substrate

Centrifugal pump

Stationary part sealing structure

Process for producing a layer system

Gas turbine shroud assemblies

Impingement cooling mechanism, turbine blade and cumbustor

Coating interface

Turbine blade

Vortex generators for improved film effectiveness

Turbine

ROTATING ASSEMBLY FOR A TURBINE ASSEMBLY

Gas turbine stator assembly

Turbine component including airfoil with contour

Bucket assembly for turbine system

Airfoil including trench with contoured surface

REDUCTION IN THERMAL STRESSES IN MONOLITHIC CERAMIC OR CERAMIC MATRIX COMPOSITE SHROUD

Platform cooling passages and methods for creating platform cooling passages in turbine rotor blades

Turbofan and indoor unit of air-conditioning apparatus including the same

Methods of fabricating a coated component using multiple types of fillers

Endwall component for a turbine stage of a gas turbine engine

Composite vane mounting

Composite vane mounting

Flow discouraging systems and gas turbine engines

Reverse vortex ring (RVR) for dramatic improvements in rocket engine turbomachinery rotordynamic stability margins