HEAT EXCHANGERS FOR GAS TURBINE ENGINES

HEAT EXCHANGER INLET VANE ASSEMBLIES WITH IMPROVED MIXING TRAILING EDGE FEATURES

Exhaust mixer with protrusions

Turbine rotor for a turbomachine

Rotor containment structure

Turbomachinery seal plate with variable lattice densities

Auxiliary turbomachinery weight reduction using internal engineered design

Rotor containment structure

Labyrinth seal and gas turbine

Turbomachinery seal plate with variable lattice densities

Barrier layer and surface preparation thereof

Flared central cavity aft of airfoil leading edge

Inner barrel of an engine inlet with laser-machined acoustic perforations

Investment casting core bumper for gas turbine engine article

Impingement cooling with impingement cells on impinged surface

Labyrinth seal with variable tooth heights

Cost effective manufacturing method for GSAC incorporating a stamped preform

Flared central cavity aft of airfoil leading edge

Balance bracket

Hot section dual wall component anti-blockage system

Cooling circuit with shaped cooling pins

Inner barrel of an engine inlet with laser-machined acoustic perforations

Labyrinth seal with variable tooth heights

Gas turbine engine hollow fan blade rib orientation

GAS TURBINE ENGINE COMPONENT HAVING TIP VORTEX CREATION FEATURE

Reduced drag system for windmills, fans, propellers, airfoils, and hydrofoils

Turbine component with shaped cooling pins

Split-zone flow metering T-tube

Flared central cavity aft of airfoil leading edge

Acoustic Nozzles For Inlet Bleed Heat Systems

Fluid system

Turbine blade with sectioned pins and method of making same

Turbine component including mixed cooling nub feature

Method of manufacturing a component of a turbomachine, component of a turbomachine and turbomachine

Impeller for an exhaust gas turbocharger

Aerofoil

Turbine component thermal barrier coating with depth-varying material properties

Vehicle cooling fan with aerodynamic stator struts

Turbine component thermal barrier coating with crack isolating engineered groove features

Composite fan inlet blade containment

Cost effective manufacturing method for GSAC incorporating a stamped preform

Gas turbine engine end-wall component

Gas turbine engine component having tip vortex creation feature

Cooling hole arrangement for engine component

Method for 3-D printing a pattern for the surface of a turbine shroud

Panel attachment system

Damping device for being situated between a housing wall and a casing ring of a housing of a thermal gas turbine

Noise attenuation in rotating blades

Airfoil having a profiled trailing edge for a fluid flow machine, blade, and integrally blade rotor

Stator vane mistake proofing

Bipod flexure ring

Gas turbine engine and cooled flowpath component therefor

Turbine blade tip shroud for use with a tip clearance control system

Discreetly defined porous wall structure for transpirational cooling

Airfoil incorporating tapered cooling structures defining cooling passageways

PATTERNED TURBOMACHINE COMPONENT AND METHOD OF FORMING A PATTERN ON A TURBOMACHINE COMPONENT

Method of manufacturing a blade

WALL OF A ROCKET ENGINE

Bipod flexure ring

Method for the manufacture of an ejector nozzle tube

Method of manufacturing a blade

Diffuser for decelerating a compressed fluid

COMPONENT WITH DIAGONALLY EXTENDING RECESSES IN THE SURFACE AND PROCESS FOR OPERATING A TURBINE

LABYRINTH SEAL WITH REDUCED LEAKAGE FLOW BY GROOVES AND TEETH SYNERGISTIC ACTION

Bipod Flexure Ring

Airfoil and method for protecting airfoil leading edge

Airfoil and method for protecting airfoil leading edge

Patterned reduction of surface area for abradability

Turbomachine casing with treatment, a compressor, and a turbomachine including such a casing

Air-cooled component

Fanned trailing edge teardrop array

Refractory metal core cooling technologies for curved leading edge slots

Counterflow film cooled wall

Methods and apparatus for maintaining rotor assembly tip clearances

Fanned trailing edge teardrop array