GEOMETRICALLY SEGMENTED COATING FOR THERMAL INSULATION AND ABRADABILITY PROTECTION

MOVING BLADE FOR A TURBINE OF A TURBINE ENGINE, COMPRISING A STILT EQUIPPED WITH PROJECTIONS FOR RADIALLY RETAINING THE BLADE

Engine component with structural segment

Systems and methods for manufacturing film cooling hole diffuser portion

A TURBOMACHINE BLADE OR VANE HAVING A VORTEX GENERATING ELEMENT

Film-cooled multi-walled structure with one or more indentations

ANGLED IMPINGEMENT INSERTS WITH COOLING FEATURES

Turbomachine component with coating-capturing feature for thermal insulation

Systems and methods for manufacturing film cooling hole diffuser portion

Turbine wheel with clamped blade attachment

Impingement insert

Turbine engine airfoil insert

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

Film-cooled gas turbine component

Method for repairing a fan casing

Cooled hot section components for a gas turbine engine

Impingement holes for a turbine engine component

Angled impingement inserts with cooling features

Film cooled multi-walled structure with one or more indentations

Turbine engine component with diffuser holes

Engine component

Turbine wheel with clamped blade attachment

Shroud assembly for a turbine engine

Gas turbine engine component external surface micro-channel cooling

Gas turbine blade

Turbine casing false flange flow diverter

Turbine blade

Gas turbine engine component with multi-lobed cooling hole

Turbine blade tip with vortex generators

Passive boundary layer control elements

Burner including non-uniformly cooled tetrahedron vortex generators and method for cooling

Airfoil with tapered radial cooling passage

ARTICLE HAVING A PROTECTIVE COATING AND METHODS

Wall cooling arrangement