TURBINE ENGINE WITH A BLADE ASSEMBLY HAVING COOLING CONDUITS

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

Pressure sensor noise filter prior to surge detection for a gas turbine engine

Radial turbine

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

Gas turbine engine airfoil trailing edge passage and core for making same

Active clearance control manifold system

Gas turbine engine airfoil with dirt purge feature and core for making same

Rotatable component with controlled load interface

Fluid flow machine including rotors with small rotor exit angles

Method for repair of housings

Turbine engine and bladed rotor for a compression stage of a turbine engine