Composite airfoil assembly for an interdigitated rotor

Film cooling hole including offset diffuser portion

Gas turbine engine airfoil platform edge geometry

Gas turbine engine shaft bearing configuration

Systems and apparatus relating to compressor stator blades and diffusers in turbine engines

Method for forming a pressure measurement hole in a component

Variable nozzle mechanism

Method for the production of coated turbine moving blades and moving-blade ring for a rotor of an axial-throughflow turbine

Variable geometry turbine

Bullnose seal turbine stage

Turbo machine with a rotor which has at least one rotor disk with a bore

Turbine blade and method of fabricating same

Bullnose step turbine nozzle