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The United States Government embarked on the Integrated High Performance Turbine Engine Technology (IHPTET) initiative to double the thrust to weight (Fn/Wt) performance from baseline turbine engines produced in the mid 1980’s. In order to achieve these improvements, increases in engine systems temperature and pressure and decreases in weight must be simultaneously accomplished. Under IHPTET, the United States Air Force (USAF) funded the Component and Engine Structural Assessment Research (CAESAR) Program, whose goal is to demonstrate the rules and tools of the design intent for transitioning new materials. Of these materials, this article will critically review gamma titanium aluminide (TiAl), and comment on design issues, material property comparisons and manufacturing challenges required for successful static and rotating component demonstration.

Designing with Gamma Titanium CAESAR Program Titanium Aluminide Component Applications