Integral Blade Disc Deformation Control in Five-Axis Machining: Prediction, Suppression, and Compensation Method
Integrated blade discs are core components of aircraft engine compressors and turbines. By replacing the traditional tongue-and-groove joint between blades and the disc with an integrated design, they can reduce weight by approximately 30% and improve aerodynamic efficiency by more than 15%, making them a hallmark technology of advanced aircraft engines.










