Viscous material leakage at rotor shaft interfaces causes equipment downtime and batch contamination during high-torque rubber compounding.
Inconsistent pressure during retreading leads to wing portion deflection and poor adhesion between the thermoplastic tread and tire carcass.
High-viscosity elastomer compounds escape through rotating shaft gaps when labyrinth and thread clearances are not optimized for pressure containment.
Abrasive rubber compounds cause rapid degradation of rotor blade tips, necessitating frequent maintenance and causing surface profile inaccuracies.