An anti-lock braking system for an aircraft, including a braking actuator configured to apply a braking pressure to a brake stator, and a piezoelectric actuator connected in series with the braking actuator. The piezoelectric actuator is operable to modify the braking pressure applied to the brake stator to provide anti-skid protection.
ANTI-LOCK BRAKING SYSTEM
2024-07-11
Patent
Elektronische Ressource
Englisch