TEST BENCH FOR ACTUATORS USED IN AERONAUTICS
The main objective of this activity is to design and build an innovative test bench capable of subjecting linear electromechanical actuators, used in the aeronautical field, to both static and dynamic functional tests with variable resistant load throughout the actuator stroke, simulating conditions of critical work according to the high standards required for these applications (limit load, last load, backlash, endurance, temperature …).