Structure and Operation of the Test Bench
An advanced facility with hydraulic, electrical, and cooling systems designed to operate autonomously, ensuring safety and efficiency in aviation testing
The system consists of the following main groups:
Mechanical structure and guards including:
- work surface equipped with component clamping system and drip surface
- machine fairing with interlocked and fixed guards
- operator side access doors equipped with openings in transparent safety material
Hydraulic system including:
- n°1 hydraulic power unit
- n°4 hydraulic blocks for the control of different pressure and flow ranges
- n°1 closed circuit oil recirculation, filtering and cooling circuit with chiller for water cooling
Electrical power, actuation and safety system including:
- n°1 main general power cabinet with standard PLC and safety PLC
- n°1 pendant control panel
- n°1 consent pedal for opening doors
Cooling system including:
- n°1 oil recirculation and filtering unit
- n°1 plate water/oil heat exchanger
- n°1 chiller for the conditioning of the water cooling
The bench is designed to be started and left running autonomously.