Cooling system of the AVIONIC RIGS of the M346 aircraft present in the test laboratory

The system created has the purpose of allowing the equipment to cool
avionics of RIG 1, 2 and 3 of the M346 aircraft and consists of the following parts:
1. Liquid chiller unit
2. Motor fan with flow rate of about 800 m³/h for “RIG2” test bench
3. Plenum for connection to the “RIG2” test bench
4. Motor fan with flow rate of about 1000 m³/h for “RIG1” and “RIG3” test bench
5. Plenum for connection to the “RIG1” test bench
6. PIPING three-way distribution to the devices placed individually in the technical compartments of
reference