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While designing refrigeration system of an aircraft, the prime consideration is that
1. System has high COP
2. Power per TR is low
3. Mass of refrigerant circulated in the system is low
4. Mass of refrigeration system is low

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Correct Answer - Option 4 : Mass of refrigeration system is low

Explanation:

Aircraft cooling systems:

In an aircraft, cooling systems are required to keep the cabin temperatures at a comfortable level. Even though the outside temperatures are very low at high altitudes, still cooling of cabin is required due to: 

  • Large internal heat generation due to occupants, equipment etc. 
  • Heat generation due to skin friction caused by the fast moving aircraft.
  • At high altitudes, the outside pressure will be sub-atmospheric. When air at this low pressure is compressed and supplied to the cabin at pressures close to atmospheric, the temperature increases significantly.
  • Solar radiation

For low speed aircraft flying at low altitudes, cooling system may not be required, however, for high speed aircraft flying at high altitudes, a cooling system is a must.

Even though the COP of air cycle refrigeration is very low compared to vapour compression refrigeration systems, it is still found to be most suitable for aircraft refrigeration systems as: 

  • Air is cheap, safe, non-toxic and non-flammable. Leakage of air is not a problem.
  • Cold air can directly be used for cooling thus eliminating the low temperature heat exchanger (open systems)
  •  The aircraft engine already consists of a high speed turbo-compressor, hence separate compressor for cooling system is not required. This reduces the weight per kW cooling considerably. Typically, less than 50% of an equivalent vapour compression system
  • Design of the complete system is much simpler due to low pressures. Maintenance required is also less. 

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