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Commercial Aircraft Environmental Control Systems

Airframe Systems Series

  • Research Code : 9AB0-00-1E-00-00
  • SKU : AE00147-NA-MR_00147
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  • Release Date : 15-Sep-2015
  • Region : North America
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In the typical aircraft environmental control systems (ECS), the bleed air is cooled by air from the aircraft slipstream and then enters a compressor, which boosts the turbine inlet pressure to increase the temperature drop. Air leaving the compressor is cooled to eliminate the excess moisture before entering the turbine. Cold air from the turbine is cooled before it is mixed with warm air from the cabin. Air at controlled temperature is then pumped into the cabin. This research was conducted based on the aircraft deliveries during 2014, including the costs and sources of ECS equipment on board those aircraft as they were delivered to the airlines. The forecast extends through 2020.
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