An apparatus is provided for supplying electrical power and cooling for an aircraft. The apparatus includes a cooling turbine coupled to a shaft, a compressor coupled to the shaft, and including an input for receiving engine bleed air or ambient air, and an output for discharging compressed air, a flywheel coupled to the shaft, a power turbine coupled to the shaft, and a starter generator coupled to the shaft between the compressor and the power turbine.
Apparatus for aircraft with high peak power equipment
03.05.2016
Patent
Elektronische Ressource
Englisch
APPARATUS FOR AIRCRAFT WITH HIGH PEAK POWER EQUIPMENT
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