Invention Grant
US09328661B2 Apparatus for aircraft with high peak power equipment 有权
具有高峰值功率设备的飞机设备

Apparatus for aircraft with high peak power equipment
Abstract:
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.
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