Unit for supplying auxiliary power to aircraft includes a gas turbine with a combustion chamber, a blower, a turbine coupled to a compressor to generate compressed air and a fuel cell to generate electrical energy.

摘要

A gas turbine (GT) has a combustion chamber (BK), a blower (V) and a turbine (T). A compressor (K) is coupled to the turbine to generate compressed air. A fuel cell (BZ) generates electrical energy.