| 摘要 |
The aircraft has a supply system with first electrochemical reactor (1) for generating energy, hydrogen, oxygen and clear water from grey water, hydrocarbon fuel and air, whereby the first reactor at least partly forms at least one of the systems selected from an auxiliary drive mechanism for generating compressed air and electrical energy, a ram air turbine, a clear water tank of a water system, a drive mechanism generator for generating electrical energy and an oxygen supply system. |
