FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft auxiliary power plant. Proposed power plant comprise conversion reactor, battery of fuel cells, fuel storage and feed units communicated with conversion reactor, afterburner, turbine with its shaft supporting compressor and electric generator. Conversion reactor generating synthesis gas is integrated with battery of said fuel cells. Synthesis gas generation channel communicates with fuel or oxygen feed channels and intermediate gas manifold of synthesis gas passage into fuel cells, while anode and cathode gas discharge channels are communicated with afterburner.
EFFECT: higher power output and reduced fuel consumption.
3 cl, 1 dwg
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