FIELD: thermal aerostatic flying vehicles. SUBSTANCE: heat generator includes fan 9, turbine 7, combustion chamber 6 with injectors 1 connected to fuel gas bottle 5, gas-to-air heat exchanger 13 and gas-to-fuel heat exchanger 3, compressor, swivel exhaust branch pipe 11 and mixer 12. Turbine 7, compressor 8 and fan 9 are mechanically interconnected. Mixer 12 is located under lower neck of montgolfier envelope and mixture of air fed by fan 9 and combustion products is forced to this envelope. EFFECT: enhanced economical efficiency and safety of flights. 4 cl, 2 dwg
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|---|---|---|---|
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