FIELD: thermal aerostatic flying vehicles. SUBSTANCE: heat generator includes fan 9, turbine 8 whose blades are secured on fan rim, combustion chamber 6 with injectors 1 connected to fuel gas bottle, compressor 7, swivel exchaust branch pipe 13 and mixer 14. Turbine 8, compressor 7 and fan 9 are mechanically interconnected. Mixer 14 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. 5 cl, 3 dwg
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|---|---|---|---|
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