FIELD: transport.
SUBSTANCE: set of invention relates to auxiliary power plants for aircraft. Proposed power supply system comprises engine, system of fuel elements to supply aircraft, first engine fuel tank and second engine fuel tank with fuel for fuel elements. First fuel tank is separated from second fuel tank. System of fuel elements is connected with the wing de-icing device to prevent wing icing by using products accumulated in operation of the system of fuel elements.
EFFECT: aircraft uninterrupted power supply.
26 cl, 3 dwg
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