FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to water bombers water intake systems. Water intake consists of the hatch at tank bottom, cylindrical manifold to house the pump, vertical shaft to engage the latter with the drive mechanism composed by sealed motor-driven conical gears, sliding carriage fitted in said vertical shaft with tight cover to allow water feed to said pump by means of levers and hydraulic cylinder. Water intake from pool into tank is performed at stay thereat via one hatch at tank bottom equipped with the pump driven by self-contained DC motor supplied from onboard storage batteries.
EFFECT: possibility of water intake from small pools.
6 cl, 6 dwg
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