FIELD: aviation.
SUBSTANCE: fuel tank (1) is located in wing panel (2) of the aircraft and is equipped with filler. Filler is made from material capable of adsorption of used aviation fuel with subsequent desorption. Part of internal volume of fuel tank (4) from sides of wing end part (5) is filled with filler directly.
EFFECT: ruled out static electricity charges and hydraulic shock inside tank space.
7 cl, 4 dwg
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