Oil tank for aircraft

Aeronautics and astronautics – Aircraft structure – Fuel supply

Patent

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Details

220 1B, 220 3, 220 86R, 220 5A, 220 85S, 141325, B64D 3702, B65D 602

Patent

active

044443668

ABSTRACT:
An oil tank for an aircraft mounted engine compensates for differences in oil capacity occasioned when the oil tank in each engine mounted under the wing is oriented with respect to the wing's dihedral angle and the angle of the engine which is normal to the wing. The tank includes a first portion for receiving the oil and integral expansion portion where the oil tank is below the right wing dihedral and the expansion is above the left wing dihedral.

REFERENCES:
patent: 2621719 (1952-12-01), Eaton et al.

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