The present application belongs to the technical field of
aviation fuel structure design, and particularly relates to a method and structure for reducing fuel violent shaking. The structure comprises a
fuel tank shell, a rear guide plate, a rear
flow divider, a
fuel tank interior, a crescent guide plate, a front guide plate and a front
flow divider. The overall shape of the
fuel tank is a long cylindrical
ellipse, which is symmetrical in front and back and symmetrical in left and right. The fuel tank interior is arranged with a flow guiding and dividing mechanism composed of the rear guide plate, the rear
flow divider, the crescent guide plate, the front guide plate and the front flow divider. The fuel with opposite speed components collides, thereby reducing the overall
momentum of the fuel, which conforms to scientific principles. The flow guiding and dividing mechanism can be
cut from the same material as the fuel tank, has a simple shape, no thickness requirement, is directly welded on the fuel tank shell, is economical and practical, does not need to be maintained, and has strong practicality. The position, shape and size of the flow guiding and dividing mechanism are set precisely, and the
maximum efficiency of the internal collision of the
oil can be achieved to achieve the purpose of fuel anti-shaking.