Bidirectional fuel supply balance system and correction method for fuel tanks in left and right wings of aircraft

The invention relates to a bidirectional fule supply balance system for fuel tanks in left and right wings of an aircraft, the system comprises a left fuel tank breather pipe, a left stamping air inlet pipe, a right fuel tank breather pipe, a right stamping air inlet pipe, a fuel tank pressure balance pipe, a fuel collecting tank, a left fuel tank fuel supply pipeline, a right fuel tank fuel supply pipeline and an aircraft engine fuel supply pipeline, wherein, the fuel tank pressure balance pipe is communicated with the fuel tank in the left wing of the aircraft and the fuel tank in the right wing of the aircraft. In addition, the invention relates to a bidirectional fuel supply balance correction method for the fuel tanks in the left and right wings of the aircraft, and the method is implemented based on the bidirectional fuel supply balance system for the fuel tanks in the left and right wings of the aircraft. 本申请涉及一种飞机左右机翼内燃油箱双向供油平衡系统，包括左侧油箱通气管、左侧冲压进气管、右侧油箱通气管、右侧冲压进气管、油箱压力平衡管、集油箱、左侧油箱供油管路、右侧油箱供油管路、飞机发动机供油管