The invention discloses an optimization method for impeller blades of a low-pressure axial flow fan. Low-pressure axial flow fans are widely used, but there are problems of low total pressure, large air volume, and low impeller efficiency. In the present invention, a blade of the impeller model to be optimized is divided into n sections along the radial direction of the impeller, and the chord length bi, the outlet geometric angle β2A(i) and the inlet airflow angle β1(i) of the n sections are obtained. Draw a sketch, the sketch includes the first line segment, the second line segment, the third line segment, the fourth line segment, the fifth line segment, the sixth line segment, the first arc, the second arc, the seventh line segment and the eighth line segment. The first arc and the second arc form a new type of line. According to the new line, n new sections are obtained, and the optimized impeller model is obtained according to the n new sections. The present invention can optimize the performance of the low-pressure axial flow fan only by knowing the chord length of the blade section to be optimized, the inlet flow angle and the outlet geometric angle, greatly reducing the design time and cost.