The invention relates to a multi-
propeller heating and balancing method of a
propeller-driven aircraft. The method comprises the following steps of: forming
propeller heating elements on every three engines into a group and heating propellers on the engines respectively according to an sequence of 1, 2, 3; 2, 3, 4; 1, 3, 4 and 1, 2, 4, wherein the heating
cycling time is controlled by a propeller heating balance controller, when
atmosphere temperature is +5 to -12 DEG C, the
heating time is 39s, and the power-down time is 80s, and when the
atmosphere temperature is -12 to -55 DEG C, the
heating time is 84s, and the power-down time is 92s so as to guarantee the propellers and rectifying covers thereof not to ice; when the aircraft enters an
icing area, switching on a propeller heating switch on a control board on the top of a driver so that an indication
green light is lightened when the propeller on the control board on the top of the driver is normally heated, and heating the propellers on the engines by a propeller heating controller according to received
atmosphere temperature so as to achieve the deicing effect.