The invention discloses an automatic parachute fall off mechanism of an unmanned aerial vehicle. The automatic parachute fall off mechanism is composed of fall off joint connectors, a rotary electromagnet, a rotary guide rail, a spring, a parachute belt, a parachute belt shaft and a cotter pin. The automatic fall off mechanism is connected to the parachute belt through an upper fall off joint connector and a lower fall off joint connector, and the parachute belt is connected with the unmanned aerial vehicle. When the unmanned aerial vehicle parachutes and lands, a control circuit controls therotary electromagnet to drive the rotary guide rail to rotate, so that the ball falls into an arc-shaped groove of the guide rail to fall off, the constraint of the ball on the fall-off joint upper connector and the fall-off joint lower connector is relieved; after the ball falls off, the spring release force is increased to separate the fall-off joint upper connector from the fall-off joint lower connector, and parachute throwing is completed. The rotary electromagnet and the rotary guide rail are designed, the rotary electromagnet is used for driving the rotary guide rail to rotate to achieve ball falling, and an unlocking structure and the unlocking process are simplified. The automatic parachute fall off mechanism is simple in structure, convenient to install and capable of safely andreliably achieving separation of the parachute and the unmanned aerial vehicle.