The invention discloses an engine combined-cooling system on a small single-rotor-wing unmanned helicopter. The engine combined-cooling system comprises a cylinder A, a water cooled jacket A, a cylinder B, a water cooled jacket B, a water cooling evaporator, a water storage tank and a water pump. When a double-cylinder-oppositely-arranged type air cooled engine works, cooling water enters an annular water cavity A through a water inlet connector of the water cooled jacket A, absorbs heat of the cylinder A and is then drained out through a water outlet connector of the water cooled jacket A; the drained cooling water enters an annular water cavity B through a pipe and a water inlet connector of the water cooled jacket B, absorbs heat of the cylinder B, is then drained out through a water outlet connector of the water cooled jacket B, enters the water cooling evaporator through a pipe and is forcedly cooled through wind generated by a propeller and wind generated by flight; and the cooled water then enters the annular water cavity A through a hose, the water storage tank, a hose, the water pump, a hose and the water inlet connector of the water cooled jacket A in sequence and circulates according to the above path.