Vertical coaxial dual -rotor aircraft

The utility model relates to an aircraft field specifically is a vertical coaxial dual -rotor aircraft. Vertical coaxial dual -rotor aircraft, the aircraft includes the base, the base top is equippedwith oil tank, engine and rotating system in proper order, the rotating system through the reducing gear box with the engine is connected, the top of base still is equipped with the support, the oil tank with the engine outside is equipped with the casing, the casing with support fixed connection, being close to of support casing department is equipped with control device and fin, control device is including controlling the arm, it extends to the first direction to control the arm, the fin extends along the second direction, the first direction with the second direction is opposite direction.The utility model provides a vertical coaxial dual -rotor aircraft compact structure, the quality is light, area is little. 本实用新型涉及飞行器领域，具体为种立式共轴双旋翼飞行器。所述立式共轴双旋翼飞行器，所述飞行器包括底座，所述底座上方依次设有油箱、发动机和旋动系统；所述旋动系统经减速箱与所述发动机连接；在所述底座的上方还设