A propeller-type vertical take-off and land aircraft with a torque removal and balancing function, the aircraft comprising: a body; a body support frame to support the body; at least two main rotor blades provided out of the body; a rotation rotor coupled centrally to the main rotor blades; a rotation drive axis operatively coupled to the rotation rotor; a main rotor motor operatively coupled to the rotation drive axis; and a counter-torque and balancing wheel disposed under the body support frame, wherein the counter-torque and balancing wheel, when in use, rotates in an opposite direction to a rotation of the main rotor blades, wherein the counter-torque and balancing wheel is coupled to a torque-removal motor, wherein the counter-torque and balancing wheel is configured to balance the body using a gyro effect, wherein the counter-torque and balancing wheel is housed in the body, wherein the counter-torque and balancing wheel has, in top view, a circular shape, characterized in that the counter-torque and balancing wheel is made of a metal, wherein a weight thereof is concentrated on an outer circumference, wherein the counter-torque and balancing wheel includes: a central coupler axially coupled to a rotation shaft of the torque-removal inverse motor; a connection extending around the central coupler, wherein the connection has weight-reduction holes defined therein; and a weight concentration portion extending around the connection, wherein the weight concentration portion is thicker than the connection such that a weight concentrates on the weight concentration portion. a body; a body support frame to support the body; at least two main rotor blades provided out of the body; a rotation rotor coupled centrally to the main rotor blades; a rotation drive axis operatively coupled to the rotation rotor; a main rotor motor operatively coupled to the rotation drive axis; and a counter-torque and balancing wheel disposed under the body support frame, wherein the counter-torque and balancing wheel, when in use, rotates in an opposite direction to a rotation of the main rotor blades, wherein the counter-torque and balancing wheel is coupled to a torque-removal motor, wherein the counter-torque and balancing wheel is configured to balance the body using a gyro effect, wherein the counter-torque and balancing wheel is housed in the body, wherein the counter-torque and balancing wheel has, in top view, a circular shape, characterized in that the counter-torque and balancing wheel is made of a metal, wherein a weight thereof is concentrated on an outer circumference, wherein the counter-torque and balancing wheel includes: a central coupler axially coupled to a rotation shaft of the torque-removal inverse motor; a connection extending around the central coupler, wherein the connection has weight-reduction holes defined therein; and a weight concentration portion extending around the connection, wherein the weight concentration portion is thicker than the connection such that a weight concentrates on the weight concentration portion. a central coupler axially coupled to a rotation shaft of the torque-removal inverse motor; a connection extending around the central coupler, wherein the connection has weight-reduction holes defined therein; and a weight concentration portion extending around the connection, wherein the weight concentration portion is thicker than the connection such that a weight concentrates on the weight concentration portion.