Patent ID: 7445536

Claim:
A micro aerial vehicle comprising: several blades in airfoil shape that are placed in calculated angle and space; hubs that connect the blades with a body of a vehicle; a rotor which gives lifting force with its spin; a spin-able axle having a vertical hem, the vertical hem being bound to the hubs; a rotor drive disposed to spin the rotor; a vehicle body that is placed right under the rotor in order to fly from lifting force that is obtained by revolutions of the rotor; and fixed-wings that are placed in certain angle and space around the outside of the vehicle body in order to reduce a reaction torque, which affects the body to turn in a direction opposite to a rotation direction of the rotor, from the rotor's movement; further comprising: a counterbalancing-reaction-torque-system on the fixed-wings that cancels the reaction torque given to the body by air flow, caused by a rotor's movement, coming down through the blades; wherein the above fixed-wings are designed to be bent in order to control angle and surfaces where the above air flow is contacted.