Resumen
The present invention relates to a peripheral support wind turbine intended to harness non-linear airspeed profiles, wherein the turbine comprises a rotor with blades having constant chord and increasing thickness; the blades are fastened by means of a peripheral rotary ring, wherein the twist angle of the blade segment that is attached to the peripheral rotary ring is greater than that of the other blade segments; wherein the chord length of the wing profiles is constant along the extension of the blades; wherein the thickness of the wing profiles increases along the extension of the blades, with the thinner wing profiles being located closer to the centre; and wherein the turbine has an automatic protection folding system intended to radially fold the blades so that the turbine enters aerodynamic loss.