Wind turbine blade with double airfoil profile
Double blade airfoils and related systems are disclosed. The double blade design may efficiently use a minimal amount of material yet achieve exceptional aerodynamic efficiencies well above the previously understood theoretical maximum. The disclosed designs may operate at lower wind speeds than those known in the art. Furthermore, the balance of forces generated by the disclosed designs may also reduce the stress felt by the airfoils and rotor, enhancing the longevity of the system.
1. A wind turbine comprising:
an airfoil connected to a rotor on the wind turbine, the airfoil being configured to rotate about an axis upon an impact of a wind flow on the airfoil, the airfoil comprising:
a lower blade and an upper blade, the lower blade and the upper blade being separated by a gap extending along a radial direction of the airfoil from a portion of the airfoil connected to the rotor to a tip of the airfoil;
wherein the lower blade and the upper blade have profiles with different shapes, an inner surface of the lower blade comprising a profile having both a convex-shaped portion and a concave-shaped portion along a chord direction of the lower blade, and an inner surface of the upper blade comprising a profile having both a convex portion-shaped and a concave-shaped portion along a chord direction of the upper blade; and
wherein the lower blade profile tapers from a larger cross section at the portion of the airfoil connected to the rotor to a smaller cross section at the tip of the airfoil, and wherein the upper blade profile tapers from a larger cross section at the portion of the airfoil connected to the rotor to a smaller cross section at the tip of the airfoil.
2. The wind turbine of claim 1 , wherein a size of the gap varies along a longitudinal axis of the airfoil.
3. The wind turbine of claim 1 , wherein each of the lower blade profile and the upper blade profile contains at least 5 aerodynamically distinct surfaces.
4. The wind turbine of claim 1 , wherein the inner surfaces of the lower blade and the upper blade comprise complementary inner surfaces configured to expand air along the inner surfaces between the lower blade and the upper blade.
5. The wind turbine of claim 4 , wherein the complementary inner surfaces are configured to increase pressure and decrease air speed in the space between the lower blade and the upper blade.
6. A wind turbine comprising:
an airfoil connected to a rotor on the wind turbine, the airfoil being configured to rotate about an axis upon an impact of a wind flow on the airfoil, the airfoil comprising:
a lower blade and an upper blade, the lower blade and the upper blade having inner surfaces separated by a gap extending along a radial direction of the airfoil from a portion of the airfoil connected to the rotor to a tip of the airfoil;
wherein a profile of the inner surface of the lower blade changes from a convex-shaped portion to a concave-shaped portion along a chord of the lower blade, and wherein a profile of the inner surface of the upper blade changes from a convex-shaped portion to a concave-shaped portion along a chord of the upper blade; and
wherein the profile of the lower blade tapers from a larger cross section at the portion of the airfoil connected to the rotor to a smaller cross section at the tip of the airfoil, wherein the profile of the upper blade tapers from a larger cross section at the portion of the airfoil connected to the rotor to a smaller cross section at the tip of the airfoil.
7. The wind turbine of claim 6 , wherein a size of the gap changes along a longitudinal axis of the airfoil.
8. The wind turbine of claim 6 , wherein each of the lower blade profile and the upper blade profile contains at least 5 aerodynamically distinct surfaces.
9. The wind turbine of claim 6 , wherein the lower blade and the upper blade comprise complementary inner surfaces configured to expand air along the inner surfaces between the lower blade and the upper blade.
10. The wind turbine of claim 9 , wherein the complementary inner surfaces are configured to increase pressure and decrease air speed in the space between the lower blade and the upper blade.