Winglet for a wind turbine rotor blade

1. A winglet for a rotor blade, comprising:

a winglet body extending at least partially between a winglet origin and a blade tip and including a plurality of radial locations between the winglet origin and the blade tip, the winglet body defining a chord at the blade tip ranging from about 0.0% to about 0.5% of the span of the rotor blade and a chord at the winglet origin ranging from about 1.2% to about 2.6% of the span of the rotor blade, the winglet body defining a twist angle at each of the plurality of radial locations generally in accordance with the values for twist angle shown in TABLE 1,

wherein each of the values for twist angle shown in TABLE 1 may be varied +/−3.0 degrees.

2. The winglet of claim 1 , wherein the winglet body further defines a cant angle, the cant angle at the blade tip ranging from about 60 degrees to about 130 degrees.

3. The winglet of claim 1 , wherein the winglet body further defines a pre-bend, the pre-bend defined between the winglet origin and the blade tip ranging from about 1,5% to about 4.5% of the span of the rotor blade.

4. The winglet of claim 1 , wherein the winglet body further defines a spanwise radius, the spanwise radius defined between the winglet origin and the blade tip ranging from about 2.4% to about 4% of the span of the rotor blade.

5. The winglet of claim 1 , wherein the winglet further defines a sweep, the sweep defined between the winglet origin and the blade tip ranging from about 0.5% to about 4.0% of a span of the rotor blade.

6. A winglet for a rotor blade, comprising:

a winglet body, the winglet body defining cross-sectional profiles at a plurality of radial locations along the winglet body generally in accordance with the values shown in TABLE 1, the cross-sectional profiles being joined so as to define a nominal shape of the winglet body,

wherein the nominal shape lies in an envelope within +/−10% of each length value provided in TABLE 1, within +/−20 degrees of each cant angle value provided in TABLE 1 and within +/−3 degrees of each twist angle value provided in TABLE 1.

7. The winglet of claim 6 , wherein the nominal shape lies in an envelope within +/−5% of each length value provided in TABLE 1, within +/−20 degrees of each cant angle value provided in TABLE 1 and within +/−0,5 degrees of each twist angle value provided in TABLE 1.

8. A winglet for a rotor blade, comprising:

a winglet body, the winglet body defining cross-sectional profiles at a plurality of radial locations along the winglet body generally in accordance with the length values shown in TABLE 1, the cross-sectional profiles being joined so as to define a nominal shape of the winglet body,

wherein the nominal shape is scaled up or scaled down as a function of at least one constant.

9. The winglet of claim 8 , wherein the at least one constant corresponds to a span of the rotor blade.