Page 199 - Wind Energy Handbook
P. 199

4



             Wind-turbine Performance











             4.1   The Performance Curves

             The performance of a wind turbine can be characterized by the manner in which
             the three main indicators—power, torque and thrust—vary with wind speed. The
             power determines the amount of energy captured by the rotor, the torque
             developed determines the size of the gear box and must be matched by whatever
             generator is being driven by the rotor. The rotor thrust has great influence on the
             structural design of the tower. It is usually convenient to express the perform-
             ance by means of non-dimensional, characteristic performance curves from which
             the actual performance can be determined regardless of how the turbine is
             operated, e.g., at constant rotational speed or some regime of variable rotor
             speed. Assuming that the aerodynamic performance of the rotor blades does not
             deteriorate the non-dimensional aerodynamic performance of the rotor will
             depend upon the tip speed ratio and, if appropriate, the pitch setting of the
             blades. It is usual, therefore, to display the power, torque and thrust coefficients
             as functions of tip speed ratio.





             4.1.1  The C P – º performance curve


             The theory described in Chapter 3 gives the wind turbine designer a means of
             examining how the power developed by a turbine is governed by the various
             design parameters. The usual method of presenting power performance is the non-
             dimensional C P – º curve and the curve for a typical, modern, three-blade turbine
             is shown in Figure 4.1.
               The first point to notice is that the maximum value of C P is only 0.47, achieved at
             a tip speed ratio of 7, which is much less than the Betz limit. The discrepancy is
             caused, in this case, by drag and tip losses but the stall also reduces the C P at low
             values of the tip speed ratio (Figure 4.2).
               Even with no losses included in the analysis the Betz limit is not reached because
             the blade design is not perfect.
   194   195   196   197   198   199   200   201   202   203   204