Page 310 - Wind Energy Handbook
P. 310

284                        DESIGN LOADS FOR HORIZONTAL-AXIS WIND TURBINES


             180
             160
                                         Out-of-plane
             140

             120
             (kNm)  100

             80
             60
             40                                 In-plane

             20
              0

             -20
                0         60         120        180        240        300         360
                                      Rotor azimuth angle (degrees)
                        Figure 5.33  Blade Root Bending Moment in Steady Wind




            The out-of-plane moment is always positive, the mean value being dominated by
          the aerodynamic thrust on the blade. There is a systematic variation with azimuth
          resulting from the wind shear, giving a lower load at 1808 azimuth (bottom dead
          centre) than at 08. A sharp dip at 1808 is also visible, and this is the effect of the
          tower shadow (the reduction in wind speed in the vicinity of the tower). The blade
          out-of-plane vibrational dynamics contribute a significant higher-frequency varia-
          tion.
            In turbulent wind, the loads take on a much more random appearance, as shown
          in Figure 5.34. The out-of-plane load in particular is varying with wind speed and,
          as this is a pitch-controlled machine, with pitch angle. The in-plane load is more
          regular, as it is always dominated by the reversing gravity load.
            Spectral analysis provides a useful means of understanding these variations.
          Figure 5.35 shows auto-spectra of the blade root out-of-plane bending moment and
          the hub thrust force. The out-of-plane bending moment is dominated by peaks at all
          multiples of the rotational frequency of 0.8 Hz. These are caused mainly by the
          rotational sampling of turbulence by the blade as it sweeps around, repeatedly
          passing through turbulent eddies. Wind shear and tower shadow also contribute to
          these peaks. A small peak due to the first out-of-plane mode of vibration at about
          3.7 Hz is just visible. There is also a significant effect of the first tower fore–aft
          mode of vibration at about 0.4 Hz.
            This tower effect is also visible in the spectrum of the hub thrust force. However,
          this force is the sum of the shear forces at the roots of the three blades. These forces
          are 1208 out of phase with each other, with the result that the peak at the rotational
          frequency (1P) is eliminated, as are the peaks at multiples of this frequency such as
   305   306   307   308   309   310   311   312   313   314   315