Page 422 - Wind Energy Handbook
P. 422

396                                                     COMPONENT DESIGN


          same time it should be more accurate because of the avoidance of uncertainties
          associated with stall. It is instructive to focus comparisons on the blade bending
          moment about the weak axis at 60 percent radius once again. This time it is referred
          to as the flapwise bending moment rather than the out-of-plane (of rotation)
          moment because of blade pitching.
            Figure 7.10 presents the variation of 60 percent radius flapwise bending moment
          with short-term mean wind speed at several yaw angles for a 500 kW, 40 m
          diameter pitch-regulated machine fitted with TR blades and rotating at 33 r.p.m.
          The rated speed, V R , is 12 m/s and other parameters, including the wind shear
          exponent, are the same as in the stall-regulated example above. The figure only
          shows the bending moments resulting from slow variations in wind speed, i.e.,
          those which can be followed by the pitch control system, so moments arising from
          faster wind speed fluctuations must be added to obtain the total. The curves are
          very different in shape from those obtained for the stall-regulated machine. The
          12 m radius flapwise bending moment reaches a peak at rated wind speed, and
          then drops off sharply, becoming negative by about 24 m/s in the case of zero yaw
          and zero wind shear. This is because the blade has pitched to such an extent that
          the outboard section of the blade is providing a braking torque to counteract the
          increased torque from the inboard section. At high wind speeds and yaw angles,
          large negative bending moments are developed, which approach the magnitude of
          the peak positive moment at rated speed. Note that the bending moment reduces
          with negative yaw angle at zero azimuth, instead of increasing as it does for stall-
          regulated operation. This is because blade pitching renders angle of attack, which is
          reduced under these conditions, more critical than relative velocity. Plots of the

               80

               60                                    Shear exponent = 0.2
                                                   Rotational speed = 33 r.p.m.
              12 m radius flapwise bending moment (kNm)  -20 0   20  yaw    20  yaw
                                                  Full-line curves are for 0  azimuth
                                                 Dashed lines are for 180  azimuth
               40
               20




                                                                           0  yaw,
                                                                             0
                                                             0  yaw,
                                                                            azimuth
                                     40  yaw,
              -40
              -60                  180  azimuth    20 yaw   180  azimuth
                                                     40  yaw,              20  yaw
                                                    0  azimuth
              -80
                 0      5     10     15     20      25     30     35     40     45
                                            Wind speed (m/s)
          Figure 7.10 Variation of 12 m Radius Flapwise Bending Moment with Short-term Mean
          Wind Speed at Various Yaw Angles for an Example 40 m Diameter Pitch-regulated Machine
          with TR Blades
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