Page 423 - Wind Energy Handbook
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BLADES                                                                 397


             variation of flapwise bending moment with short-term mean wind speed at inboard
             blade cross sections are essentially similar to those in Figure 7.10, because moments
             are dominated by loadings on the outboards portion of the blade.
               To the extent that the pitch control system can keep pace with the wind speed
             transients, the curves in Figure 7.10 can be used to provide an approximate
             indication of the extreme bending moments arising from some of the IEC 61400-1
             deterministic load cases. Leaving aside the grid-loss case (where the outcome is
             largely determined by rotor inertia and emergency pitching rate), it is seen that the
             extreme moments are only about one half of the maximum value for the stall-
             regulated machine.
               The spectrum of the longitudinal wind speed fluctuations will contain significant
             energy at frequencies above the level at which the pitch control system can respond,
             and these have to be considered in the analysis of the ‘Normal turbulence model’
             load case. Figure 7.11 illustrates the perturbations in 12 m radius flapwise bending
             moment for the above machine, as a result of such high frequency wind speed
             fluctuations, with respect to a sharp rise above rated wind speed (12 m/s) and
             sharp falls below steady winds of 24, 28 and 32 m/s. In the first case considered, the
             yaw angle is  208 and the azimuth 08, as this configuration yields the largest
             positive bending moment at rated wind speed. In the second case, the yaw angle is
              408, which exceeds the maximum value predicted over the design life, and
             provides an upper bound on the largest negative moment at short-term mean wind
             speeds around the cut-out value.
               It is apparent from Figure 7.11 that rapid wind speed increases above rated wind
             speed will produce a significant increase in bending moment, but rapid reductions
             in wind speed below, say, a 24 m/s steady value will not, as in this case the blade
             goes into negative stall. Over the machine lifetime, the maximum increase in wind

                 100
                  80
                                                                Rotational speed = 33 r.p.m.
                                                             Long curves show variation of bending
                12 m radius flapwise bending moment (kNm)  -20 0  0  5   0  azimuth  15   0  azimuth 20  25 moment with rapid wind-speed fluctuations 40
                  60
                                                            moment with short-term mean wind speed;
                                                             short curves show variation of bending
                  40
                                                                from short-term mean value
                                                20  yaw,
                  20
                                    40  yaw,
                                                                           35
                                                                   30
                                   10
                 -40

                 -60

                 -80
                                               Wind speed (m/s)
             Figure 7.11  Effect of Rapid Wind-Speed Fluctuations on 12 m Radius Flapwise Bending
             Moment for an Example 40 m Diameter Pitch-regulated Machine with TR Blades
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