Page 368 - Wind Energy Handbook
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342                        CONCEPTUAL DESIGN OF HORIZONTAL-AXIS TURBINES


            600
                    Pitch-regulated machine with
                    TR blades rotating at 33 r.p.m.
            500        (Blade pitch below rated
                   increased 1.4 degrees compared
                     with stall-regulated machine)  Stall-regulated machine with TR
                                              blades rotating at 30 r.p.m.
            400
           Power (kW)  300




                                                  Rotor diameter = 40 m
            200


            100


              0
               0          5          10          15         20          25         30
                                             Wind speed (m/s)
          Figure 6.4 Comparison of Power Curves for 500 kW Stall-regulated and Pitch-regulated
          Machines with the Same Planform and Twist Distribution
          to increase with rotational speed, but no account is taken of the increased loads on
          these components for a fixed-hub, two-bladed machine. Tower design is assumed
          to be governed by fatigue in the first instance, so tower weight is taken as
          proportional to rotational speed. The cyclic thrust loads on the rotor due to
          turbulence are virtually the same for two- and three-bladed machines rotating at
          the same speeds if the blade planforms are the same, so the tower cost element at
          the baseline rotational speed is left unchanged.
            The weights of the gearbox and brake are taken to be proportional to the rated
          torque, P R =Ù, while those of the generator and of the cables and equipment forming
          the grid connection are taken as proportional to rated power, P R . The foundation
          cost element is reduced by a quarter for the two-bladed machine in recognition of
          the reduced extreme tower base overturning moment.
            The various components are classified into different categories according to the
          way in which their weights vary with rotational speed and rated power in Table 6.4.
          Also tabulated are the two-bladed machine component costs as a percentage of the
          total for the baseline three-bladed machine, together with the sum for each category.
            Adopting Equation (6.1) with ì ¼ 0:9 once more for the relationship between the
          cost of a component and its mass, the following expression is obtained for machine
          cost as a function of rotational speed and rated power:

          C T ¼ C TB (0:114 þ 0:514f0:1 þ 0:9(Ù=Ù B )gþ 0:142f0:1 þ 0:9(P R =P RB )(Ù B =Ù)g
               þ 0:158f0:1 þ 0:9(P R =P RB )g)                                 (6:11)

             ¼ C TB 0:1954 þ 0:4626(Ù=Ù B ) þ 0:1278(P R =P RB )(Ù B =Ù RB ) þ 0:1422(P R =P RB ))ð
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