Page 369 - Wind Energy Handbook
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NUMBER OF BLADES                                                       343


             Table 6.4  Contribution of Different Components to the Cost of a Two-bladed Machine
             (Expressed as Percentages of Three-bladed Baseline Machine Cost) and Classified According
             to the Relationship Assumed Between the Component Mass and Rotational Speed/rated
             Torque/Rated Power
             Components for which Components for which Components for which Components for which
             the weight/cost is  the weight varies as  the weight varies as  the weight varies as
             independent of rated  rotational speed, Ù  rated torque, P R =Ù  rated power, P R
             power or rotational
             speed

             Component  Cost   Component   Cost   Component  Cost    Component  Cost
             Foundation  3.1%  Blades      12.2%  Gearbox    12.5%   Generator   7.5%
             Controller  4.2%  Hub          2.5%  Brake system 1.7%  Grid        8.3%
                                                                     connection
             Assembly    2.1%  Main shaft   4.2%
             Transport   2.0%  Nacelle     10.8%
                               Yaw system   4.2%
                               Tower       17.5%

             Total      11.4%  Total       51.4%  Total      14.2%   Total      15.8%



             Here, P RB and Ù B are the baseline values of rated power and rotational speed,
             500 kW and 30 r.p.m. respectively. The two design options can now be examined.


             (a)  Planform and rotational speed unchanged from baseline
                 The maximum output power drops by almost exactly one third due to the
                 reduction in the number of blades, but the reduction in energy yield is less
                 severe at 19 percent. This is because, although the coefficient of performance
                 (C P ) for the two-bladed machine is very nearly two thirds that of the three-
                 bladed machine at the low tip speed ratio (62:8=16 ¼ 3:9) corresponding to
                 peak power output, the maximum value of C P is almost as large as that of the
                 three-bladed machine (see Figure 6.5, which compares the C P   º curves).
                   The reduced number of blades and reduced rated power lead to an overall
                 cost reduction of 16 percent (made up of 6 percent on the blades, 1 percent on
                 the foundation and 9 percent on the gearbox, brake, generator and grid
                 connection), leading to an increase in energy cost of 4 percent compared with
                 the baseline three-bladed machine.
             (b) Chord distribution and diameter unchanged, but rotational speed increased by 18
                 percent and blade pitch adjusted to give 500 kW power rating
                 In this two-bladed design variant, the rotational speed and blade pitch are
                 chosen to maximize energy yield while restricting the rated power to that of
                 the baseline design. The resultant annual energy yield is 4 percent less than for
                 the three-bladed machine.
                   The option of increasing rotational speed is an attractive one as far as the
                 drive train is concerned because, for a given machine rating, it results in a
                 reduction in drive train torque and hence in gearbox cost. In this case, the
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