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352                        CONCEPTUAL DESIGN OF HORIZONTAL-AXIS TURBINES


             2000
                                                                          15


                                                                    12.5
             1500
                                                              10
            Power output  (kW)  1000                    7.5                   5   2.5









              500                                                             0
                                                                            500 kW

                                                                     25
                                                  17.5
                                                      20   22.5
               0
                 0          5         10         15         20         25         30
                                            Wind speed (m/s)
          Figure 6.7 Power Curves for Different Pitch Angles: 40 m Diameter Rotor Rotating at 33
          r.p.m.

            A variety of pitch actuation systems have been adopted (see also Section 8.5).
          They are divided between those in which each blade has its own actuator and those
          in which a single actuator pitches all the blades. The former arrangement has the
          advantage that it provides two or three independent aerodynamic braking systems
          to control overspeed, and the disadvantage that it requires very precise control of
          pitch on each blade in order to avoid unacceptable pitch angle differences during
          normal operation. An advantage of the latter arrangement is that the pitch actuator,
          e.g. a hydraulic cylinder, can be located in the nacelle, producing fore-aft motion of
          the pitch linkages in the hub by means of a rod passing down the middle of a
          hollow low-speed shaft (see Figure 6.8). Alternatively, the axial position of the rod
          can be controlled by means of a ball-screw and ball-nut arrangement, in which the
          ball-nut is driven by a servomotor. Normally the ball-nut is driven at the same
          speed as the rotor, but when a change of pitch is required the ball-nut rotational
          speed is altered temporarily. This system is arranged to be fail-safe, so that should
          the servomotor or its control system fail, the servomotor is braked automatically
          and the ball-nut drives the blade pitch to feather.
            Where hydraulic cylinders are used to pitch blades individually, they are
          mounted within the hub and each piston rod is usually connected directly to an
          attachment on the blade bearing (see Figure 6.9). The attachment point follows a
          circular path as the blade pitches, so the cylinder has to be allowed to pivot. The
          alternative solution of employing an electric motor to drive a pinion engaging with
          teeth on the inside of the blade bearing consequently appears rather neater (see
          Figure 6.10). Both systems require a hollow shaft to accommodate either hydraulic
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