Page 207 - Wind Energy Handbook
P. 207

CONSTANT ROTATIONAL SPEED OPERATION                                    181


                          120


                          100
                                                           +4
                                                      +2
                           80
                        Electrical power (kW)  60  -2   0





                           40


                           20               -4


                            0
                             5                    10                    15                     20                   25
                                             Wind speed (m/s)
                         Figure 4.9  Effect on Extracted Power of Blade Pitch Set Angle




             starting torque can be generated as a rotor begins to turn. A 908 pitch angle is
             usually used when shutting down because this minimises the rotor idling speed at
             which the parking brake is applied. At 908 of positive pitch the blade is said to be
             ‘feathered’. The principal disadvantages of pitch control are reliability and cost.
             Power regulation can be achieved either by pitching to promote stalling or pitching
             to feather which reduces the lift force on the blades by reducing the angle of attack.



             4.2.6  Pitching to stall

             Figure 4.9 shows the power curves for a turbine rated at 60 kW, which is achieved
             at 12 m/s. At wind speeds below the rated level the blade pitch angle is kept at 08.
             As rated power is reached only a small negative pitch angle, initially of about 28,is
             necessary to promote stalling and so to limit the power to the rated level. As the
             wind speed increases small adjustments in both the positive and negative directions
             are all that are needed to maintain constant power. The small sizes of the pitch
             angle adjustments make pitching to stall very attractive to designers but the blades
             have the same damping and fatigue problems as fixed pitch turbines.



             4.2.7  Pitching to feather

             By increasing the pitch angle as rated power is reached the angle of attack can be
             reduced. A reduced angle of attack will reduce the lift force and the torque. The
   202   203   204   205   206   207   208   209   210   211   212