Page 399 - Wind Energy Handbook
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ROTOR POSITION WITH RESPECT TO TOWER                                   373


             just one or two degrees at the low-speed shaft. An interesting variant (Leithead and
             Rogers, 1995) is to mount the generator on flexible mounts. This system can be
             tuned to absorb energy at the blade-passing frequency through an additional mode
             of vibration of the generator casing against its mountings. This mode also affects
             the generator slip speed (the difference between rotor and casing speeds) and is
             therefore damped by the slip curve. Nevertheless, generator casing displacements
             would still need to be of the order of 10–158, which is still not easy to engineer.



             6.13    Rotor Position with Respect to Tower


             6.13.1  Upwind configuration

             The upwind configuration is the one most commonly chosen. The principal
             advantage is that the tower shadow effect is much less for the same blade–tower
             spacing, reducing both dynamic loads on the blade and rhythmic noise effects. Set
             against this is the need to take great care to avoid the risk of blade–tower strikes
             with upwind machines, requiring accurate prediction of blade deflections under
             turbulent wind loading.
               The clearance between the undeflected blade and the tower can be increased by
             tilting the low-speed shaft upwards or by increasing the rotor overhang. It is
             desirable to keep the rotor overhang small in order to minimize low-speed shaft
             and nacelle bedplate bending moments, so the low-speed shaft is normally tilted
             upwards by 58 or 68 to provide the necessary blade–tower clearance, at the cost of a
             very small reduction in power output.




             6.13.2  Downwind configuration

             The wind velocity deficit behind a wind-turbine tower is much greater than that in
             front of it, to the extent that Powles (1983) has reported a turbulent region with
             essentially no forward velocity extending up to four tower diameters downstream
             of an octagonal tower. Beyond this distance, recovery is relatively rapid, with the
             deficit reduced to about 25 percent at seven tower diameters downstream.
               In addition to the mean wind-speed velocity deficit behind the tower, vortex
             shedding results in additional wind-speed fluctuations over and above those
             already present due to turbulence. The two effects combine to present a harsh
             environment to the blades immediately behind the tower. The blades are subjected
             to a large negative impulsive load each time they pass the tower, which contributes
             significantly to blade fatigue damage, and the audible tower ‘thump’ that results is
             liable to be unwelcome. Designers usually mitigate both effects by positioning the
             rotor plane well clear of the tower, but this inevitably increases nacelle costs
             somewhat.
               An important benefit of the downwind configuration is that it allows the use of
             very flexible blades without the risk of tower strike. Such blades benefit by being
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