Page 425 - Wind Energy Handbook
P. 425

BLADES                                                                 399

               800

               700
                                                                  Rotational speed = 30 r.p.m.
              Extreme out-of-plane bending moment (KNm)  500  Extreme operational out-of-plane bending moment
               600


                                       for 40.4 m/s instantaneous wind speed
                                          and 30  skewed flow angle
               400
                                          excluding dynamic effects
                                              (dotted line)
               300

               200
                   Extreme non-operational out-of-plane bending moment
                        for 60 m/s gust and 1.5 lift coefficient
               100   (lower solid line: quasistatic bending moment,
                     upper solid: bending moment including dynamic
                              magnification)
                0
                  0     2      4      6      8      10    12     14     16     18     20
                                                 Radius (m)
             Figure 7.12  Comparison of Extreme Operational and Non-operational Out-of-plane Bend-
             ing Moment Distributions for a 40 m Diameter Stall-regulated Machine with TR Blades


             moment distribution is more highly curved than the operational one, so the former
             is more likely to govern at the root and the latter to govern outboard.
               Extreme non-operational loads tend to govern blade out-of-plane bending on
             pitch-regulated machines, as extreme operational out-of-plane bending moments
             are generally significantly less than on stall-regulated machines.


             Fatigue loading


             The importance of fatigue loading relative to extreme loading is very much a
             function of material properties. As the vast majority of blades are manufactured
             from composite materials with similar fatigue properties, discussion in this sub-
             section will be based on these.
               As set out in Sections 7.1.6 and 7.1.7, composite materials are characterized by a very
             shallow S–N curve i.e., the reciprocal index m in the relation ó / N  1=m  for constant
             amplitude, reversed loading (R ¼ 1) is typically 10 or more. As a result, fatigue
             damage can be dominated by the small number of high range stress cycles associated
             with unusual wind conditions, rather than by the routine medium range cycles.
               The other significant property of composite materials is the increase in fatigue
             damage with mean stress level, which is usually accounted for by scaling up the
             stress amplitude entered in the R ¼ 1 S–N curve formulation by the factor
             1=(1   ó=ó d ), where ó d is the design strength in compression for a compression
             mean or in tension for a tension mean. This increases the relative importance of
             stress cycles with a high mean.
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