Page 405 - Wind Energy Handbook
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BLADES                                                                 379


             7.1.3  Practical modifications to optimum design

             The result of the optimization described in the previous section is typically a blade
             geometry in which both blade chord and blade twist vary approximately inversely
             with radius, as illustrated in Figure 3.19. However, because the inboard section of
             the blade makes only a small contribution to total power output (Figure 3.30), the
             aerofoil section is generally not continued inboard of about 15 percent radius in
             practice, and the chord at this radius is substantially reduced, to perhaps half the
             theoretical optimum. It is then often found expedient to taper the chord uniformly
             over the active length of the blade, with the tip chord and chord taper set so that the
             chord distribution approximates closely to the optimum over the outboard half of
             the blade (Figure 3.20).
               The blade root area is normally circular in cross section in order to match up with
             the pitch bearing in the case of pitchable blades, or to allow pitch angle adjustment at
             the bolted flange (to compensate for non-standard air density) in the case of stall-
             regulated blades. The transition from the root section to the aerofoil section outboard
             of 15 percent radius should be a smooth one for structural reasons, with the result that
             the latter section will have a high thickness to chord ratio of up to about 50 percent.



             7.1.4  Form of blade structure

             A hollow shell corresponding to the defined blade envelope clearly provides a
             simple, efficient structure to resist flexural and torsional loads and some blade
             manufacturers adopt this form of construction (see Figure 7.1). However, in the case
             of small and medium size machines, where the out-of-plane loads dominate, there
             is greater benefit in concentrating skin material in the forward half of the blade,
             where the blade thickness is a maximum, so that it acts more efficiently in resisting
             out-of-plane bending moments (see Figures 7.2 and 7.3). The weakened areas of the













                                          Glass/Epoxy
                                           25mm Wood veneers
                                          Epoxy glue
                                          Aluminium screen for lightening protection
                                        Glass/Epoxy             (unusual)
                                      Polyurethane point
             Figure 7.1  Wood/Epoxy Blade Construction Utilizing Full Blade Shell (Reproduced from
             Corbet (1991) by permission of the DT1 Renewable Energy R&D Programme)
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