Page 406 - Wind Energy Handbook
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380                                                     COMPONENT DESIGN










                                                     Filler
                                Glass/Epoxy web
                                  Glass/Epoxy     Glass/Epoxy
                                   4mm Wood veneers  Styrofoam

                                   Epoxy glue     Glass/Epoxy
                                 Glass/Epoxy             Gel coat
                           Gel coat
          Figure 7.2 Wood/Epoxy Blade Construction Utilizing Forward Half of Blade Shell (Repro-
          duced from Corbet (1991) by permission of the DT1 Renewable Energy R&D Programme)


                                                       CSM   Continuous Strand Mat





                                                                       CSM skins
                                                                   CSM
                                                   Filler
                Moulded GRP shear webs                                PVC foam
                                    UD Glass Fibre/polyester
                                                                     CSM
                                                                 Gel Coat
          Figure 7.3 Glass-fibre Blade Construction Using Blade Skins in Forward Portion of Blade
          Cross Section and Linking Shear Webs. (Reproduced from Corbet (1991), by permission of
          the DT1 Renewable Energy, R&D Programme)


          shell towards the trailing edge are then typically stiffened by means of sandwich
          construction utilizing a PVC foam filling.
            The hollow shell structure defined by the aerofoil section is not very efficient at re-
          sisting out-of-plane shear loads, so these are catered for by the inclusion of one or more
          shear webs oriented perpendicular to the blade chord. If the load-bearing structure is
          limited to a compact closed hollow section spar, consisting of two shear webs and the
          skin sections between them (see Figure 7.4), then a GFRP blade lends itself to semi-
          automatic lay-up on a rotatingmandrel which canbe withdrawn after curing.


          7.1.5 Blade materials and properties

          The ideal material for blade construction will combine the necessary structural
          properties – namely high strength to weight ratio, fatigue life and stiffness – with
          low cost and the ability to be formed into the desired aerofoil shape.
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