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ROOF BEAM ANALYSIS FOR LARGE VERTICAL DEFLECTION

                                        potential for compressive failure of the roof beam should be based on the minimum
                                        value for   c for the transversely isotropic rock unit.
                                          The possibility of shear failure of the roof beam by slip at the abutments can be
                                        assessed directly from the calculated beam loads. Referring to Figure 8.7b, the lateral
                                        thrust, T , at the abutment must mobilise a frictional resistance to slip sufficient to
                                        provide the abutment shear force, V . The maximum shear force that can be mobilised
                                        is

                                                                           1
                                                               F = T tan  =  f c nt tan
                                                                           2
                                        and the abutment shear force is given by
                                                                          1
                                                                     V =   st
                                                                          2
                                        The factor of safety against abutment shear failure is therefore defined by
                                                                          f c n
                                                                  FoS slip =  tan                     (8.12)
                                                                           s
                                          To establish an engineering estimate for the yield threshold of the buckling limit, a
                                        relation between the midspan deflection,  , and the beam thickness, t, was proposed.
                                        In various numerical studies, it was found that ultimate failure corresponded to a
                                        displacement equivalent to approximately 0.25 t. The onset of non-linear behaviour
                                        wasobservedtooccuratadeflectionequivalenttoabout0.1 t.Thatvaluewasproposed
                                        as an allowable yield limit in roof design.



                                        8.5 Roof beam analysis for large vertical deflection

                                        The preceding analysis was based on the implicit assumption that the mechanics of
                                        a voussoir beam were controlled by the central vertical crack and involved small
                                        vertical deflections of the roof. The problem could then be solved from simple statics
                                        using the free body diagram of Figure 8.7. In a more exhaustive analysis, Sofianos
                                        (1996) allowed for the possibility of large vertical deflections of the roof beam. He
                                        showed that the assumption by Evans of n = 0.5 was inadequate, and that the iterative
                                        method proposed by Brady and Brown (1985) was appropriate for small defections
                                        only. Starting from the free body diagram of Figure 8.7, and using a slightly different
                                        notation with   xx in place of f c , the moment equilibrium equation is

                                                                                1
                                                                      2
                                                                   1
                                                             M A =  ts = M R =   xx ntz               (8.13)
                                                                   8            2
                                        or
                                                                          1  s 2
                                                                      xx =                            (8.14)
                                                                          4 nz
                                        The problem is to find the equilibrium values of   xx , n and z. Sofianos proposed that
                                        to provide an efficient and quick analysis, the value of n could best be determined
                                        by independent numerical methods. From the finite element studies of Wright (1972)
                                        and the UDEC analysis of Sofianos et al. (1995), a graphical relation was established
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