Page 17 - May
P. 17

METALWORKING EQUIPMENT AND TOOLS

                                       And what dynamic characteristics should the "ideal" machine have?
      Compliance,              How to estimate the amount of bearing wear and the drop in bearing
      conventional units       stiffness due to this wear?
                                       The  answer  to  such  questions  can  be  obtained  by  modeling  the
                    316/5,14   control box and calculating its dynamic characteristics. To do this, you can
        5
                               use the program SpinDyna [10-13]. The program window with geometric
                            1  parameters and the SHU model of the TNL-120AL2 machine are shown in
                               Fig. 5. In the model (Fig. 5), the stiffness data from the bearing catalogs
        4                      were used to describe the characteristics of the bearings. Radial stiffness
                               of a roller double-row radial bearing: back support - 153 daN / μm, front
                      380/3,44
                               support - 173 daN / μm. For ball thrust radial bearings: radial stiffness -
        3                      92 daN / μm and angular stiffness 4.3E + 05 daN ∙ m / μm.
                            2          Calculation using the SpinDyna program with catalog data on the
                               stiffness  of  the  bearings  gave  the  frequency  response  of  the  SHU  as

         2                     shown in Fig. 6 (curve 1). Let us consider such a machine "ideal". If,
                               in  a  double-row  radial  roller  bearing,  the  stiffness  is  reduced  to  29.5
                               daN / μm, that is, almost 6 times, and the stiffness of the thrust radial
                               bearing is not changed, then the frequency response takes a different
         1
                                                                       form  (curve  2),  which  corresponds  to
                                                                       the  experimental  frequency  response
                                                                       of the "new" machine tool. It is unlikely
         0  100        480          880            1270       1660     that  in one  year  of  operation,  a  radial
                                                         Frequency Hz
                                                                       double-row roller bearing could wear out
    Fig. 4. AFC of SHU machines TNL-120AL2 by displacement: 1 - "old"   so  that  the  stiffness  dropped  6  times.
    machine; 2 - "new" machine.                                        Obviously,  when  assembling  the  ShU,
                                                                       the required preload in this bearing was
     not provided. No claims can be made to the supplier of this machine because the warranty
     period has expired. Therefore, the management of the enterprise made a decision to repair the
     machine on its own.
            If the stiffness of the double-row radial roller bearing of the front support is taken as
     17.3 daN / μm, that is, 10 times less than the catalog value, and the ball thrust radial bearing
     is 65 daN / μm, that is, 1.4 times less than the catalog value, then we get the AFC of the SHU
     (curve 3 in Fig. 4), which are close in natural frequency to the experimental AFC of the "old"
     machine. In this case, with a high degree of probability, it can be assumed that the decrease in
     the rigidity of the front support bearings occurred as a result of their wear. Additional studies
     have shown the presence of an axial play of the spindle of the "old" machine of the order of
     0.03 mm. As a measure to increase the rigidity of the front spindle bearing, it is possible to
     recommend regrinding the ring with labyrinth seals in front of the radial roller bearing (Fig.
     3) by an amount of the order of 0.1-0.12 mm, regrinding the lantern ring in the thrust radial
     bearing by 0.03 mm.



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