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0593_C15_fm  Page 517  Tuesday, May 7, 2002  7:05 AM





                       Balancing                                                                   517



                                           B                                           B
                                     n  2           Ω                       a  2   n  2        Ω
                                                                                    a  1
                                      G                                          G
                                                                          n  3
                                                        n  1                   a                   n  1
                                  n  3                                          3
                       FIGURE 15.4.1                              FIGURE 15.4.2
                       An arbitrarily shaped body rotating about its first  An arbitrarily shaped body rotating about a
                       principal axis of inertia.                 non-principal axis.
                                                                            *
                        If the inertia forces on B are represented by a single force F  passing through G, together
                                                 *
                                                               *
                       with a couple with torque T , then F  and T  may be expressed as (see Eqs. (8.6.5) and
                                                        *
                       (8.6.6)):
                                                        F* =−m a = 0                           (15.4.1)
                                                                G
                       and

                                                  T =− ⋅Ω  n − Ω n × ⋅ ( Ω n )
                                                          ˙
                                                                    I
                                                    *
                                                       I
                                                            1    1       1
                                                                                               (15.4.2)
                                                                 ⋅
                                                     =− Ω  2 n ×( I n )
                                                      0
                                                             1     1
                       where m is the mass of B and I is the central inertia dyadic, which may be expressed as:
                                                  I = I  n n + I  n n + I  n n                 (15.4.3)
                                                      11 1 1  22  2  2  33  3  3
                                                                   *
                        By substituting from Eq. (15.4.3) into (15.4.2), T  becomes:
                                                     T =−Ω  2 n × I  n = 0                     (15.4.4)
                                                       *
                                                              1  11 1
                       Thus, from Eqs. (15.4.1) and (15.4.4), we see that B, while rotating about its first principal
                       axis, is both statically and dynamically balanced.
                        Next, suppose that the same body B is rotating at constant speed Ω about an axis other
                       than a principal axis. Specifically, suppose that  n ,  n , and  n  are only approximately
                                                                    1
                                                                       2
                                                                               3
                       parallel to the central principal axes and that instead  a ,  a , and  a  are parallel to the
                                                                             2
                                                                          1
                                                                                    3
                       principal axes, as depicted in Figure 15.4.2. As before, let the mass center G of B lie on the
                       axis of rotation.
                        If the inertia forces on B are represented by a single force F  passing through G together
                                                                            *
                                                              *
                                                       *
                                                *
                       with a couple with torque T , then F  and T  are (see Eqs. (15.4.1) and (15.4.2)):
                                                                         ⋅
                                                 *
                                                             *
                                                F = 0 and   T = −Ω 2 n ×( I n )                (15.4.5)
                                                                     1     1
                       Because n , n , and n  are no longer parallel to the central principal inertia axes, the inertia
                                         3
                               1
                                  2
                       dyadic I no longer has the simple form of Eq. (15.4.3). Instead, I will have the general form:
                                                 I = I  n n + I  n n + I  n n
                                                     11 1 1  12  1  2  13  1  3
                                                    + I  nn + I  nn + I  nn                    (15.4.6)
                                                      21  2  1  22  2  2  23  2  3
                                                    + I  nn + I  nn + I  nn
                                                      31  3  1  32  3  2  33  3  3
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