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                                            Design at Resonance of Mechanical Microsystems

                                                    Design at Resonance of Mechanical Microsystems  5
                                  m
                                           x


                              c         k



                              Figure 1.6 Single-degree-of-freedom mass-dashpot system.
                                                        .                    íȟȦt
                                                               0 /
                                     x(t) = x cos(Ȧ t) + (x + ȟȦx ) Ȧ sin(Ȧ t) e          (1.8)
                                            0
                                                                         d
                                                        0
                                                                   d
                                                  d
                              where
                                                              2
                                                    Ȧ = 1 íȟ Ȧ                            (1.9)
                                                     d           r
                              is the damped frequency of the system and the damping ratio ȟ is de-
                              fined as
                                            ȟ = c c = c (2 mk) = c (2mȦ )                (1.10)
                                                       /
                                                                  /
                                                / c
                                                                        r
                              by means of the critical damping factor c c . The solution to Eq. (1.8) de-
                              scribes the natural response of the vibratory system in the absence of
                              the external forcing.
                                Depending on  whether the critical damping factor is less than,
                              equal  to, or larger  than  1,  the  vibrations are called,  respectively,
                              underdamped, critically damped, or overdamped.


                              1.2.2  Forced response — the resonance
                              When a force defined as
                                                    f (t) = Fsin(Ȧt)                     (1.11)

                              acts on the mass shown in Fig. 1.6, then Eq. (1.3) changes to
                                                    ..  .
                                                  mx + cx + kx = f (t)                   (1.12)

                              The general solution of Eq. (1.12) is the sum of a complementary solu-
                              tion (which describes the system’s vibration at the natural frequency)
                              and a particular solution (which is vibration-generated at the driving
                              frequency). The latter part of the solution is also called the steady-state
                              solution and is generally analyzed in the frequency domain by studying
                              its amplitude and phase angle.







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