Page 52 - Mechanical design of microresonators _ modeling and applications
P. 52

0-07-145538-8_CH02_51_08/30/05



                                    Basic Members: Lumped- and Distributed-Parameter Modeling and Design

                                 Basic Members: Lumped- and Distributed-Parameter Modeling and Design  51
                              fractions are determined in terms of  distribution  functions  that are
                              identical to the one expressed in Eq. (2.8).
                                The bending presents the characteristic of effect coupling, as deflec-
                              tion or rotation can be produced by both a moment and a force. The
                              strain energy in bending about the y axis is expressed as

                                                                        2
                                               l  M 2  (x)   E  l      d u (x)  2
                                           1
                                   U    =  2Eฒ   b,y    dx =  2ฒ  I (x)   z     dx       (2.14)
                                     b,y         I (x)            y        2
                                              0   y            0        dx
                              where M b,y  (x) is the bending moment  about the  y axis,  I y (x) is the
                              moment  of inertia calculated  about the  same axis, and  u (x) is the
                                                                                     z
                              deflection about the z axis. The differential equation for the bending
                              static equilibrium is
                                                    4
                                                   d I (x)u (x)  =0                      (2.15)
                                                      y
                                                           z
                                                       dx 4
                              The deflection at  a generic point on the micromember  length  is ex-
                              pressed in terms of the free end deflection and rotation, as well as two
                              distribution functions: the linear one f (x) and the rotary one f (x) in the
                                                                 l
                                                                                      r
                              form:
                                               u (x) = f (x)u + f (x)ș y                 (2.16)
                                                 z
                                                        l
                                                                r
                                                            z
                              The two distribution functions of Eq. (2.16) are determined as third-
                              degree polynomials (with four unknown coefficients each) by imposing
                              the following boundary conditions:
                                     u (0) = u z  ș (0) = ș  y  u (l) =0  ș (l) =0       (2.17)
                                                  y
                                                             z
                                      z
                                                                       y
                              The bending-related distribution functions are found to be
                                              3x 2  2x 3                 2x 2  x 3
                                    f (x) =1—     +            f (x) = x —   +           (2.18)
                                     l          2     3        r          l     2
                                               l     l                         l
                              We show later in this chapter, when deriving inertia fractions, that
                              other distribution functions need to be utilized when quantifying the
                              mass fraction (called the effective mass) that corresponds to bending.
                                By combining Eqs. (2.3) and (2.14) through (2.16), the three bending-
                              related stiffnesses (direct linear, direct rotary, and cross) are expressed as








                           Downloaded from Digital Engineering Library @ McGraw-Hill (www.digitalengineeringlibrary.com)
                                      Copyright © 2004 The McGraw-Hill Companies. All rights reserved.
                                        Any use is subject to the Terms of Use as given at the website.
   47   48   49   50   51   52   53   54   55   56   57