Page 44 - Automotive Engineering
P. 44

Measurement of torque, power, speed and fuel consumption        CHAPTER 2.1

                                                              rises and at n ¼ n c it becomes theoretically infinite: the
                                                              shaft may fracture or non-linearities and internal
                                                              damping may prevent actual failure. With further in-
                                                                                                        p ffiffiffiffiffiffiffi
                                                              creases in frequency the amplitude falls and at n  2n c it
                                                              is down to the level of the static deflection. Amplitude
                                                              continues to fall with increasing frequency.
                                                                The shaft connecting engine and dynamometer must
                                                              be designed with a suitable stiffness C s to ensure that
                                                              the critical frequency lies outside the normal operating
                                                              range of the engine, and also with a suitable degree of
                                                              damping to ensure that the unit may be run through the
           Fig. 2.1a-2 Two mass system (compare with Fig. 2.1a-1).  critical speed without the development of a dangerous
                                                              level of torsional oscillation. Fig. 2.1a-3 also shows the
                                                              behaviour of a damped system. The ratio q=q is known
                                                                                                     0

           The two masses can vibrate 180 out of phase about  as the dynamic magnifier M. Of particular importance is
           a node located at some point along the shaft between  the value of the dynamic magnifier at the critical fre-
           them. The oscillatory movement is superimposed on any  quency, M c . The curve of Fig. 2.1a-3 corresponds to
           steady rotation of the shaft. The resonant or critical fre-  a value M c ¼ 5.
           quency of torsional oscillation of this system is given by:  Torsional oscillations are excited by the variations in
                    s ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi                 engine torque associated with the pressure cycles in the
                  60  C c ðI e þ I Þ                          individual cylinders (also, though usually of less impor-
                              b
             n c ¼                                      (1)
                  2p     I e I b                              tance, by the variations associated with the movement of
                                                              the reciprocating components).
             If an undamped system of this kind is subjected to an  Fig. 2.1a-4 shows the variation in the case of a typical
           exciting torque of constant amplitude T ex and frequency  single cylinder four-stroke diesel engine. It is well
           n, the relation between the amplitude of the induced  known that any periodic curve of this kind may be
           oscillation q and the ratio n/n c is as shown in Fig. 2.1a-3.  synthesized from a series of harmonic components, each
             At low frequencies, the combined amplitude of    a pure sine wave of a different amplitude having a fre-
           the two masses is equal to the static deflection of the  quency corresponding to a multiple or submultiple of
           shaft under the influence of the exciting torque,   the engine speed and Fig. 2.1a-4 shows the first six
           q ¼ T ex =C s . As the frequency increases, the amplitude  components.
            0

































           Fig. 2.1a-3 Relationship between frequency ratio, amplitude and dynamic amplifier M.


                                                                                                       37
   39   40   41   42   43   44   45   46   47   48   49