Page 401 - Marks Calculation for Machine Design
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P1: Naresh
                                      15:28
                          January 4, 2005
                 Brown˙C09
        Brown.cls
                              U.S. Customary  MACHINE ENERGY      SI/Metric       383
                    deflection (y cr ) as               deflection (y cr ) as
                                                                         
                                         1/2                               1/2
                                      2                                 2
                                     λ                                 λ
                     y cr = L o C 1 1 − 1 −  eff      y cr = L o C 1 1 − 1 −  eff  
                                                               
                             
                                     C 2                               C 2
                                               1/2                                 1/2
                                            2                                   2
                                         (1.5)                              (1.5)
                       = (3in)(0.81) 1 − 1 −             = (7.5cm)(0.81) 1 − 1 −
                                          6.9                                6.9
                                         1/2                               1/2
                       = (2.43 in)[1 − (1 − 0.326)  ]    = (7.5cm)[1 − (1 − 0.326)  ]
                       = (2.43 in) [1 − (0.821)]         = (7.5cm) [1 − (0.821)]
                       = (2.43 in)(0.179) = 0.44 in      = (7.5cm)(0.179) = 1.3cm
                     Note that this critical deflection (y cr ) repre-  Note that this critical deflection (y cr ) repre-
                    sents almost a 15 percent reduction in length  sents just over a 17 percent reduction in length
                    before the design is unsafe.       before the design is unsafe.
                    9.2.7 Critical Frequency
                    Helical springs, such as those used in the valve trains of internal combustion engines, can fail
                    if the frequency of loading coincides with the natural, or critical, frequency of the spring,
                    called resonance. Different end-conditions, like those summarized in Table 9.2, produce
                    different critical frequencies. To avoid problems, it is usually recommended that the spring
                    design be such that its critical frequency is 15 to 20 times the frequency of the applied cyclic
                    loading frequency.
                      For a helical spring positioned between flat parallel surfaces, where one of the surfaces is
                    driven by a sinusoidal forcing function, the critical frequency ( f cr ) in cycles per second (Hz)
                    is given by Eq. (9.43) as


                                                    1  k
                                                f cr =                          (9.43)
                                                    2  m
                    where (m) is the mass of the active part of the spring.
                      The mass (m) can be found by multiplying the density (ρ) of the spring material times
                    its volume. The development of an expression for the mass of the active part of a spring is
                    given by Eq. (9.44) as

                                         m = density × volume = ρ A
                                                   2
                                                 πd
                                           = (ρ)      (πDN a )                  (9.44)
                                                  4


                                                  A
                                                2 2
                                             ρπ d DN a
                                           =
                                                 4
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