Page 33 - Analysis and Design of Machine Elements
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An Overview of Machine Design
                            In summary, failure is the response of a machine or machine element to operating  11
                          loads and service environments. Imperfection in design, materials and manufacturing
                          may cause failure. Identification of possible failure modes under prescribed operating
                          condition is an essential step in the early stage of machine element design. It is the
                          designer’s responsibility to predict, analyse and prevent prospective failure to ensure
                          a successful design of machine elements or machines throughout a design’s lifetime.

                          1.3.3  Design Criteria
                          Safety is always the paramount criterion in machine design [9], as catastrophic failures
                          result in life losses, property destruction and environmental damage and must be pre-
                          vented. To provide a safe, reliable and cost-effective machine element, it is essential to
                          establish design criteria against potential failure modes. The design criteria commonly
                          used against the previously discussed failure modes include strength, rigidity, life and
                          wear criteria.

                          1.3.3.1  Strength Criteria
                          Strength is the ability to resist loads. It is expressed in terms of ultimate strength, yield
                          strength and fatigue strength [1]. Almost all kinds of failure modes, including yielding,
                          fracture, fatigue, pitting, spalling, wear, scoring, scuffing, galling and seizure, are due
                          to insufficient material strength to withstand loads. Design approaches must satisfy a
                          strength criterion in the form of a stress-strength relationship, either within an element
                          or on the element surface, to ensure safe design.
                            The strength criterion indicates that the actual stresses    acting on an element at a
                          critical location under operating conditions must be less than the allowable stress of
                          material [  ], expressed as
                                  ≤ [  ]                                                      (1.1)

                            The limiting condition to the right of the inequality depends on material properties.
                          Under a static load, the allowable stress is the material strength divided by the allowable
                          safety factor. The material strength is the yield strength in tension, compression or shear
                          for ductile materials; and ultimate strength for brittle materials. Under a fluctuating load,
                          the material strength is the endurance strength corresponding to the operating condi-
                          tions. Detailed discussion about endurance strength will be introduced in Chapter 2.
                            The ability to quantify stress states at a critical location in a machine element is impor-
                          tant for assessing failure possibility of an element. Stresses are obtained by simplified
                          calculations according to various loading conditions. For uniaxial loading, the stress
                          calculation is quite straightforward, using stress formula loaded by basic tension, shear
                          or bending. For complex loading, a combined stress theory, either the maximum shear
                          stress theory or the maximum distortion energy theory, is used to calculate multiax-
                          ial stresses [14, 15]. For contact loading, the contact stress is calculated by the Hertz
                          formula [16].
                            Designers must ensure the maximum stresses at critical locations are less than mate-
                          rial strength     by a sufficient margin to guarantee adequate safety for an element. This
                                      lim
                          margin is the factor of safety, a reasonable measure of relative safety of a load-carrying
                          element. Thus, an alternate expression for strength criterion by safety factor S is
                                      lim
                               S =     ≥ [S]                                                  (1.2)
                                      
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