Page 82 - Analysis and Design of Machine Elements
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                            radial distance between centroid
                       r Analysis and Design of Machine Elements        helix angle,  ∘
                        i
                            and ith bolt centre, mm              lead angle,  ∘
                       S    safety factor                        deflection, mm
                       S p  safety factor for crushing           tensile stress, MPa
                       T    torque, N mm                       ca  calculated tensile stress, MPa
                       T 1  frictional torque in the thread,     p  bearing stress, MPa
                            Nmm                                  yield strength, MPa
                                                              s
                       T  2  frictional torque at bearing surface,  [  ]  allowable tensile stress, MPa
                            Nmm                             [   ] allowable bearing stress, MPa
                                                              p
                       W    effective section modulus, mm 3       shear stress, MPa
                       z    number of bolts in a joint group  [  ]  allowable shear stress, MPa
                            thread angle,  ∘                     equivalent frictional angle,  ∘
                                                              v

                       3.1 Introduction

                       3.1.1  Applications, Characteristics and Structures
                       Machine joints are used to connect two or more components together. They form
                       indispensable parts in machine constructions, as they facilitate manufacturing and
                       assembly, accommodate shipping and handling, permit disassembly for repair, replace-
                       ment and maintenance. Virtually all machines comprise an assemblage of individual
                       parts, separately manufactured and joined together by various fastening methods [1].

                       For example, a jumbo jet such as Boeing’s 747 uses about 2.5 million fasteners [2].
                         Machine joints can be broadly classified as detachable and permanent joints. Detach-
                       able joints can be disassembled without damaging any element in the connection. Con-
                       nections using threaded fasteners, keys and splines are typical examples of detachable
                       joints. Permanent joints refer to connections like riveting, welding, bonding (brazing,
                       soldering, adhesive bonding) and so on that cannot be disassembled without damaging
                       elements of the joint.
                         As joints and connections cause geometrical and material discontinuities, high local
                       stresses and potential failures, the number of joints should be reduced [1–4]. As a mat-
                       ter of fact, joints remain the weakest link in a machine and their high safety concern
                       presents an incessant challenge to designers and engineers. It is therefore necessary to
                       have a thorough understanding of performance and careful analysis of joints under all
                       conditions of service, especially in cars, aeroplanes, steam and gas turbines and so on
                       where mechanical reliability and human safety are vital.
                         This chapter will discuss in detail the analysis and design of conventional standard
                       threaded fasteners. The detachable fastening methods for shaft and hub, as well as per-
                       manent connection methods will be introduced in the following chapters.


                       3.1.2  Selection of Fastening Methods
                       The selection of fastening methods depends upon many factors. The first is whether
                       the joint is to be permanent or detachable. The selection of permanent joints is
                       mainly due to the consideration of manufacturing and assembly costs; while the
                       selection of detachable joints considers far more factors, including structure, assembly,
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