Page 198 - Handbook of Structural Steel Connection Design and Details
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Welded Joint Design and Production

                                                   Welded Joint Design and Production  183

                      The requirements for fabrication of aluminum are contained in
                    AWS D1.2 Structural Welding Code—Aluminum.


                    3.2 Weld Cracking/Solutions
                    Weld cracking is a problem faced occasionally by the fabricator. This
                    section will discuss the various types of cracking and possible solu-
                    tions for steel alloys.
                      Several types of discontinuities may occur in welds or heat-affected
                    zones. Welds may contain porosity, slag inclusions, or cracks. Of the
                    three, cracks are by far the most detrimental. Whereas there are
                    acceptable limits for slag inclusions and porosity in welds, cracks are
                    never acceptable. Cracks in, or in the vicinity of, a weld indicate that
                    one or more problems exist that must be addressed. A careful analysis
                    of crack characteristics will make it possible to determine their cause
                    and take appropriate corrective measures.
                      For the purposes of this section, “cracking” will be distinguished
                    from weld failure. Welds may fail due to overload, underdesign, or
                    fatigue. The cracking discussed here is the result of solidification,
                    cooling, and the stresses that develop due to weld shrinkage. Weld
                    cracking occurs close to the time of fabrication. Hot cracks are those
                    that occur at elevated temperatures and are usually solidification
                    related. Cold cracks are those that occur after the weld metal has
                    cooled to room temperature and may be hydrogen related. Neither is
                    the result of service loads.
                      Most forms of cracking result from the shrinkage strains that
                    occur as the weld metal cools. If the contraction is restricted, the
                    strains will induce residual stresses that cause cracking. There are two
                    opposing forces: the stresses induced by the shrinkage of the metal
                    and the surrounding rigidity of the base material. The shrinkage
                    stresses increase as the volume of shrinking metal increases. Large
                    weld sizes and deep penetrating welding procedures increase the
                    shrinkage strains. The stresses induced by these strains will
                    increase when higher-strength filler metals and base materials are
                    involved. With a higher yield strength, higher residual stresses will
                    be presented.
                      Under conditions of high restraint, extra precautions must be uti-
                    lized to overcome the cracking tendencies which are described in the
                    following sections. It is essential to pay careful attention to welding
                    sequence, preheat and interpass temperatures, postweld heat treat-
                    ment, joint design, welding procedures, and filler material. The judi-
                    cious use of peening as an in-process stress relief treatment may be
                    necessary to fabricate highly restrained members.





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