Page 429 - 04. Subyek Engineering Materials - Manufacturing, Engineering and Technology SI 6th Edition - Serope Kalpakjian, Stephen Schmid (2009)
P. 429

Section 16.7  Deep Drawing  409


              capable of undergoing a reduction in width due to a reduction in
              diameter and (b) must also resist thinning under the longitudinal ten-  R : él
                                                                                     s
              sile stresses in the cup wall. Deep drau/ability generally is expressed    S  Sf
              by the limiting drawing ratio (LDR) as

                                Maximum blank diameter    DO
                              =                         =    .     16.10
                         LDR         Punch diameter       DI,     (     )
              Whether a sheet metal can be deep drawn successfully into a round
              cup-shaped part has been found to be a function of the normal
              anisotropy, R (also called plastic anisotropy), of the sheet metal.
              Normal anisotropy is defined in terms of the true strains that the  FIGURE |6.32  Strains on  a tensile-test
              specimen undergoes in tension (Fig. 16.32):                   specimen removed from  a piece of sheet
                                                                            metal. These strains are used in determining
                                     Width strain    sw                     the normal and planar anisotropy of the
                               R                       .           1 6. 1 1
                                    Thickness strain  s,          (     )   sheet metal.
                   In order to determine the magnitude of R, a tensile-test specimen is first pre-
              pared and subjected to an elongation of 15 to 20%. The true strains that the sheet
              undergoes are calculated in the manner discussed in Section 2.2. Because cold-rolled
              sheets generally have anisotropy in their planar direction, the R value of a specimen
              cut from a rolled sheet will depend on its orientation with respect to the rolling
              direction of the sheet. For this condition, an average value, Ravg, is calculated from
              the equation
                                           _ R0 + 2R45 + R90
                                       Ravg _       4        s                  (16.12)

              where the subscripts are the angles with respect to the rolling direction of the sheet.
              Some typical Ravg values are given in Table 16.4.
                   The experimentally determined relationship between Ravg and the limiting
              drawing ratio is shown in Fig. 16.33. lt has been established that no other mechani-
              cal property of sheet metal shows as consistent a relationship to LDR as does Ravg.
              Thus, by using a simple tensile-test result and obtaining the normal anisotropy of
              the sheet metal, the limiting drawing ratio of a material can be determined.

              Earing.  In deep drawing, the edges of cups may become wavy-a phenomenon
              called earing (Fig. 16.34). Ears are objectionable on deep-drawn cups because they
              have to be trimmed off, as they serve no useful purpose and interfere with further
              processing of the cup, resulting in scrap. Earing is caused by the planar anisotropy



                            TABLE l6.4

                              Typical Ranges of Average Normal Anisotrnpy,
                              Rays, fur Various Sheet Metals
                             Zinc alloys                      0.4-0.6
                            Hot-rolled steel                  0.8-1.0
                             Cold-rolled, rimmed steel        1.0-1.4
                             Cold-rolled, aluminum-killed steel  1.4-1.8
                            Aluminum alloys                   0.6-0.8
                             Copper and brass                 0.6-0.9
                            Titanium alloys (cz)              3.0-5.0
                             Stainless steels                 0.9-1.2
                            High-strength, low-alloy steels   0.9-1.2
   424   425   426   427   428   429   430   431   432   433   434