Page 87 - Pressure Vessel Design Manual
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68    Pressure Vessel Design Manual

                                                  PROCEDURE 2-12
                                ~~
                           REINFORCEMENT FOR STUDDING OUTLETS






















                                                 Figure 2-40.  Typical studding outlet.


                                                          Table 2-9
                                                   Tapped Hole Area Loss, S, in.'*
           ds       % in.   %  in.   '/8  in.   lin.   1% in.  12, in.   1% in.   1% in.   1% in.   1% in.   1% in.   2in.   2% in.
           X        1.11    1.33   1.55   1.77    2.00   2.44   2.66    2.88   3.10    3.32    3.56
           S        1.28    1.84   2.50   3.28    4.15   5.12    6.20   7.38   8.66   10.05   11.55



                                                                         1 00
               Calculation of Area of Reinforcement
                             (Figure 2-40)                               0 95

                                                                         0 90
            A = (dt,F) + S
            L = Greater of d or R,  + t,  + t                            0 85
           A1 = 2(L - R,  - t,)(t  - t,)
                                                                         0 80
           A2  = 2(tp - h - tr)(t,  - tm)                              LL
                                                                       L
           A3  = 2(ht,)                                                5075
                                                                       -
           AT=AI+AZ+AB                                                 2
                                                                         0 70


                                                                         0 65
                                 Notes
                                                                         0 60
             1. Check  plane  which  is  nearest  the  longitudinal  axis of
               the vessel and passes through a pair of studded holes.    0 55
             2.  Sb=allowable  stress  of  stud  material  at  design  tem-
               perature.                                                 050 1
               Sf, = allowable stress of flange material  at design tem-    0"  10"  20"  30" 40"  50"  60" 70" 80" 90"
               perature.                                                        Anqla of plane with Longitudinal Axis
             3. A2 as computed ignores raised face.              Figure 2-41.  Chart for determining the value of F. (Reprinted by permis-
                                                                sion from ASME Code, Section VIII, Div. 1, Figure UG-37.)
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