Page 34 - Pressure Vessel Design Manual
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20    Pressure Vessel Design Manual

         possible, stiffeners should always clear shell nozzles. If una-   Step  9: Select  a  stiffener  spacing  based  on  the  maximum
         voidable, special attention should be given to the design of a   length of unstiffened  shell (see Table 2-la). The stiffener
         boxed stiffener or connection to the nozzle neck.       spacing can vary up to the  maximum value  allowable for
                                                                 the assumed thickness. Determine the number of stiffen-
            Design Procedure For Cylindrical Shells              ers necessary and the correspondmg “L’ dimension.
                                                               Step 10: Assume an approximate ring size based on the fol-
         Step 1: Assume a thichess if one is not already determined.   lowing equation:
         Step 2: Calculate  dimensions “L’ and “D.” Dimension  “L’
           should include one-third the depth of the heads. The over-   I=  O.lGD~P,L,
           all length of  cylinder would be as follows for the various    E
           head types:
                                                               Step  11: Compute  Factor  “B” from  the  following equation
                                                                 utilizing the area of the ring selected:
              W/(2) hemi-heads         L = LT-T  + 0.333D
                                                                       0.75PD0
              W/(2) 2:1 S.E. heads     L = LT-T + 0.16661)         g=-
                                               +
              W/(2) 100% - 6% heads    L = h-~ 0.112D                  t+As / Ls
                                                               Step 12: Utilizing Factor “B” computed  in step 11, find the
         Step 3: Calculate  UD,  and D,Jt  ratios                corresponding  “A’ Factor  from  the  applicable  material
          Step 4: Determine Factor “A’ from ASME Code, Section 11,   curve.
           Part  D,  Subpart  3,  Fig  G:  Geometric  Chart  for   Step 13: Determine the required moment of inertia from the
           Components  Under  External  or  Compressive  Loadings   following equation. Note that Factor “A” is the one found
            (see Figure 2-le).                                   in step 12.
          Step  5: Using  Factor  “A’ determined  in  step 4,  enter the
            applicable  material  chart  from  ASME  Code,  Section  11,   Ls(t+As /Ls 1-41
            Part  D,  Subpart  3 at  the  appropriate  temperature  and   I,  =   14
           determine Factor  “B.”
          Step 6: If Factor “A’ falls to the left of the material line, then   Step  14: Compare  the  required  moment  of inertia, I, with
            utilize the following equation to determine the allowable   the actual  moment  of  inertia  of  the  selected member.  If
            external pressure:                                   the  actual  exceeds  that  which  is  required,  the  design  is
                                                                 acceptable  but  may  not  be  optimum.  The  optimization
                                                                 process  is  an  iterative  process  in  which  a  new  member
                                                                 is  selected,  and  steps  11  through  13  are  repeated
                                                                 until  the  required  size and actual  size are approximately
          Step 7: For values of  “A’ falling on the material line of the   equal.
            applicable  material chart, the allowable external pressure
            should be computed  as follows:
                    4B                                                               Notes



          Step 8: If the computed  allowable external pressure  is less   1. For conical sections where c( < 22.5 degrees, design the
            than the design external pressure, then a decision must be   cone as a cylinder where  Do  = DL and length is equal
            made on how to proceed. Either (a) select a new thickness   to L.
            and start the procedure  from  the  beginning or  (b) elect   2.  If  a  vessel  is  designed  for  less  than  15psi,  and  the
            to  use  stiffening  rings  to  reduce  the  “L’ hmension.  If   external pressure  condition is not going to be stamped
            stiffening rings are to be utilized, then  proceed  with the   on  the  nameplate,  the  vessel  does  not  have  to  be
            following steps.                                        designed  for the external pressure  condition.
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