Page 213 - Pressure Vessel Design Manual
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Design of  Vessel Supports   191

            Assume thickness t,  and calculate I and Z:

               tcy3
            I=---
                12














                  f
            Mx =a



                                                                       f
                                                                  M  - - [l + (e-Bx(cos px - sin px))]
                                                                     - 4/53
          Note:  These  calculations  are  based  on  a  beam  on  elastic
          foundation methods.                                   Bx is in radians. See Procedure 5-2.

                                                                      M,
          Double Gusset                                           fb = - 0.6F,
                                                                         <
                                                                      Z
                            f  +-+f








          Figure 3-68. Loading diagram of compression plate with two gussets.













                                                         Table 3-31
                                                     Standard Lug Dimensions

          Type           e           b            Y            X            h            tg=b           Capacity (b)
          1              4           6            2            6            6              %               23.500
          2              4           6            2            6             9            36               45,000
          3              4           6            2            6            12             ?h              45,000
          4              5           7            2.5          7            15            9/16             70,000
          5              5           7            2.5          7            18             %               70,000
          6              5           7            2.5          7            21           "e                70,000
          7              6            8           3            8            24             %              100,000
   208   209   210   211   212   213   214   215   216   217   218