Page 228 - Pressure Vessel Design Manual
P. 228

206    Pressure Vessel Design Manual


               LARGE OPENING-MEMBRANE                              AND BENDING ANALYSIS


                             Notation                            Membrane  stress,  S,n  nozzles  without  reinforcing  pads
                                                                 (Cases 2 and 4).
            A, = area of steel, in.  2                                                         +
                                                                        (Ri(ri + t +e J-
           Ap = area of pressure, in.  2                         0,=P   [                +  Ri(T   rrnt)’l
            P =internal  pressure, psi (design or test)                               AS
            r,  = mean radius of nozzle, in.
           R,  =mean  radius of shell, in.                     a  Bending stress, ab.
            T =thickness  of shell, in.                               (5  1
             t = thickness of nozzle, in.                        M = P  2 + RiriC
            Fy = minimum  specified yield strength, ksi
            u =maximum  combined stress, psi
            Ob =bending  stress, psi
           urn = membrane stress, psi
             I = moment of inertia, in.  4
            M =bending  moment, in.-lb

                            Procedure

         Step 1: Compute boundary limits for bending along shell and
           nozzle in accordance with Note 3. Limit will be governed                  Notes
           by whether material  of  construction has a yield strength,
           F,,  less than or greater than 40 ksi.                 1. Openings that exceed the limits of  UG-36(b)(l) shall
                                                                    meet the requirements  of the 2/3 rule.
             Along shell =                                        2.  This analysis combines the primary membrane stress
             Along nozzle =                                         due  to  pressure  with  the  secondary  bending  stress
                                                                    resulting  from  the  flexure  of  the  nozzle  about  the
         Step 2: Utilizing the appropriate case (Figure 4-3) calculate   hard  axis.
           the moment of inertia, I, and the distance from centroid to   3.  Boundaries  of  metal  along the  shell and nozzle wall
           the inside of the shell, C.                              are as follows:

              I=
              C=                                                                   Along Shell     Along Nozzle
                                                               Cases 1 and 2          m                m
         Step 3: Compute membrane and bending stresses in accor-   Cases 3 and 4       1 6T            16t
           dance with the equations given later.
              urn =
              ub =                                                4. This procedure applies to radial nozzles only.
         Step 4: Combine stresses and compare with allowable.

           urn  +ub  =



                           Calculations
         a Membrane stress, a,  nozzles with reinforcing pads (Cases
           1 and 3).

                 [                 AS                                Figure 4-2.  Areas of pressure and steel for nozzles.
           urn= P   (Ri(ri + t + JRZ,) + R~(T + T,! +  rmt”l
   223   224   225   226   227   228   229   230   231   232   233