Page 385 - Mechanics Analysis Composite Materials
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370                 Mechanics and analysis of composiie materials

              A  = 1/3. Because Nxu = 0, the structure of the laminate is symmetric with respect to
              the cylinder meridian, and Eqs. (8.12)-(8.14)  can be reduced to

                  h=-3PR                                                        (8.16)
                      2a,  '

                   k
                  Chi(3cos24i- 1) = 0  .                                        (8.17)
                  i=  1
              Comparing Eq. (8.16)  with  the corresponding expression for the thickness  of the
              metal pressure vessel which is h,  =pR/G we can see that the thickness of an optimal
              composite  vessel  is  1.5  times  higher  than  h,.   Nevertheless,  because  of  higher
              strength and lower density, composite pressure vessels are significantly lighter than
              metal ones. To show this, consider pressure vessels with radius R  = 100 mm made of
              different materials and designed for the burst pressure p = 20 MPa. The results are
              listed in Table 8.1. As can be seen, the thickness of the glass-poxy  vessel is the same
              as that of the thickness  of the steel vessel, because the factor  1.5 in Eq. (8.16)  is
              compensated by the composite strength which is 1.5 times higher than the strength
              of  steel. However, the density of a glass-epoxy  composite is much lower than the
              density of steel, and as a result, the mass of the unit surface area of the composite
              vessel makes only 27%  of  the corresponding characteristic for a  steel vessel. The
              most promising for pressure vessels are aramid composites having the highest tensile
              specific strength (see Table 8.1).
                Consider  Eq. (8.17)  which  shows  that  there  can  exist  an  infinite  number  of
              optimal laminates with one and the same thickness specified by Eq. (8.16).
                The  simplest  is  the  cross-ply  laminate  having  k = 2,  Q,l  = 0",  hl =ha, and
              +2  = 90",h2  = h90. For this structure, Eq. (8.17) yields h90  = 2ho. This result seems
               obvious because Ny/Nx = 2. For symmetric &+ angle-ply laminate, we should take
              k = 2, hl  = h2  = h4/2, 4,  = +4, 42= -6.  Then

                  cos  Q, = 1  4 = 40 = 54"44'  .
                     2
                          3'
              Table 8.1
              Parameters of metal and composite pressure vessels.
               Parameter        Material

                                Steel   Aluminum   Titanium   Glass-  Carbon-  Aramid-
                                                           epoxy    epoxy   epoxy
              Strength, Z,5,  (MPa)   1200   500   900     1800     2000    2500
               Density, p  (g/cm3)   7.85   2.7     4.5      2.1      1.55     1.32
               Thickness of the vessel,   1.67   4.0   2.22   1.67    1.5      1.2
               h,,  h (mm)
               Mass of the unit surface   13.1 I   10.8   10.0   3.51   2.32   1.58
               area, ph (kg/m2)
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