Page 291 - Academic Press Encyclopedia of Physical Science and Technology 3rd Polymer
P. 291

P1: GPQ Final Pages/GNB  P2: GTV
 Encyclopedia of Physical Science and Technology  En012c-604  July 26, 2001  16:2






               800                                                                              Polymers, Thermally Stable


                      CO      CO
                                               sol n  or melt
                        N  R  N   +  H 2 N  R′  NH 2  peroxide catalyst          O   R 1             O   R 1
                      CO      CO                                                   N    ∆               N
                                                                       R       +             R
                                                                                     O
                                                                                                         O
                         CO      CO
                                                                      (LI)       R 1       ∆
                           N  R  N                                          O                 O  N  R 1
                                     NH  R′  NH                                N
                         CO      CO            (XLIX)                                R 1        O
                                             n                                   O O
                                                                        R           N
                                                                                      O
                                 ∆  pressure
                                                                   The resulting modified materials have exhibited en-
                                cross-linked                     hanced mechanical and environmental (hot/wet) prop-
                                 resin
                                                                 erties over the base BMI resin system. For example,
                                                                                                             2
                                                                 compared with a fracture toughness (G IC = 50 J/m )
                                                                 for base resin, the optimized cured BMI/allylphenyl
                 BMIs have attractive processing characteristics, sim-
                                                                 comonomer blend exhibited significantly enhanced tough-
               ilar to the epoxy resins but with the bonus of higher                 2
                                                                 ness (G IC = 500–600 J/m ). Properties of the carbon fiber-
               temperature performance. Prepregs are produced by im-
                                                                 reinforced laminates have reflected the improved prop-
               pregnating fiber matrix from the melt or from a solu-
                                                                 erties of the unreinforced resins. As discussed earlier
               tion of the monomers. BMI resins are available in a
                                                                 (Section 2), the blending of BMIs with cyanate ester (CE)
               wide range of commercial resin systems. Although sin-
                                                                 resins has enhanced the toughness characteristics of the
               gle monomers can be used, they invariably produce rather                         R
                                                                 BMIs, resulting in a range of (Skyflex ) BT resins.
               brittle products and more frequently eutectic mixtures of
                                                                   The reactivity of the norbornylene (endomethylene
               monomers are supplied in order to lower the viscosity of
                                                                 tetrahydrobenzene) group to “pyrolytic polymerization”
               themeltandimprovethewetting/flowbehavioronthefiber
                                                                 above 300 C forms the basis of the volatileless ther-
                                                                          ◦
               matrix.
                                                                 mal cure of bisarylnadimides (LII) to yield cross-linked
                 Other techniques have been used to improve the tough-
                                                                 resins.
               ness characteristics of the BMIs. The introduction of flex-
               ible groups, e.g., urethane or epoxy segments in the poly-  CO  CO  CO  CO  >300°C
                                                                       N  R  N  A  N  R  N    Cross-linked
               mer chain, while improving toughness, limits the thermal  CO  CO  CO  n=2  CO    resin
                                                                            (LII)
               stability of the BMI resin. Addition of liquid rubber during
               cure has produced a two-phase system that contributes to   R  =    CH 2   ,       ,      O
               a much tougher resin. Unfortunately, the presence of the  e.g.,
                                                                                  CO          C(CF 3 ) 2
               rubber modifier also increases susceptibility to hot/wet     A  =         ,
               degradation.
                 Improvementstotheprocessingandmechanicalproper-   In the thermal polymerization, the rate-determining
               ties of BMI resins have also been achieved by melt blend-  steps involve reverse Diels–Alder reactions to produce
               ing base monomers, including close-to-eutectic mixtures,  N-arylmaleimide moieties, which then provide the key
               with propenyl (L) or allyl (LI) substituted comonomers.  monomers for the final polymerization to the cross-
               Proposed reaction schemes that postulate Diels–Alder cy-  linked resin. Overall fabrication problems associated with
               cloaddition mechanisms are shown below.           this process led to the development of the PMR poly-
                                                                 imides. These are formed by the in situ polymerization of
                                                                 monomeric reactants on the fiber matrix according to the
                                O
                          CH 3                                   scheme shown below.
                                                         CH 3
                                          ∆
                 R           +    N  R 1       R                   Processing of fiber composites (prepregs) involves con-
                                                          O
                                                                 version of the initially formed low-molecular-weight pre-
                                O                       N
                (L)                                  O           polymer into the required component by compression or
                                                          R 1
                                        ∆                        autoclave moulding.
                          O
                               R 1                                                            CO
                             N            O                        PMR-15 (LIII,  R =  CH 2  A  =  ), a key matrix
                                                                 resin for high temperature applications, is the most widely
                                          N R 1
                               O
                                          O                      commercially accepted of the norbornene-terminated
                               CH 3
                     R                                           range of addition PIs. Compared with other high-
                                O
                                                                 temperature materials, it is relatively easy to process, and
                              N
                          O                                      carbon fiber reinforced composites can be fabricated by a
                                R 1
                                                                 variety of techniques. Uses of these materials have been
   286   287   288   289   290   291   292   293   294   295   296