Page 409 - Corrosion Engineering Principles and Practice
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378    C h a p t e r   9                                                                                                       A t m o s p h e r i c   C o r r o s i o n    379



                           Material    Urban industrial *  Rural †  Marine ‡
                           Nickel           0.15       3.66        0.22
                                            0.24       1.65        0.23
                           Monel            0.16       1.57        0.17
                                            3.56       0.81        0.21
                           Incoloy          0.06       0.02        0.02
                           Inconel          0.05       0.03        0.02
                           Nionel           0.03       0.02        0.02

                          * Newark, N.J.; New York City

                          †   State College, Pa.
                          ‡   Kure Beach, N.C.; La Jolla, Calif.
                      TABLE 9.7   Corrosion in mm/y of Nickel and Its Alloys in Various
                      Atmospheres


                      reason, alloys containing copper and silicon as the principal alloying
                      constituents are susceptible and should be used with care.
                         In  a  rural  atmosphere,  the  corrosion  rate  for  most  alloys  is
                      approximately 0.06 m m/y, while those containing large amounts of
                      copper  about  double  this  low  rate.  In  a  marine  environment,  the
                      differences between alloys appear as a tenfold increase, from about
                      0.6 m m/y for the less corrosion-resistant materials, to about 0.7 m m/y
                      for the better materials. Pitting also is about 10 times greater in marine
                      atmospheres and corrosion can be much greater in a severe industrial
                      atmosphere than in the marine atmosphere.
                         Some aluminum alloys develop severe pitting and a voluminous
                      white  corrosion  product  under  some  exposure  conditions  such  as
                      marine  atmospheres. Aluminum  roofs  have  been  known  to  corrode
                      severely at the overlaps. Some aluminum alloys may also be attacked in
                      their intergranular regions when exposed after certain manufacturing
                      processes  involving  cold  work  or  precipitation  hardening.  General
                      intergranular attack or exfoliation can then occur. In extreme cases, the
                      edges of the affected area are leaf-like and resemble the separated pages
                      of  a  wetted  book  that  has  become  swollen  and  begun  to  open  up
                      (Fig. 9.49). The attack tends to start at sheared edges or punched holes,
                      but is not restricted to these areas. Aircraft manufacturers, in particular,
                      must guard against this type of corrosion.
                         In  designing  aluminum  equipment,  care  must  be  exercised  to
                      avoid dissimilar metal couples and the attendant galvanic corrosion.
                      Copper  and  rusty  steel  are  particularly  detrimental  to  aluminum.
                      Where  it  is  impractical  to  avoid  dissimilar  metals,  the  aluminum
                      should be electrically insulated from the more noble metal by means
                      of  washers,  sleeves,  and  so  forth.  In  some  instances,  covering  the
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