Page 736 - Corrosion Engineering Principles and Practice
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688   C h a p t e r   1 5                      H i g h - Te m p e r a t u r e   C o r r o s i o n    689


                      in Cr or Al, whose oxides are stabilized by increasing O  levels. Alloys,
                                                                   2
                      which  generally  exhibit  increased  oxidation  rates  as  the  O
                                                                               2
                      concentration increase, are S30400, S41000, and S44600 stainless steels
                      and 9Cr-1Mo, Incoloy DS, alloys 617, and 253MA. These alloys tend to
                      form poor oxide scales [2].
                         Most  alloys  tend  to  have  increasing  penetration  rates  with
                      increasing temperature for all oxygen concentrations. Some exceptions
                      are alloys with one to four percent aluminum such as alloy 214. This
                      alloy  requires  higher  temperatures  to  form Al O   as  the  dominant
                                                                3
                                                              2
                      surface oxide, which grows more slowly than the Cr O  that dominates
                                                                2
                                                                  3
                      at  lower  temperatures.  Figure  15.18  summarizes  oxidation  after
                      one year for some common alloys exposed to air.
                             10



                                       Carbon steel
                                                        9Cr 1 Mo

                              1





                          Penetration (mm)  0.1  Nickel  S30400  S31000
                                                                  Alloy 800 H






                                  S41000



                            0.01




                                          Alloy 617


                           0.001
                               550  600  650  700 750  800  850 900  950 1000 1050
                                               Temperature (°C)
                      FIGURE 15.18  Effect of temperature upon metal penetration of some common
                      alloys by oxidation after exposure for one year to air.
   731   732   733   734   735   736   737   738   739   740   741