Page 735 - 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


                      The vapor aluminum-diffused surface layer is hard and brittle, but
                      the bulk substrate retains the properties of conventional steels.
                         Extensive testing of alloys has shown that many alloys establish
                      parabolic time dependence after a minimum time of 1000 hours in air
                      at temperatures above 900°C. If the surface corrosion product (scale) is
                      removed or cracked so that the underlying metal is exposed to the gas,
                      the rate of oxidation can be much faster. The influence of O  partial
                                                                         2
                      pressure on oxidation above 900°C is specific to each alloy, as illustrated
                      for  some  common  alloys  in  Fig.  15.17.  Most  alloys  do  not  show  a
                      strong influence of the O  concentration upon the total penetration.
                                           2
                      Alloys  such  as  Alloy  HR-120,  and  Alloy  214  even  exhibit  slower
                      oxidation rates as the O  concentration increases. These alloys are rich
                                          2
                            100




                                                Carbon steel



                             10



                                                          9Cr 1 Mo
                            Penetration (mm)  1  Nickel     S30400

                                                              S41000








                             0.1                            S31000 Alloy 800 H

                                               Alloy 617






                            0.01
                              0.001          0.01           0.1            1
                                                     (atma)
                                                  P O
                                                    2
                      FIGURE 15.17  Effect of oxygen partial pressure upon metal penetration of
                      some common alloys by oxidation after exposure for one year at 930°C.
   730   731   732   733   734   735   736   737   738   739   740