Page 144 - The Tribology Handbook
P. 144

Table 25.2 Relevant properties of some flexure materials

                                                            Faiigue strength'   T-Qu~~s .Maddicr                 Atmospheric  Approximate  maximum
                                                                                  E
                     Material                                   ff           (For G see note 7)   k,     k,      resistance4   temperature in air
                                                                                                               -
                                                         N/m2 x lo7  Ibf/in2 X lo3  N/mZ ~10'~ Ibf/in2 x IO6  W/m "C  Btu/h ft "F  %IACS3
                                        N/mZ x IO7   Ibf/in2 x IO'   ____   --  -_               --__            __      "C     "F
                                              _-
                     Spring steels   o'6-1*oc   80-210   120-300   40-70   60-100   21   30   45   26    9.5     P       230    450
                               0.3-0.9Mn      - _.         _.___                                   -                        -
                     Carbon chromium stainless   150   200   60   85      21       30      24     14     2.8     M       540    1000
                       steel (BS 420 S45)
                                          ___l_l--___-- -
                     High strength alloy steels :   210   300   66   96   19       27      17     10     4       P       480    900
                       nickel maraging steel
                     DTD 5192 (NCMV)    210      300     80       115     21       30      35     20     6       P       400    750
                     Inconel X           165     240     65       95      21       31      12     7       I .7   E       650    1200
                     High strength titanium alloy   95   140   65   95    11       16      9      5       1.1    G       480    900   -
                 R   High strength aluminium alloy  50   -  73   15   -   7.2      10.4    ! 20   70     30      P       200    400
                                                                  22
                 tn
                 h)   Beryllium copper   90      I35     38       55      12.5     18      100    60     25      G       230    450
                     Low beryllium copper   65   95      24       35      11.5     16.5    170    100    45      G       200    400
                                               -
                     Phosphor bronze    60       90      20       29      11       16      55     32      12     G       180    350
                       (8% Sn; hard)
                     Glass fibre reinforced nylon   20   30   NA   NA     1.2      1.8     0.35   0.20   negligible  E   1 IO   230
                       (40% G.F.)
                     Polypropylene       3.7     5.45    NA       NA      0.14     0.25    0.17   0.1    negligible  E6   50    120

                     Notes:  1, Very dependent on heat treatment and degree of working. Figures given are typical of   5.  At high strain rate. Substantial creep occurs at much reduced stress levels, probably
                           fully  heat  treated  and  processed  strip  material  of  about  0.1 in  thickness at  room   restricting  applications  to  where  the  steady  load  is  zero  or  very  small,  and  the
                           temperature. Thinner strip and wire products can have higher yield strengths.   deflections are of short duration.
                         2.  Fatigue strengths are typical for reversed bending of smooth finished specimens sub-   6.  But the material deteriorates rapidly in direct sunlight.
                          jected to lo7 cycles. Fatigue strengths are reduced by  poor surface finish and corrosion,   7.  Modulus of Rigidity, G = E/2 (1 +Poisson's ratio, v). For most materials  u   0.3, for
                           and may continue to fall with increased cycles above IO7.   which G   E/2.6.
                         3.  Percentage of the conductivity of annealed  high-purity  copper at 20°C.
                         4.  Order ofresistanceon following scale: P-poor,  M-moderate,  G-good,  E-excellen:.   NA  Data not available.
                           Note, however, that protection  from corrosion can often be given to materials which
                           are poor in this respect by grease or surface treatments.
   139   140   141   142   143   144   145   146   147   148   149