Page 145 - The Tribology Handbook
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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.
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