Table 12-2-6 Stress values of compression, tension and torsion spring materials MPa
Wire Type | Oil Quenched-Tempered Spring Wire | Carbon Spring Wire Important Uses Carbon Spring Wire | Stainless steel wire for spring | Bronze wire Bronze plated wire (aged) | 60Si2Mn,60Si2MnA 50CrA、55CrSiA 60CrMnA、60CrMnBA 60Si2Cra,60Si2Crva | ||||||
Compression Spring | Test stress | 0.550, | 0.50 | 0.450, | 0.40r, | 710~890 | |||||
Static load allowable stress | 0.500 | 0.450 | 0.400 | 0.36r, | |||||||
Dynamic load allowable shear stress | finite fatigue life | (.40-0.50 | (0.38-0.45)0 | 70.34-0.40)0 | 70.33~0.36)0 | 568~712 | |||||
infinite fatigue life | 70.35-0.40)0 | 70.33-0.38)0 | 0.30-0.36)0 | 70.30-0-33)0 | 426~534 | ||||||
Tension Spring | test shear stress | 0.440、 | 0.40, | 0.38r, | 0.32o | 475~596 | |||||
Static load allowable stress | 0.40。 | 0.360 | 0.320, | 0.300、 | |||||||
Dynamic load allowable shear stress | finite fatigue life | 70.32-0.40)0 | (0.30-0.36)0 | 70.27-0.32)0 | 70.26~0.29)0, | 405-507 | |||||
infinite fatigue life | (0.28-0.32)0 | (0.27-030)☐ | (0.24-0.30)0, | (0.24-0.28)0 | 356-447 | ||||||
Torsion Spring | Test bending stress | 0.80, | 0.78o | 0.75o, | 0.75o | 994~1232 | |||||
Static load allowable bending stress | 0.720, | 0.70 | 0.680, | 0.680, | |||||||
Dynamic load allowable bending stress | finite fatigue life | 70.60-0.68)0 | (0.58-0.66)0, | 0.55-0.65)0, | 70.55-0.65)0 | 795-986 | |||||
infinite fatigue life | (0.50-0.60)0 | (0.49-0.58)0 | 70.45-0.55)0。 | (0.45~0.55)0, | 636-788 |
Note: 1 Take the intermediate value of tensile strength in table 12-2-3 and table 12-2-4 and the value in table 12-2-4 respectively.
2. For springs with material diameter d<1.0mm, the test shear stress is 90% of the value in the table
3. After the hot coil spring is formed, the hardness after heat treatment is 42~52hrc. When the hardness is the upper limit, the upper limit value in the table shall be taken.
The following points shall be paid attention to when selecting materials and determining allowable stress:
1. for important springs, if their damage has a significant impact on the whole machine, the allowable stress shall be appropriately reduced;
2. the spring treated by strong pressure can improve the fatigue limit, have obvious effect on improving the relaxation under load, and appropriately increase the allowable stress;
3. The shot peened spring can also improve the fatigue strength or fatigue life, and its allowable stress can be increased by 20%;
4. When the working temperature exceeds 60 ℃, the shear modulus G shall be corrected, and the correction formula is Gt =Kt G
Where G – shear modulus at normal temperature;
Gt- shear modulus at working temperature;
Kt- Temperature correction coefficient, its value is obtained from table 12-2-7.
Table 12-2-7 Temperature Correction Factor
Material | Operating temperature/℃ | Material | Operating temperature℃ | ||||||
≤60 | 150 | 200 | 250 | ≤60 | 150 | 200 | 250 | ||
Kt | |||||||||
50CrVA 60Si2Mn 1Cr18Ni9Ti | 1 | 0.96 | 0.95 | 0.94 | 1Cr17Ni7AL QBe2 | 1 | 0.95 | 0.94 | 0.92 |
1 | 0.99 | 0.98 | 0.98 | 1 | 0.95 | 0.94 | 0.92 | ||
1 | 0.98 | 0.94 | 0.9 |