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This SAE Recommended Practice provides comprehensive engineering guidelines for oil-tempered chromium-silicon alloy steel wire and the springs manufactured from it. Designed for service at moderately elevated temperatures where resistance to set is critical, the standard covers material requirements per ASTM A401/A401M, spring processing, heat treatment, hardness verification, and surface quality acceptance criteria. Adhering to these practices helps ensure consistent performance in demanding applications such as automotive valvetrain, suspension, and industrial spring systems.
The standard applies to oil-tempered chromium-silicon alloy steel wire used to fabricate springs that must resist permanent deformation (set) under load at moderately elevated temperatures. Wire must conform to the chemical and mechanical requirements of ASTM A401/A401M. A longitudinal microstructural examination must reveal a fine, homogeneous tempered martensite structure. Decarburization is evaluated on a polished transverse section etched in nital, examined at 100× magnification, and must not exceed:
These limits are critical to maintain fatigue resistance and consistent mechanical properties in the finished spring.
Springs must be stress relieved immediately after coiling to relieve residual stresses without reducing hardness. The recommended temperature range is 340–430 °C (650–800 °F), with a minimum soak time of 30 minutes at heat. Lower stress relief temperatures may be used for certain torsional or extension springs, but any deviation should be agreed upon between purchaser and supplier.
Hardness testing is performed on finished springs. For wire diameters 1.60 mm (0.062 in) and larger, a suitable ground flat is prepared; for smaller diameters, ground-mounted sections are used. Hardness scale and values must comply with Tables 1A (SI) or 1B (inch-pound) depending on wire diameter. The table below summarizes the inch-pound hardness requirements for selected wire sizes from Table 1B.
| Wire Diameter (in) | Hardness Scale | Min | Max |
|---|---|---|---|
| 0.032 | R15N | 88.5 | 90.0 |
| 0.041 | R15N | 88.5 | 90.0 |
| 0.054 | R15N | 88.0 | 89.5 |
| 0.062 | R45N | 59.5 | 63.0 |
| 0.080 | R45N | 59.0 | 62.0 |
| 0.120 | R45N | 57.5 | 61.0 |
| 0.135 | RC | 51.5 | 54.0 |
| 0.312 | RC | 49.0 | 52.0 |
| 0.438 | RC | 48.0 | 51.0 |
Values for intermediate diameters may be interpolated. Always confirm that the finished spring hardness falls within the appropriate range for its wire size.
Surface condition of finished springs must be free from excessive coiling marks, nicks, or gouges that could impair serviceability. Shot peening is permitted only when specified or agreed upon, and its use changes surface appearance. The shot peening process reduces relaxation resistance, hence the mandatory lower-temperature stress relief afterward.
Wire diameters 0.032–0.054 in (0.80–1.40 mm) use the R15N scale; diameters 0.062–0.120 in (1.60–3.00 mm) use the R45N scale; diameters 0.135 in (3.50 mm) and larger use the Rockwell C scale. Refer to Tables 1A or 1B in the standard for exact minimum and maximum values. Intermediate wire sizes can be interpolated.
Decarburization is evaluated on a polished transverse section etched with nital and examined at 100× magnification. Carbon-free depth must not exceed 0.5% of the wire diameter, and combined depth of carbon-free and partial decarburization must not exceed 2% of the wire diameter. These limits help ensure adequate fatigue strength.
As-coiled springs: stress relieve at 340–430 °C (650–800 °F) for at least 30 minutes. Shot-peened springs: stress relieve at 200–245 °C (400–475 °F) for at least 30 minutes. The lower temperature for shot-peened springs minimizes relaxation of the compressive surface layer while still providing stress relief.
Excessive coiling marks, nicks, gouges, or any other surface imperfection that could impair the serviceability of the spring is not allowed. The surface must be smooth enough to avoid stress concentrations that could lead to premature fatigue failure.