Steel bars, forgings and rings, 0.95Cr 0.20Mo (0.38-0.43C), annealed. (SAE standard)
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings. These products have been used typically for parts, 0.50 inch (12.7 mm) and under in nominal section thickness at time of heat treatment, requiring a through-hardened steel capable of developing hardness as high as 50 HRC when properly hardened and for parts of greater thickness but requiring proportionally lower hardness, but usage is not limited to such applications. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking after heat treatment; ARP1110 recommends practices to minimize such conditions. Alloy: 4140 UNS Number: G4140.
- Research Organization:
- Society of Automotive Engineers, Inc., Warrendale, PA (United States)
- OSTI ID:
- 591038
- Report Number(s):
- SAE-AMS-6382L/XAB; TRN: 80903335
- Resource Relation:
- Other Information: DN: Copyright Society for Automotive Engineers (SAE), 400 Commonwealth Drive, Warrendale, PA. 15096, USA. This document is available from NTIS under license from SAE. See also MIL-S-5626; PBD: May 1995
- Country of Publication:
- United States
- Language:
- English
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