SAE AMS 6417F-2002

Steel, Bars, Forgings, and Tubing 1.6Si - 0.82Cr - 1.8Ni - 0.40Mo - 0.08V (0.38 - 0.43C) Consumable Electrode Vacuum Remelted

SAE AMS 6417F-2002 发布历史

This specification covers a premium aircraft quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. These products have been used typically for parts 3.5 inches (89 mm) and under in nominal cross-sectional thickness, requiring a through-hardening steel capable of developing a minimum hardness of 52 HRC, the parts being subject to very rigid magnetic particle inspection standards. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking after heat treatment; ARP 1110 recommends practices to minimize such conditions.

SAE AMS 6417F-2002由美国机动车工程师协会 US-SAE 发布于 2002-01-01。

SAE AMS 6417F-2002在国际标准分类中归属于: 49.025.10 钢。

SAE AMS 6417F-2002的历代版本如下：

• 2002年01月01日 SAE AMS 6417F-2002

SAE AMS 6417F-2002 于 2011-05-24 变更为 SAE AMS 6417G-2011 0.08V 消耗电极真空重熔的1.6Si 0.82Cr 1.8Ni 0.40Mo钢制条材,锻件和管材。

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标准号

SAE AMS 6417F-2002

发布日期

2002年01月01日

实施日期

废止日期

无

国际标准分类号

49.025.10

发布单位

US-SAE

代替标准

SAE AMS 6417G-2011

适用范围

This specification covers a premium aircraft quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. These products have been used typically for parts 3.5 inches (89 mm) and under in nominal cross-sectional thickness, requiring a through-hardening steel capable of developing a minimum hardness of 52 HRC, the parts being subject to very rigid magnetic particle inspection standards. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking after heat treatment; ARP 1110 recommends practices to minimize such conditions.