SAE AMS 5920A-2013
真空感应加真空自耗电极融化溶解热处理工作增强和老化,改进强度耐蚀耐热钴镍合金圆棒材19Cr 36Co 25Ni 7.0Mo 0.50Cb (Nb) 2.9Ti 0.20Al 9.0Fe

Cobalt-Nickel Alloy, Corrosion and Heat-Resistant, Round Bars 19Cr 36Co 25Ni 7.0Mo 0.50Cb (Nb) 2.9Ti 0.20Al 9.0Fe Vacuum Induction Plus Vacuum Consumable Electrode Melted Solution Heat Treated, Work Strengthened and Aged, Modified Strength


 

 

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标准号
SAE AMS 5920A-2013
发布日期
2013年02月07日
实施日期
废止日期
中国标准分类号
V11
国际标准分类号
49.025.99
发布单位
US-SAE
引用标准
ASTM E 8-2004 ASTM E 8M-2004 ASTM E 18-2011 ASTM E 18-2012 ASTM E 112-2012 ASTM E 112-2013 ASTM E 354-1993 SAE AMS 2261 SAE AMS 2269 SAE AMS 2371 SAE AMS 2750 SAE AMS 2806
被代替标准
SAE AMS 5920-2003
适用范围
This specification covers a corrosion and heat-resistant, work strengthened and aged cobalt-nickel-chromium alloy in the form of bars 2 inches (50.8 mm) and under in nominal diameter. These bars have been used typically for parts, such as fasteners, requiring a room temperature minimum tensile strength of 170 ksi (1172 MPa) for use up to 850 °F (454 °C) in applications requiring high ductility to promote toughness and resistance to cracking under shock loading conditions, but usage is not limited to such applications. This alloy exhibits exceptionally good resistance to corrosion, crevice corrosion, and stress-corrosion cracking.




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