SAE AMS 4909J-2012
超低间隙退火,5Al 2.5Sn板材,带材和片材钛合金

Titanium Alloy, Sheet, Strip, and Plate 5Al 2.5Sn, Extra Low Interstitial Annealed


SAE AMS 4909J-2012 发布历史

This specification covers a titanium alloy in the form of sheet, strip, and plate. These products have been used typically for parts requiring a combination of weldability, ductility, and good notch-toughness down to -423 °F (-253 °C), but usage is not limited to such applications. Certain processing procedures and service conditions may cause those products to become subject to stress-corrosion cracking; SAE ARP 982 recommends practices to minimize such conditions.

SAE AMS 4909J-2012由美国机动车工程师协会 US-SAE 发布于 2012-08-16。

SAE AMS 4909J-2012 在中国标准分类中归属于: V11 航空与航天用金属铸锻材料,在国际标准分类中归属于: 49.025.30 钛。

SAE AMS 4909J-2012 发布之时,引用了标准

SAE AMS 4909J-2012的历代版本如下:

  • 2012年08月16日 SAE AMS 4909J-2012 超低间隙退火,5Al 2.5Sn板材,带材和片材钛合金

SAE AMS 4909J-2012 由 SAE AMS 4909H-2008 变更而来。

 

 

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标准号
SAE AMS 4909J-2012
发布日期
2012年08月16日
实施日期
废止日期
中国标准分类号
V11
国际标准分类号
49.025.30
发布单位
US-SAE
引用标准
ASTM E 8/E 8M-2011 ASTM E 290-2009 ASTM E 384-2011 ASTM E 1409-2008 ASTM E 1447-2009 ASTM E 1941-2010 ASTM E 2371-2004 SAE AMS 2242 SAE AMS 2249 SAE AMS 2368-1995 SAE AMS 2631 SAE AMS 2750 SAE AMS 2809-1986 SAE ARP 982
被代替标准
SAE AMS 4909H-2008
适用范围
This specification covers a titanium alloy in the form of sheet, strip, and plate. These products have been used typically for parts requiring a combination of weldability, ductility, and good notch-toughness down to -423 °F (-253 °C), but usage is not limited to such applications. Certain processing procedures and service conditions may cause those products to become subject to stress-corrosion cracking; SAE ARP 982 recommends practices to minimize such conditions.




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