This specification covers an aluminum alloy in the form of sheet and plate. These products have been used typically for parts requiring high strength up to 500 φF (260 φC), but usage is not limited to such applications. Product may be welded in the specified condition but properties are improved by reheat treatment after welding. Reheat treatment after welding, however, may reduce resistance to stress-corrosion cracking. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking; ARP823 recommends practices to minimize such conditions.
SAE AMS 4599-2011由美国机动车工程师协会 US-SAE 发布于 2011-07-08。
SAE AMS 4599-2011 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: 49.025.20 铝。
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