A highly alloyed secondary hardening steel 16NiCo has been studying for more than three years.The optimum alloy compeition of the steel should be 0.16C-2Cr-10Ni-1Mo-14Co. After quenching and ag-ing,the microstructure is composed of highly dislocated lath martensite,a small amounts of interlath retained austenite and twinnig,and some carbides which strengthening the alloy. This stecl possessed excellent combined mechanical properties,the typical mechanical values are as follows:the ultimate strength of 1740MPa,the plane fracture toughness KIC of 153MPa √mand and the KISCC of 82MPa√m. 16NiCo met the requirements of aerospace application,and could be widely used to manufacture the critieal joints,horizontal stabilator shaft,arresting hooks and carrier-based aircraft landing gears,etc.
Key words
Ultra-Highstrength steel /
16NiCo
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References
[1] AMS6527
[2] 钟炳文等,航空材料学报,第13卷,第4期,P21, 1993
[3] 16NiCo钢等温与连续冷却转变的特点,621所内部资料,1994
[4] 16NiCo钢中残余奥氏体与逆转变奥氏体的测定,621所内部资料,1993
[5] 中国航空材料手册,第一册,中国标准出版社,1988,北乐
[6] 美国军用手册,航空与航天飞行器结构用金属材料与元件,上册,1984
[7] 300M钢性能数据手册,621研究所,1991
[8] Cytemp Special Steel,Unimach AF1410,1990
[9] 40CrMnSiMoVA钢性能数据汇编,621研究所内部资料,1978
[10] 国产35NCD16钢试验研究,621所内部资料,1979
[11] 轰七用30CrMnSiNi 2A钢油淬工艺研究,621所内部资料.1980
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Footnotes
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