江阴兴澄特种钢铁有限公司棒线材研究所,江阴 214429
郑晓伟(1985—),男,本科,高级工程师;E-mail : zhengxiaowei@citicsteel.com
收稿:2025-12-22,
修回:2026-02-09,
录用:2026-02-12,
网络首发:2026-03-04,
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郑晓伟,祁战,张剑锋等.航空紧固件用易切削奥氏体不锈钢303Se冷拉棒材的开发[J].特殊钢,
Zheng Xiaowei,Qi Zhan,Zhang Jianfeng,et al.Development of Cold-drawn Bars of Free-cutting Austenitic Stainless Steel 303Se for Aviation Fasteners[J].Special Steel,
针对航空紧固件对材料的高性能需求,开展了航空用303Se易切削奥氏体不锈钢冷拉棒材的开发研究。基于SAE AMS5640标准,设计并优化了303Se不锈钢的化学成分,重点控制关键成分(质量分数)/%:≤0.03C、0.03~0.06N、0.30Se、0.13P等,以实现良好的切削性能与力学性能匹配。通过热塑性试验研究,设置加热炉均热段温度1 220~1 260 ℃,开轧温度1 120~1 200 ℃,终轧温度≥1 000 ℃的轧制工艺。线材吐丝后水冷至室温,冷拉变形量15%~25 %,成功制备出
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13.7 mm规格的303Se冷拉棒材。冷拉棒材抗拉强度937 MPa(目标区间897~1 030 MPa),断面收缩率58%;硬度171HBW(固溶态要求140~255HBW);组织为单相奥氏体(XRD 检测无铁素体),晶粒度7级,非金属夹杂物综合≤3.0级,产品化学成分、力学性能及金相组织均满足标准要求,具备良好的加工稳定性和使用可靠性。研究结果为航空紧固件用高性能不锈钢材料的国产化提供了技术支撑。
To meet the stringent property demands of aviation fasteners, the development of aviation-grade 303Se free-cutting austenitic stainless steel cold-drawn bars was undertaken. Based on SAE AMS5640, the chemical composition was designed and refined by precisely controlling key elements to/%:≤0.03C ,0.03-0.06N ,0.30Se, 0.13P, to secure an optimum balance between machinability and mechanical strength. According to hot-ductility test results, the reheating soak temperature 1 220 ℃-1 260 ℃, the start rolling temperature 1 120 ℃-1 200 ℃, the finish rolling temperature ≥ 1
000 ℃ was established to roll the wire. the wire was cooled with water to room temperature after wire rod laying,and then cold drew with deformation of 15%-25%, to the
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13.7 mm 303Se cold-drawn bars. The final product exhibits an ultimate tensile strength of 937 MPa (target range 897 MPa-1 030 MPa) ,a reduction of area of 58 % with hardness of 171 HBW (solution-treated target range 140 HBW-255 HBW). The microstructure is composed of single-phase austenite (no ferrite detected by XRD),with the grain size of grade 7 and the overall non-metallic inclusion rating of ≤ 3.0. All chemical, mechanical and metallographic requirements of the standard are satisfied, providing excellent processing stability and service reliability. The results offer a technical foundation for the localization of high-performance stainless steels for aviation fasteners.
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