钢丝编织的 SUS 304 奥氏体不锈钢的拉伸强度

Rando Tungga Dewa, Daffa Mandala Adinata, Raja Akbar, Muhammad Raihan Atallah Yasir
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引用次数: 0

摘要

本文对拉丝 SUS 304 进行了一系列拉伸测试,以满足所需的规格要求,从而使其可用于飞机战斗机部件,在发动机运行时保持稳定,避免晃动或振动。所研究的材料有望用于侧翼机身,以提高其强度、耐磨性、耐腐蚀性和美观性。根据 ASTM E8 标准,使用带有改良夹具配置的万能试验机(1 吨)进行了一系列拉伸试验。试样是根据生产要求制作的,如波浪形销钉和直销连杆。钢丝直径已被拉伸到最终直径,即 Φ8.0 毫米。从拉伸试验来看,屈服强度分别为 1165.8 兆帕和 1588.1 兆帕。由此可见,SUS 304 编织拉丝的强度已达到飞机紧固件制造所需的规格。所研究的 SUS 304 编织拉丝的安全系数高达 2.0。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Tensile Strength of Wire-Woven SUS 304 Austenitic Stainless Steel
In this paper, a series of tensile testing on wire drawing SUS 304 were conducted in order to meet the required specifications, thus, it can be utilized on the aircraft fighter components to remain stable and avoid shaking or vibration when the engine is operated. The studied material is expected to be used on flank airframes to improve its strength, wear resistance, corrosion, and aesthetic appearance. Series of tensile test has been conducted with universal testing machine (1 tonne) with modified jig configuration according to ASTM E8. The specimens were made according to the manufacture requirements such as wavy pin and straight pin connecting rod. The wire diameter has been drawing into the final diameter, which is Φ8.0 mm. From the tensile tests, yielding 1165.8 MPa and 1588.1 MPa, respectively. It is observed that the strength of woven SUS 304 wire drawing has reached the required specification to be manufactured in aircraft fastener. Factor of safety up to 2.0 has been acquired to the studied woven SUS 304 wire drawing.
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