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现行 EN 3388:2009
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Aerospace series - Fasteners, externally threaded, in heat resisting nickel base alloy NI-PH2601 (Inconel 718) - Classification 1 275 MPa/650 °C - Manufacturing method optional - Technical specification 航空航天系列 - 紧固件 外螺纹 耐热镍基合金NI-PH2601(Inconel 718) - 分类1 275 MPa/650°C - 制造方法可选 - 技术规格
发布日期: 2009-04-08
实施日期: 2009-04-08
本标准规定了室温下材料NI-PH2601(Inconel 718)的拉伸强度等级为1 275 MPa,材料最高试验温度650°C的外螺纹紧固件的技术和质量保证要求。 本文规定的外螺纹紧固件可以通过机械加工制造,也可以通过制造商的选择进行锻造来制造,如果锻造不需要控制谷物流动。 主要用于航空航天应用,当在产品标准或图纸上引用时,它适用于这种外螺纹紧固件
This standard specifies the technical and quality assurance requirements for externally threaded fasteners in material NI-PH2601 (Inconel 718) of tensile strength class 1 275 MPa at room temperature, maximum test temperature of material 650 °C. The externally threaded fasteners specified herein may be manufactured by machining from bar or by forging at the manufacturer's option, if forged there is no requirement for control of grainflow. Primarily for Aerospace applications it is applicable to such externally threaded fasteners when referenced on the product standard or drawing.
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现行
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DIN EN 3388
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航空航天系列.耐高温镍基合金NI-PH2601(Inconel 718)制外螺纹紧固件.等级:1 275 MPa/650°C.可选制造方法.技术规范;德语和英语版本EN 3388:2009
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