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TB/T 2075.19-1990 电气化铁道接触网零件 横承力索线夹

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基本信息
标准名称:电气化铁道接触网零件 横承力索线夹
中标分类: 铁路 >> 牵引供电 >> 接触网零件
替代情况:TB 1321-1978;被TB/T 2075.3-2002代替
发布日期:
实施日期:2002-08-01
首发日期:
作废日期:
出版日期:
页数:2页
适用范围

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前言

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目录

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引用标准

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所属分类: 铁路 牵引供电 接触网零件
【英文标准名称】:Transportablerefillableweldedsteelcylindersforliquefiedpetroleumgas(LPG)-Designandconstruction;GermanversionEN1442:1998/A2:2005
【原文标准名称】:液化石油气(LPG)用可移动可再充装焊接钢瓶.设计和建造
【标准号】:DINEN1442/A2-2005
【标准状态】:作废
【国别】:德国
【发布日期】:2005-06
【实施或试行日期】:
【发布单位】:德国标准化学会(DIN)
【起草单位】:
【标准类型】:()
【标准水平】:()
【中文主题词】:
【英文主题词】:
【摘要】:
【中国标准分类号】:J74
【国际标准分类号】:23_020_30
【页数】:6P;A4
【正文语种】:德语


Product Code:SAE AS7471
Title:Bolts and Screws, Nickel Alloy, UNS N07001 Tensile Strength 165 ksi, Corrosion and Heat Resistant, Procurement Specification
Issuing Committee:E-25 General Standards For Aerospace And Propulsion Systems
Scope: This procurement specification covers bolts and screws made from a corrosion and heat resistant, age hardenable nickel base alloy of the type identified under the Unified Numbering System as UNS N07001. The following specification designations and their properties are covered:AS7471165 ksi minimum ultimate tensile strength at room temperature. 75 ksi stress-rupture strength at 1350 °F.AS7471-1165 ksi minimum ultimate tensile strength at room temperature . 99 ksi minimum ultimate shear strength at room temperature.Primarily for aerospace propulsion systems applications where a good combination of tensile strength, and resistance to relaxation at elevated temperatures up to approximately 1500 °F is required.
Rationale: This procurement specification covers bolts and screws made from a corrosion and heat resistant, age hardenable nickel base alloy of the type identified under the Unified Numbering System as UNS N07001. The following specification designations and their properties are covered:AS7471165 ksi minimum ultimate tensile strength at room temperature. 75 ksi stress-rupture strength at 1350 °F.AS7471-1165 ksi minimum ultimate tensile strength at room temperature . 99 ksi minimum ultimate shear strength at room temperature.Primarily for aerospace propulsion systems applications where a good combination of tensile strength, and resistance to relaxation at elevated temperatures up to approximately 1500 °F is required.