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HB 5501-1983 平头抗剪环槽铆钉

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基本信息
标准名称:平头抗剪环槽铆钉
替代情况:替代HB 5501-1980 HB 5502-1980
发布日期:1984-05-31
实施日期:1984-07-01
首发日期:1900-01-01
作废日期:1900-01-01
出版日期:1900-01-01
适用范围

附加编制说明

前言

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所属分类: 机械 加工工艺 焊接与切割
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基本信息
标准名称:软式透水管
英文名称:Flexible permeable hose
中标分类: 建材 >> 建材产品 >> 建筑用塑料制品
ICS分类: 建筑材料和建筑物 >> 建筑物中的设施 >> 下水道系统
发布部门:中华人民共和国国家发展和改革委员会
发布日期:2004-10-20
实施日期:2005-04-01
首发日期:1900-01-01
作废日期:1900-01-01
提出单位:中国建筑材料工业协会
归口单位:建筑材料工业技术监督研究中心
起草单位:同济大学铁道与城市轨道交通研究院路基与土工技术研究所等
起草人:周顺华、韩国军、杨镇夏、杨斌、杨明昌、邱敏钟、黄力、蒋才荣、徐益鑫
出版社:中国标准出版社
出版日期:1900-01-01
页数:7页
适用范围

本标准规定了软式透水管的术语和定义、产品规格与标记、原材料、技术要求、试验方法、检验规
则以及标志、包装、运输、贮存等。
本标准适用于铁路、公路、机场、港口、水利、电力、矿山、房建、市政、地下工程等排除渗透水、降低地下水位及水土保持所用的软式透水管。

前言

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目录

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引用标准

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所属分类: 建材 建材产品 建筑用塑料制品 建筑材料和建筑物 建筑物中的设施 下水道系统
Product Code:SAE ARP4118
Title:Isolation and Corrosion Protection of Dissimilar Materials
Issuing Committee:Ams G9 Aerospace Sealing Committee
Scope: This SAE Aerospace Recommended Practice (ARP) provides methods and guidelines for isolating dissimilar repair patch materials from carbon composite structure during a repair operation.These procedures are applicable to any repair procedure for carbon composite parts in which the repair patch is a metallic alloy that can form a galvanic cell with carbon in the presence of moisture or other electrolytes. The principal patch materials addressed are aluminum, titanium, and stainless steel.The procedures are primarily concerned with bolted repairs that introduce the most severe, potential corrosion problem but bonded repairs are also considered.The procedures are also applicable to repairs that involve reinstallation of metallic inserts into a carbon composite part.Fiberglass and aramid composites do not have galvanic reactions with other materials, and the procedures outlined herein are, therefore, not essential with these materials. The sealing procedures covered herein are still recommended, however, as a means of preventing moisture entry. Boron filaments can produce a galvanic reaction by contact between the tungsten core of the fiber and adjacent metal, particularly in a bolted repair where the metal fasteners can contact cut fibers. Thus, the procedures outlined herein are advisable for bolted repairs of boron composites.Generic materials and parts are described herein with no specific vendor identifications. All materials used in the procedures outlined herein shall be accompanied by a Material Safety Data Sheet (MSDS) and shall be handled in accordance with MSDS instructions.
Rationale: This SAE Aerospace Recommended Practice (ARP) provides methods and guidelines for isolating dissimilar repair patch materials from carbon composite structure during a repair operation.These procedures are applicable to any repair procedure for carbon composite parts in which the repair patch is a metallic alloy that can form a galvanic cell with carbon in the presence of moisture or other electrolytes. The principal patch materials addressed are aluminum, titanium, and stainless steel.The procedures are primarily concerned with bolted repairs that introduce the most severe, potential corrosion problem but bonded repairs are also considered.The procedures are also applicable to repairs that involve reinstallation of metallic inserts into a carbon composite part.Fiberglass and aramid composites do not have galvanic reactions with other materials, and the procedures outlined herein are, therefore, not essential with these materials. The sealing procedures covered herein are still recommended, however, as a means of preventing moisture entry. Boron filaments can produce a galvanic reaction by contact between the tungsten core of the fiber and adjacent metal, particularly in a bolted repair where the metal fasteners can contact cut fibers. Thus, the procedures outlined herein are advisable for bolted repairs of boron composites.Generic materials and parts are described herein with no specific vendor identifications. All materials used in the procedures outlined herein shall be accompanied by a Material Safety Data Sheet (MSDS) and shall be handled in accordance with MSDS instructions.