欢迎来到麦多课文档分享! | 帮助中心 海量文档,免费浏览,给你所需,享你所想!
麦多课文档分享
全部分类
  • 标准规范>
  • 教学课件>
  • 考试资料>
  • 办公文档>
  • 学术论文>
  • 行业资料>
  • 易语言源码>
  • ImageVerifierCode 换一换
    首页 麦多课文档分享 > 资源分类 > PDF文档下载
    分享到微信 分享到微博 分享到QQ空间

    AECMA PREN 3475-506-2006 Aerospace Series Cables Electrical Aircraft Use Test Methods Part 506 - Plating Continuity Edition P 2《航天系列 飞行器用的电缆试验方法.第506部分.镀层连续性》.pdf

    • 资源ID:420343       资源大小:102.78KB        全文页数:4页
    • 资源格式: PDF        下载积分:2000积分
    快捷下载 游客一键下载
    账号登录下载
    微信登录下载
    二维码
    微信扫一扫登录
    下载资源需要2000积分(如需开发票,请勿充值!)
    邮箱/手机:
    温馨提示:
    如需开发票,请勿充值!快捷下载时,用户名和密码都是您填写的邮箱或者手机号,方便查询和重复下载(系统自动生成)。
    如需开发票,请勿充值!如填写123,账号就是123,密码也是123。
    支付方式: 支付宝扫码支付    微信扫码支付   
    验证码:   换一换

    加入VIP,交流精品资源
     
    账号:
    密码:
    验证码:   换一换
      忘记密码?
        
    友情提示
    2、PDF文件下载后,可能会被浏览器默认打开,此种情况可以点击浏览器菜单,保存网页到桌面,就可以正常下载了。
    3、本站不支持迅雷下载,请使用电脑自带的IE浏览器,或者360浏览器、谷歌浏览器下载即可。
    4、本站资源下载后的文档和图纸-无水印,预览文档经过压缩,下载后原文更清晰。
    5、试题试卷类文档,如果标题没有明确说明有答案则都视为没有答案,请知晓。

    AECMA PREN 3475-506-2006 Aerospace Series Cables Electrical Aircraft Use Test Methods Part 506 - Plating Continuity Edition P 2《航天系列 飞行器用的电缆试验方法.第506部分.镀层连续性》.pdf

    1、ASD STANDARD NORME ASD ASD NORM prEN 3475-506 Edition P 2 September 2006 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATION Gulledelle 94 - B-1200 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 763 3565 - www.asd-stan.orgICS: 49.060 Supersedes issue P 1 of Augus

    2、t 1992 and will supersede EN 3475-506:2002 Descriptors: ENGLISH VERSION Aerospace series Cables, electrical, aircraft use Test methods Part 506: Plating continuity Srie arospatiale Cbles lectriques usage aronautique Mthodes dessais Partie 506 : Continuit du revtement Luft- und Raumfahrt Elektrische

    3、Leitungen fr Luftfahrtverwendung Prfverfahren Teil 506: Gleichmaigkeit des berzugs This “Aerospace Series“ Prestandard has been drawn up under the responsibility of ASD-STAN (The AeroSpace and Defence Industries Association of Europe - Standardization). It is published for the needs of the European

    4、Aerospace Industry. It has been technically approved by the experts of the concerned Domain following member comments. Subsequent to the publication of this Prestandard, the technical content shall not be changed to an extent that interchangeability is affected, physically or functionally, without r

    5、e-identification of the standard. After examination and review by users and formal agreement of ASD-STAN, it will be submitted as a draft European Standard (prEN) to CEN (European Committee for Standardization) for formal vote and transformation to full European Standard (EN). The CEN national membe

    6、rs have then to implement the EN at national level by giving the EN the status of a national standard and by withdrawing any national standards conflicting with the EN. Edition approved for publication 30 September 2006 Comments should be sent within six months after the date of publication to ASD-S

    7、TAN Electrical Domain Copyright 2006 by ASD-STAN Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3475-506:20062 Contents Page Foreword2 1 Scope 3

    8、 2 Normative references 3 3 Preparation of specimens.3 3.1 General3 3.2 Strands before stranding or screening .3 3.2.1 Copper strands 3 3.2.2 Copper-clad aluminum strands3 3.3 Strands after stranding or screening.4 3.3.1 General4 3.3.2 Copper conductors or copper screens .4 3.3.3 Copper-clad aluminu

    9、m conductors .4 4 Method 4 5 Requirements.4 Foreword This standard was reviewed by the Domain Technical Coordinator of ASD-STANs Electrical Domain. After inquiries and votes carried out in accordance with the rules of ASD-STAN defined in ASD-STANs General Process Manual, this standard has received a

    10、pproval for Publication. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3475-506:20063 1 Scope This standard specifies a method of verifying the

    11、 continuity of plating on strands which are: either checked before stranding or screening, or checked after stranding or screening It shall be used together with EN 3475-100. 2 Normative references The following referenced documents are indispensable for the application of this document. For dated r

    12、eferences, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 3475-100, Aerospace series Cables, electrical, aircraft use Test methods Part 100: General. ASTM B 33-81, Standard specification for tinned soft or

    13、annealed copper wire for electrical purposes. 1)ASTM B 298-99, Standard specification for silver-coated soft or annealed copper wire. 1)ASTM B 355-95, Standard specification for nickel-coated soft or annealed copper wire. 1)3 Preparation of specimens 3.1 General The ASTM B 33 or ASTM B 298 or ASTM B

    14、 355 plating continuity test method applies to single end wires taken before stranding or before screening. Thus the applicability of the polysulfide test is restricted by the ASTM in recognition of the abrasion to the wire inherent in the stranding or in the screening process. 3.2 Strands before st

    15、randing or screening 3.2.1 Copper strands Prepare three strands at least 150 mm long as specimens and carefully straighten them by hand. Degrease the strands without damaging them and wipe them with a clean dry cloth. After cleaning, the strands shall not be touched with bare fingers. The length of

    16、the specimen which is immersed shall be at least 110 mm. 3.2.2 Copper-clad aluminum strands Prepare three strands at least 150 mm long as specimens. 1) Published by: American Society for Testing and Materials (ASTM), 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, USA. Copyrigh

    17、t Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3475-506:20064 Degrease the strands without damaging them and wipe them with a clean dry cloth. After cle

    18、aning, the strands shall not be touched with bare fingers. By using gloves, wind five turns of each strand on a mandrel which diameter is about 12 times the strand diameter. NOTE Due to hardness differences between, aluminium, copper and coating (particularly nickel) materials and possible associate

    19、d drawbacks during strand drawings after plating, turns are necessary to reveal possible weakness. 3.3 Strands after stranding or screening 3.3.1 General Due to the above restriction by the ASTM in recognition of the abrasion to the wire inherent in the stranding or in the screening process, the fol

    20、lowing preparation of specimens apply when testing stranded or screened product: 1) Unilay or Concentric constructions to be tested as the whole conductor 2) Two members from each layer of rope constructions to be tested after they have been carefully removed from the finished rope 3) Screen to be t

    21、ested as whole conductor after it has been carefully separated from cable jacket and from inner core(s) 3.3.2 Copper conductors or copper screens Prepare three samples at least 150 mm long as specimens. Degrease the specimens without damaging them and wipe them with a clean dry cloth. After cleaning

    22、, the specimens shall not be touched with bare fingers. The length of the specimen which is immersed shall be at least 110 mm. 3.3.3 Copper-clad aluminum conductors Prepare three samples at least 150 mm long as specimens. Degrease the specimens without damaging them and wipe them with a clean dry cl

    23、oth. After cleaning, the specimens shall not be touched with bare fingers. By using gloves, wind five turns of each conductor on a mandrel which diameter is about 12 times the conductor diameter. 4 Method Place the specimens for 30 s in a sodium polysulphide solution which has a density of 1,142 g/c

    24、m3at 20 C, then wash them carefully in distilled water. In addition, for silver plating, the samples shall then be immersed for 15 s in a solution of hydrochloric acid which has a density of 1,088 g/cm3at 20 C. The specimens shall then be washed carefully again in distilled water. 5 Requirements Exa

    25、mination shall occur immediately after the solution cycle. There shall be no adherent or distinctly visible black spots when examined with the naked eye. Any blackening occurring less than 15 mm from each end shall be disregarded. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-


    注意事项

    本文(AECMA PREN 3475-506-2006 Aerospace Series Cables Electrical Aircraft Use Test Methods Part 506 - Plating Continuity Edition P 2《航天系列 飞行器用的电缆试验方法.第506部分.镀层连续性》.pdf)为本站会员(priceawful190)主动上传,麦多课文档分享仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知麦多课文档分享(点击联系客服),我们立即给予删除!




    关于我们 - 网站声明 - 网站地图 - 资源地图 - 友情链接 - 网站客服 - 联系我们

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1 

    收起
    展开