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

    ASD-STAN PREN 4710-02-2014 Aerospace series Quick release fastening systems for non-structural applications Part 02 Spring clamp stud combination (Edition P 1).pdf

    • 资源ID:453524       资源大小:87.35KB        全文页数:5页
    • 资源格式: PDF        下载积分:10000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10000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。

    ASD-STAN PREN 4710-02-2014 Aerospace series Quick release fastening systems for non-structural applications Part 02 Spring clamp stud combination (Edition P 1).pdf

    1、ASD-STAN STANDARD NORME ASD-STAN ASD-STAN NORM prEN 4710-02 Edition P 1 February 2014 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATIONRue Montoyer 10 - 1000 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 775 8131 - www.asd-stan.orgICS: Descriptors: ENGLISH VER

    2、SION Aerospace series Quick release fastening systems for non-structural applications Part 02: Spring clamp stud combination Srie arospatiale Fixations rapides filetes pour applications non-structurales Partie 02 : Combinaison de colliers lyre et pions Luft- und Raumfahrt Druckverschlsse nicht-struk

    3、turelle Anwendungen Teil 02: Federclip-Bolzen Kombination 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 Aerospace Industry. It ha

    4、s 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 re-identification of the s

    5、tandard. 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 members have then to implement

    6、 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 28 February 2014 Comments should be sent within six months after the date of publication to ASD-STAN Mechanical Domain Copy

    7、right 2014 by ASD-STAN prEN 4710-02:2014 (E) 2 Contents Page Foreword 2 1 Scope 3 2 Normative references 3 3 Representations . 3 4 Example of installation 5 Foreword This standard was reviewed by the Domain Technical Coordinator of ASD-STANs Mechanical Domain. After inquiries and votes carried out i

    8、n accordance with the rules of ASD-STAN defined in ASD-STANs General Process Manual, this standard has received approval for Publication. prEN 4710-02:2014 (E) 3 1 Scope This standard describes the compilation of the component system the spring clamp pin family for use in the fuselage interior equip

    9、ment and in the not structural or secondary structural area for aerospace applications. 2 Normative references The following referenced documents are indispensable for the application of this document. For dated references, only the edition cited applies. For undated references, the latest edition o

    10、f the referenced document (including any amendments) applies. EN 4710-01, Aerospace series Quick release fastening systems for non-structural applications Part 01: Technical specification 1)EN 4710-03, Aerospace series Quick release fastening systems for non-structural applications Part 03: Spring c

    11、lamp 1)EN 4710-04, Aerospace series Quick release fastening systems for non-structural applications Part 04: Spring clamp One way tolerance compensation1) EN 4710-05, Aerospace series Quick release fastening systems for non-structural applications Part 05: Spring clamp Two ways tolerance compensatio

    12、n 1) EN 4710-06, Aerospace series Quick release fastening systems for non-structural applications Part 06: Stud - quick-release and locking 1) EN 4710-07, Aerospace series Quick release fastening systems for non-structural applications Part 07: Retaining grommet 1) EN 10088-3, Stainless steels Part

    13、3: Technical delivery conditions for semi-finished products, bars, rods, wire, sections and bright products of corrosion resisting steels for general purposes EN 10132-4, Cold rolled narrow steel strip for heat treatment Technical delivery conditions Part 4: Spring steels and other applicationsEN 10

    14、151, Stainless steel strip for springs Technical delivery conditions EN 12165, Copper and copper alloys Wrought and unwrought forging stock 3 Representations Table 1 shows the different components of the quick release fastening systems for non-structural and lining applications including the differe

    15、nt family numbers of the standard EN 4710-03 to EN 4710-07. EN 4710-01 is reserved for the technical specification of the system. 1) Published as ASD-STAN Prestandard at the date of publication of this standard. http:/www.asd-stan.org/ prEN 4710-02:2014 (E) 4 Table 1 Types EN 4710- Figure Descriptio

    16、n Type Type code a Plate codes Material code 03 Spring Clamp CS CM CL 3 4 5 A = Alloy steel per EN 10132-4 S = Stainless steel per EN 10151 Fixed shift none 04 Spring Clamp Tolerace compensation Direction CTS CTM 3 4 A = Alloy steel per EN 10132-4 S = Stainless steel per EN 10151 shift (left right)

    17、05 Spring Clamp Tolerance compensation Direction CSM 5 A = Alloy steel per EN 10132-4 S = Stainless steel per EN 10151 shift (left right- up - down) 06 Stud quick release and locking PS PM PL C = Stainless steel per EN 10088-3 B = Copper alloy per EN 12165 turning 07 Grommet RS RM RL A = Silicone aO

    18、nly type code with the same end letter can be combined. Possible combinations are given through the type code small (xS), medium (xM) and large (xL). A sample of the CM/CSM/CTM, PM and RM combination can be found in chapter 4. prEN 4710-02:2014 (E) 5 4 Example of installation Figure 1 shows an examp

    19、le of installation of EN 4710-06 (1), EN 4710-07 (2) and EN 4710-03 to EN 4710-05 (3). Example of possible end letter combinations: CM (3), CTM (3) and CSM (3) can be combined with PM (1) and RM (2) Key 1 Stud as per EN 4710-06 (1) 2 Grommet as per EN 4710-07 (2) 3 Spring Clamp as per EN 4710-03 to EN 4710-05 (3) Figure 1 Example of installation


    注意事项

    本文(ASD-STAN PREN 4710-02-2014 Aerospace series Quick release fastening systems for non-structural applications Part 02 Spring clamp stud combination (Edition P 1).pdf)为本站会员(roleaisle130)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