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 3373-001-2006 Aerospace Series Terminal Lugs and In-Line Splices for Crimping on Electric Conductors Part 001 Technical Specification Edition P 3《航空航天系列终端接线片和卷曲电力电缆轴向接合..pdf

    • 资源ID:420207       资源大小:203.45KB        全文页数:23页
    • 资源格式: PDF        下载积分:5000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5000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 3373-001-2006 Aerospace Series Terminal Lugs and In-Line Splices for Crimping on Electric Conductors Part 001 Technical Specification Edition P 3《航空航天系列终端接线片和卷曲电力电缆轴向接合..pdf

    1、ASD STANDARD NORME ASD ASD NORM prEN 3373-001 Edition P 3 May 2006 PUBLISHED BY AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATION Gulledelle 94 - B-1200 Brussels - Tel. + 32 2 775 8110 - Fax. + 32 2 775 8111 - www.asd-stan.orgICS: 49.060 Supersedes edition P 2 November 1999 De

    2、scriptors: ENGLISH VERSION Aerospace series Terminal lugs and in-line splices for crimping on electric conductors Part 001: Technical specification Srie arospatiale Cosses et prolongateurs pour sertissage sur conducteurs lectriques Partie 001 : Spcification technique Luft- und Raumfahrt Kabelschuhe

    3、und Stoverbinder zum Crimpen von elektrischen Leitern Teil 001: Technische Lieferbedingungen This “Aerospace Series“ Prestandard has been drawn up under the responsibility of ASD-STAN (Aerospace and Defence Industries Association of Europe - Standardization). It is published for the needs of the Eur

    4、opean 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, wit

    5、hout re-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

    6、 members 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 31 May 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 3373-001:20062 Foreword This standard was review

    8、ed 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 approval for Publication. Contents Page 1 Scope . 3 2 Normative references 3 3

    9、 Terms and definitions . 3 4 General. 3 4.1 Physical characteristics . 3 4.2 Functional characteristics . 4 4.2.1 Recommended cables 4 4.2.2 Crimping tools. 4 5 Tests 4 5.1 General. 4 5.2 Special tests. 4 5.2.1 Crimping at low temperature 4 5.2.2 Sleeve strength. 5 5.2.3 Sealing 5 5.2.4 Flammability

    10、. 5 5.3 Qualification tests for crimped connections on copper cable. 5 5.4 Qualification tests for crimped connections on aluminium cable . 12 6 Quality assurance 14 6.1 General. 14 6.2 Initial qualification conditions. 14 6.2.1 General. 14 6.2.2 Sampling and definition of samples. 14 6.2.3 Preparat

    11、ion of specimens 15 6.2.4 Programme of qualification tests. 22 6.3 Acceptance and inspection conditions 23 6.4 Quality control. 23 6.5 Maintaining qualification . 23 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo re

    12、production or networking permitted without license from IHS-,-,-prEN 3373-001:20063 1 Scope This standard specifies the general characteristics, the conditions of qualification, acceptance and quality assurance, as well as the test programs and groups for terminal lugs and in-Iine splices designed f

    13、or crimping on copper and copper alloy conductors and on aluminium and aluminium alloy conductors. 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 lates

    14、t edition of the referenced document (including any amendments) applies. IEC publication 50, International Electrotechnical Vocabulary Chapter 581: Electromechanical components for electronic equipment. EN 2083, Aerospace series Copper or copper alloy conductors for electrical cables Product standar

    15、d. EN 2242, Aerospace series Control of tools used for crimping of electrical cables with conductors defined by EN 2083 and EN 2346. 1)EN 2591*, Aerospace series Elements of electrical and optical connection Test methods General. EN 3719, Aerospace series Aluminium or aluminium alloy conductors for

    16、electrical cables Product standard. 1)EN 9133, Aerospace series Quality management systems Qualification Procedure for aerospace standard parts. 3 Terms and definitions For the purposes of this document, the following terms and definitions apply. IEC publication 50, International Electrotechnical Vo

    17、cabulary Chapter 581: Electromechanical components for electronic equipment. 4 General 4.1 Physical characteristics The forms and dimensions, masses, materials and operating temperature ranges are defined in the product standards. * All its parts quoted in this standard. 1) Published as ASD Prestand

    18、ard at the date of publication of this standard. 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 3373-001:20064 4.2 Functional characteristics 4.

    19、2.1 Recommended cables The terminal lugs and in-line splices shall allow the correct connection (in accordance with EN 2242) of copper cables conforming to EN 2083 and of aluminium cables conforming to EN 3719. 4.2.2 Crimping tools The tools which are referred to in the product standards regarding t

    20、erminal lugs and in-line splices shall be designed so that: they ensure the correct positioning of the crimping area; they have a full closure mechanism which ensures that the crimping cycle is fully completed; the crimping operation does not damage the terminal lug or the in-line splice and does no

    21、t cause any significant burring; a reference mark identifying the gauge is made in the crimping area, if possible. 5 Tests 5.1 General Unless otherwise specified, the tests shall be selected from those in EN 2591. These tests are listed in Tables 1 and 3. The tests shall be carried out on each combi

    22、nation of gauge, material and plating of the crimp barrel crimped on the appropriate section of each type of cable (material and plating), for each type of crimping tool. When a crimping barrel is designed to accommodate a range of cables for a s specific type of tool or for a type or size of die or

    23、 stop, the tests shall be carried out on only the smallest and largest permitted cable sections. To rationalise the test procedures and avoid confusion between the tests for copper and aluminium cables, the tests have been grouped together, and are defined as Group Cu 0, Cu 1, Cu 2, etc. for copper

    24、cables and Group Al 0, AI 1, AI 2, etc. for aluminium cables. For the purposes of these groups, copper and copper alloy cables are included within test Groups Cu 0, Cu 1, Cu 2, etc. Likewise aluminium and aluminium alloy cables are included within the test Groups AI 0, AI 1, AI 2, etc. 5.2 Special t

    25、ests 5.2.1 Crimping at low temperature Keep the components (cable, terminal lugs or in-line splices and crimping tools) at a temperature of ( 15 2) C for 1 h, then crimp at that temperature. Keep the specimens at a temperature of ( 65 2) C for 1 h. Recover at (20 5) C for 1 h. Copyright Association

    26、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 3373-001:20065 5.2.2 Sleeve strength The insulating sleeve shall have a good grip on the terminal lug barrel before and

    27、 after crimping and, when held by a fork passed around the crimping barrel, the displacement shall not be more than 1 mm under an axial load of 35 N. 5.2.3 Sealing The cable shall be placed in a tube connected to a compressed air supply; the pressure shall be increased in 105Pa stages every 5 min up

    28、 to 2 105Pa and maintained at this value for 1 h (see Figure 1). The specimen shall be immersed with the end of the barrel approximately 50 mm below the water level. There shall not be any leakage in the crimping area. Key 1 60 mm to 100 mm 2 Terminal lug 3 Cable 4 Collar clamp 5 Compressed air supp

    29、ly pipe Figure 1 Assembly for the sealing test 5.2.4 Flammability The specimen shall be suspended in a still air chamber above a Bunsen burner with a 100 mm long tube and an internal diameter of (9,5 0,5) mm. The end of the 25 mm blue flame produced by the Bunsen burner shall be applied for 20 s to

    30、half the length of the insulation of the specimen. There shall be no flame or incandescence 15 s after the flame is withdrawn. 5.3 Qualification tests for crimped connections on copper cable See Table 1. NOTE Where a requirement for an individual test is not quoted, see Table 7 for sequence of furth

    31、er tests. 3145 2 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 3373-001:20066 Table 1 Designation of the test Details EN 2591-101 Visual examin

    32、ation With the naked or normally corrected eye on crimped specimens. An optical magnification of 6 to 10 may be used if required. Check that: the combined section of cable/barrel size or in-line splice/crimping tool conforms; the form and position of crimping are correct; there are no major cracks o

    33、r burrs on the barrel; the cable core is correctly inserted in the barrel; the cable core and insulation are not damaged; the identification marks stamped on the crimp by the die are correct (if applicable). EN 2591-102 Examination of dimensions and mass Before crimping, dimensions and masses shall

    34、conform to the requirements of the product standard. EN 2591-206 Measurement of insulation resistance The insulation resistance measured between the outer surface of the insulating sleeve and the cable core shall be a minimum of 1 000 M. EN 2591-217 Voltage drop under specified current for terminal

    35、lugs and in-line splices See Figures 2 and 3. EN 2591-218 Ageing of terminal lugs and in-line splices by temperature and current cycling Test current as per Table 2. Requirement: see EN 2591-218. EN 2591-219 Voltage strength for insulated terminal lugs and in-line splices Test applicable to terminal

    36、 lugs and in-line splices with insulated barrels. Requirement see EN 2591-219. EN 2591-301 Endurance at temperature Method B. 120 h in a dry heat chamber at a temperature 15 C above the operating temperature of the terminal lug or in-line splice. Test applicable terminal lugs and in-line splices wit

    37、h insulated barrels. EN 2591-305 Rapid change of temperature TA= operating temperature of the terminal lug or in-line splice plus 15 C TB= 65 C EN 2591-307 Salt mist 48 h unless otherwise specified in the product standard. Check that no flaking of the protective treatment has occurred. continued Cop

    38、yright 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 3373-001:2006 7 Table 1 (concluded) Designation of the test Details EN 2591-314 Immersion at low air

    39、 pressure The in-line splice, fitted with its sealing accessories, shall be immersed in the solution. The ends of the cables shall protrude from the solution with neither the sealing accessories and the crimps being subjected to any stress. Pressure of chamber 4 kPa. EN 2591-315 Fluid resistance Tes

    40、t applicable to terminal lugs and in-line splices with insulated barrels. EN 2591-403 Sinusoidal and random vibration Method A. Assembly as per Figure 4. No sign of fracture. Applicable to terminal lugs only. EN 2591-417 Tensile strength (crimped connection) See Figure 5. The specimen shall not brea

    41、k at a value less than those specified in Table 2. EN 3373-001 Crimping at low temperature See 5.2.1. EN 3373-001 Sleeve strength See 5.2.2. EN 3373-001 Flammability See 5.2.4. Test applicable to terminal lugs and in-line splices with insulated barrels. Copyright Association Europeene des Constructe

    42、urs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3373-001:20068 Key 1 Reference cable 2 Measurement point 3 Supply terminal Figure 2 Assembly for measuring the voltage drop in terminal lugs in

    43、 accordance with EN 2591-217 L1500 min. L12UrUs213 500 min.3Copyright 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 3373-001:20069 Key 1 Reference cable

    44、2 Measurement point 3 Supply terminal Figure 3 Assembly for measuring the voltage drop in in-line splices in accordance with EN 2591-217 3 500 min.1L1Ur2 L1Us500 min. 2 3Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleN

    45、o reproduction or networking permitted without license from IHS-,-,-prEN 3373-001:200610 Key 1 Fixed point 2 Movement point 3 Attachment by nut and spring washer R = 5 external diameter of cable Figure 4 Assembly for the vibration test R 20 20 X YZR 1321Copyright Association Europeene des Constructe

    46、urs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3373-001:2006 11 Key 1 Upper jaws of tensile testing machine 2 Cable 3 In-line splice 4 Terminal lug 5 Lower jaws of tensile testing machine Fi

    47、gure 5 Principle of tensile testing machine 1 2 324 5 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 3373-001:200612 Table 2 Tensile strength an

    48、d voltage drop (copper conductor) Current cycling Measurementcurrent Maximum voltage drop for one crimp b Nominal section of the cables Minimum tensile strength cEN 2083 code mm2AWG a A A Initial mV After testing mV N 001 0,15 26 3,7 3 3 5 39 002 0,25 24 5,6 4,5 2 4 55 004 0,40 22 11,3 9 1 3 60 006 0,60 20 13,8 11 1 3 90 010 1 18 18 16 1 3 150 012 1,20 16 27,5 22 1 3 180 020 2 14 40 32 1 3 300 030 3 12 51,3 41 1 3 450 050 5 10 68,8 55 1 3 700 090 9 8 92,3 73 1 3 1 080140 14 6 126,3


    注意事项

    本文(AECMA PREN 3373-001-2006 Aerospace Series Terminal Lugs and In-Line Splices for Crimping on Electric Conductors Part 001 Technical Specification Edition P 3《航空航天系列终端接线片和卷曲电力电缆轴向接合..pdf)为本站会员(bowdiet140)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