FORD EST-M1L103-A-2003 COPPER WIRE - BATTERY CABLE - #3 GAGE TO BE USED WITH FORD WSS-M99P1111-A 《电池电缆用铜丝》.pdf

上传人:syndromehi216 文档编号:746632 上传时间:2019-01-14 格式:PDF 页数:2 大小:69.90KB
下载 相关 举报
FORD EST-M1L103-A-2003 COPPER WIRE - BATTERY CABLE - #3 GAGE  TO BE USED WITH FORD WSS-M99P1111-A  《电池电缆用铜丝》.pdf_第1页
第1页 / 共2页
FORD EST-M1L103-A-2003 COPPER WIRE - BATTERY CABLE - #3 GAGE  TO BE USED WITH FORD WSS-M99P1111-A  《电池电缆用铜丝》.pdf_第2页
第2页 / 共2页
亲,该文档总共2页,全部预览完了,如果喜欢就下载吧!
资源描述

1、 ENGINEERING MATERIAL SPECIFICATION Material Name Specification Number Date Action Revisions 2003 04 29 Revised Para 3.0 inserted; Para 3.9 & 4 deleted 1978 08 30 Metricated & Retyped 1976 09 14 Released HG2-00NA-250 Orig./s/K. GillisPrinted copies are uncontrolled Page 1 of 2 Copyright 2003, Ford G

2、lobal Technologies, Inc. COPPER WIRE - BATTERY CABLE - #3 GAGE EST-M1L103-A 1. SCOPE The material defined by this specification is stranded insulated battery cable. 2. APPLICATION This specification was released originally for battery cables on heavy duty installations. 3. REQUIREMENTS 3.0 STANDARD

3、REQUIREMENTS FOR PRODUCTION MATERIALS Material suppliers and part producers must conform to the Companys Standard Requirements For Production Materials (WSS-M99P1111-A). 3.1 CABLE SIZES The finished cable diameter shall not exceed 0.48 in (12.2 mm). 3.2 CABLE QUALITY Shall meet all the requirements

4、listed herein and must be equal to the original approved samples. 3.3 CABLE CONSTRUCTION Shall consist of 518 strands (nominal of #30 gage round wire layed in rope construction and served with 1 x 0.003 in (25.4 x 0.08 mm) minimum paper tape with 12-1/2% minimum overlap. Absolute minimum number of s

5、trands at any one time to be 515. No individual group is to contain more than 20% of the total strands. Minimum area is 51 548 cmil (26.12 mm2). 3.4 WIRE QUALITY The conductor strands prior to stranding or bunching shall consist of bare ESF-M2L1-A, soft or annealed round copper wire. 3.5 INSULATION

6、COLOR Black, unless otherwise specified on the engineering drawing. ENGINEERING MATERIAL SPECIFICATION EST-M1L103-A Page 2 of 2 Copyright 2003, Ford Global Technologies, Inc. 3.6 INSULATION QUALITY The neoprene or vinyl-nitrile insulation must meet all basic SAE J 558 type SGR requirements and have

7、a nominal wall thickness of 0.080 in (2.03 mm). 3.7 RESISTIVITY at 20 C, max 211 /ft (692 /m) 3.8 PHYSICAL AND ELECTRICAL PROPERTIES Three samples of cable are required. One for high temperature, low temperature and oil absorption tests. All samples are subjected to the dielectric breakdown test at

8、the completion of their respective tests. These samples are 24 in (0.6 m) in length with 1 in (25 mm) of insulation stripped from both ends. 3.8.1 High Temperature Resistance Suspend sample over a 10 in (254 mm) mandrel with a 6 lb (2.72 kg) weight at each end. Soak at 121 +/- 1 C for 120 h in a cir

9、culating air oven. Cool to room temperature, remove the weight and bend the sample around the mandrel in a reverse direction at a rate not exceeding 1 turn per minute until a 180 bend is completed. Insulation shall not fracture or split. 3.8.2 Low Temperature Resistance Lower the temperature on a st

10、raight piece of sample to -34 C at a rate not to exceed 68 C per minute. Hold for 3 h and then wrap around a 10 in (254 mm) mandrel at 6 turns per minute for 180. Insulation shall not fracture. 3.8.3 Oil Absorption Resistance Immerse sample to within 1-1/2 in (38 mm) from the ends into a solution of

11、 50% kerosene, 50% SAE 10W engine oil for 20 h at 49 +/- 1 C. The cable diameter shall not increase more than 15%. Wrap sample around a 10 in (254 mm) mandrel for 180. Insulation shall not fracture or split. 3.8.4 Dielectric Resistance Join exposed ends of sample and immerse loop to within 6 in (150 mm) of ends in a 5% salt bath (salt content weight at 27 C). Soak 5 h and then apply 500V (RMS) 60 cps (Hz) between sample conductor and salt bath for 1 minute. Insulation shall not rupture.

展开阅读全文
相关资源
猜你喜欢
  • DIN 65567-1992 Aerospace reinforcement fibres determination of finish content of aramid filament yarns woven fabrics and chopped strands《航空航天 增强纤维 芳族聚酰胺长丝纱 织物和短切原丝的整理剂含量的测定》.pdf DIN 65567-1992 Aerospace reinforcement fibres determination of finish content of aramid filament yarns woven fabrics and chopped strands《航空航天 增强纤维 芳族聚酰胺长丝纱 织物和短切原丝的整理剂含量的测定》.pdf
  • DIN 65568-1992 Aerospace reinforcement fibres determination of thermal oxidative resistance of carbon filament yarns woven fabrics and short cuts《航空航天 增强纤维 碳素长丝纱、织物和短切原丝的耐热氧化性能的测定》.pdf DIN 65568-1992 Aerospace reinforcement fibres determination of thermal oxidative resistance of carbon filament yarns woven fabrics and short cuts《航空航天 增强纤维 碳素长丝纱、织物和短切原丝的耐热氧化性能的测定》.pdf
  • DIN 65569-1-1992 Aerospace reinforcement fibres determination of density of filament yarns sink-float method《航空航天 增强纤维 复丝纱密度的测定 悬浮法》.pdf DIN 65569-1-1992 Aerospace reinforcement fibres determination of density of filament yarns sink-float method《航空航天 增强纤维 复丝纱密度的测定 悬浮法》.pdf
  • DIN 65569-2-1992 Aerospace reinforcement fibres determination of density of filament yarns hydrostatic weighing method《航空航天 增强纤维 复丝纱密度的测定 流体比重秤量法》.pdf DIN 65569-2-1992 Aerospace reinforcement fibres determination of density of filament yarns hydrostatic weighing method《航空航天 增强纤维 复丝纱密度的测定 流体比重秤量法》.pdf
  • DIN 65570-1990 Aerospace heat treatment facilities general requirements《航空航天 热处理设施 一般要求》.pdf DIN 65570-1990 Aerospace heat treatment facilities general requirements《航空航天 热处理设施 一般要求》.pdf
  • DIN 65571-1-1992 Aerospace reinforcement fibres determination of filament diameter and cross-sectional area of filament yarns calculation method《航空航天 增强纤维 复丝纱横截面面积和复丝纱直径的测定 计算方法》.pdf DIN 65571-1-1992 Aerospace reinforcement fibres determination of filament diameter and cross-sectional area of filament yarns calculation method《航空航天 增强纤维 复丝纱横截面面积和复丝纱直径的测定 计算方法》.pdf
  • DIN 65571-2-1992 Aerospace reinforcement fibres determination of filament diameter of filament yarns longitudinal projection method《航空和航天 增强纤维 复丝纱直径的测定 纵向投影法》.pdf DIN 65571-2-1992 Aerospace reinforcement fibres determination of filament diameter of filament yarns longitudinal projection method《航空和航天 增强纤维 复丝纱直径的测定 纵向投影法》.pdf
  • DIN 65571-3-1992 Aerospace reinforcement fibres determination of filament diameter cross-sectional shape and area of filament yarns measurement of transverse micro-section《航空航天 增强纤.pdf DIN 65571-3-1992 Aerospace reinforcement fibres determination of filament diameter cross-sectional shape and area of filament yarns measurement of transverse micro-section《航空航天 增强纤.pdf
  • DIN 65571-4-1992 Aerospace reinforcement fibres determination of filament diameter of filament yarns laser interferometry《航空航天 增强纤维 复丝纱的长丝直径的测定 激光干涉测量法》.pdf DIN 65571-4-1992 Aerospace reinforcement fibres determination of filament diameter of filament yarns laser interferometry《航空航天 增强纤维 复丝纱的长丝直径的测定 激光干涉测量法》.pdf
  • 相关搜索

    当前位置:首页 > 标准规范 > 国际标准 > 其他

    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