HD 21 1 S2 A5-1990 AMD 5 Polyvinyl Chloride Insulated Cables of Rated Voltages up to and Including 450 750 V Part 1 General Requirements《修改件5 额定电压450 750 V以下的聚氯.pdf

上传人:花仙子 文档编号:1340785 上传时间:2019-10-20 格式:PDF 页数:4 大小:90.86KB
下载 相关 举报
HD 21 1 S2 A5-1990 AMD 5 Polyvinyl Chloride Insulated Cables of Rated Voltages up to and Including 450 750 V Part 1 General Requirements《修改件5 额定电压450 750 V以下的聚氯.pdf_第1页
第1页 / 共4页
HD 21 1 S2 A5-1990 AMD 5 Polyvinyl Chloride Insulated Cables of Rated Voltages up to and Including 450 750 V Part 1 General Requirements《修改件5 额定电压450 750 V以下的聚氯.pdf_第2页
第2页 / 共4页
HD 21 1 S2 A5-1990 AMD 5 Polyvinyl Chloride Insulated Cables of Rated Voltages up to and Including 450 750 V Part 1 General Requirements《修改件5 额定电压450 750 V以下的聚氯.pdf_第3页
第3页 / 共4页
HD 21 1 S2 A5-1990 AMD 5 Polyvinyl Chloride Insulated Cables of Rated Voltages up to and Including 450 750 V Part 1 General Requirements《修改件5 额定电压450 750 V以下的聚氯.pdf_第4页
第4页 / 共4页
亲,该文档总共4页,全部预览完了,如果喜欢就下载吧!
资源描述

1、I Teletex 206 2210097 - CENCEL - Tx i72210097 (* 32 21 519 68.71 - Fax: (+ 32 2) 519 69.19 I I Amendment 5 Issue 1 1990-11-13 Polyvinyl chloride insulated cables of rated voltages up o and including 4501750 V Part 1: General requirements Conducteurs et cibles isols au Polyvinylchlorid-isolierte Leit

2、ungen polychlorure de vinyle, de tension mit Nennspannungen bis 4501750 V nominale au plus gale a 4501750 V Teil 1: Allgemeine Anforderungen Premire partie: Prescriptions gnrales RD: IEC 227-1:1979; IEC/SC 208 (not appended) This amendment consists of the following: - Title Page Related to Directive

3、 73/23/EEC - Text prepared by CENELEC Technical Committee TC 20 date of ratification : 1990-06-11 date of announcement : 1990-12-01 date of withdrawal : 1991-06-01 date of latest publication : 1991-06-01 LIST OF NATIONAL STANDARDS IS GIVEN OVERLEAF riARflONIZE0 NATIONAL STANDARDS HO 21.1 52 Amendme

4、nt 5 AT : BE : CH : DE : DK : ES : FI : FR : GI3 : GR : IE : IS : IT : LU : NOS NL : NO : PT : SE : PENELEC u =-e .Je Classarl. 35 - C50 aruxelles -91 r * 32 2i St9 68 71 - Fax (+ 32 2) 519 69 19 Teletex 206 2210087 - CENCEL - Tx 172210097 *21.1*S2 9C W 340Lf583 0003bh9pb HO 21. 1 52 Amendment 5 Nov

5、ember 1990 I ENGLISH VERSION Date of issue: 1990-11-13 doa: 1990-12-01 dog: 1991-06-01 dw: 1991-06-01 POLYVINYL CHLORIDE INSULATED CABLES OF RATED VOLTAGES UP TO AND INCLUDING 4501750 V PART 1: GENERAL REQUIREMENTS Conducteurs et cbles isoles au polychlorure de vinyle, de tension nominale au plus eg

6、ale 1 4501750 V Premire partie: Prescriptions gnrales Polyvinylchlorid-isolierte Leitungen mit Nennspannungen bis 4501750 V Teil 1: Allgemeine Anforderungen Amendment 5 to HO 21.1 S2 was prepared by CENELEC Technical Committee TC 20 and ratified by CENELEC on 1990-06-11. It correctstmodifies the Eng

7、lish version of HO 21.1 S2. The changes to be made to the HD are given overleaf. Copyright reserved to CENELEC members HD*23i 1i*S2 90 34134583 0003670 2 = 8 AMENDMENT 5 HD 21.1 S2 Add the following to Appendix 1: Guide to Use of Harmonized Types of Cables PART 8 Single core dual insulated cables fo

8、r Indoor Decorative Lighting Chains Clause 3 (H03VH7-H) For indoor decorative lighting chains Suitable for indoor fitted with E5 series connected lampholders Christmas Tree Lighting and having a maximum loading of 100 W. Unsuitable for outdoor usage of any type, or for industrial or agricultural buildings or for portable tools. Unsuitable for cooking or heating appliances. Unsuitable for use in damp premises.

展开阅读全文
相关资源
猜你喜欢
  • NASA NACA-TN-1977-1949 Summary of the theoretical lift damping-in-roll and center-of-pressure characteristics of various wing plan forms at supersonic speeds《在超音速下 多个机翼平面升力 滚转阻尼和压力.pdf NASA NACA-TN-1977-1949 Summary of the theoretical lift damping-in-roll and center-of-pressure characteristics of various wing plan forms at supersonic speeds《在超音速下 多个机翼平面升力 滚转阻尼和压力.pdf
  • NASA NACA-TN-2001-1956 Aerodynamic characteristics of damping screens《阻尼屏幕的空气动力特性》.pdf NASA NACA-TN-2001-1956 Aerodynamic characteristics of damping screens《阻尼屏幕的空气动力特性》.pdf
  • NASA NACA-TN-2010-1950 Effect of horizontal tail on low-speed static lateral stability characteristics of a model having 45 degree sweptback wing and tail surfaces《水平尾翼对带有45后掠翼和尾翼面.pdf NASA NACA-TN-2010-1950 Effect of horizontal tail on low-speed static lateral stability characteristics of a model having 45 degree sweptback wing and tail surfaces《水平尾翼对带有45后掠翼和尾翼面.pdf
  • NASA NACA-TN-2069-1950 Cylinder-head temperatures and coolant heat rejection of a multicylinder liquid-cooled engine of 1650-cubic-inch displacement《1 650 in3位移且多汽缸的液体冷却发动机的汽缸头温度和冷.pdf NASA NACA-TN-2069-1950 Cylinder-head temperatures and coolant heat rejection of a multicylinder liquid-cooled engine of 1650-cubic-inch displacement《1 650 in3位移且多汽缸的液体冷却发动机的汽缸头温度和冷.pdf
  • NASA NACA-TN-2080-1950 Wind-tunnel investigation at low speed of an unswept untapered semispan wing of aspect ratio 3 13 equipped with various 25-percent-chord plain flaps《装配有多个25%.pdf NASA NACA-TN-2080-1950 Wind-tunnel investigation at low speed of an unswept untapered semispan wing of aspect ratio 3 13 equipped with various 25-percent-chord plain flaps《装配有多个25%.pdf
  • NASA NACA-TN-2114-1950 Theoretical lift and damping in roll of thin wings with arbitrary sweep and taper at supersonic speeds supersonic leading and trailing edges《在超音速下 带有任意掠角和锥形薄.pdf NASA NACA-TN-2114-1950 Theoretical lift and damping in roll of thin wings with arbitrary sweep and taper at supersonic speeds supersonic leading and trailing edges《在超音速下 带有任意掠角和锥形薄.pdf
  • NASA NACA-TN-2146-1950 On the effect of subsonic trailing edges on damping in roll and pitch of thin sweptback wings in a supersonic stream《关于亚音速机翼后缘对在超音速流下薄后掠翼滚动和倾斜阻尼的影响》.pdf NASA NACA-TN-2146-1950 On the effect of subsonic trailing edges on damping in roll and pitch of thin sweptback wings in a supersonic stream《关于亚音速机翼后缘对在超音速流下薄后掠翼滚动和倾斜阻尼的影响》.pdf
  • NASA NACA-TN-2169-1950 Wind-tunnel investigation at low speed of a 45 degree sweptback untapered semispan wing of aspect ratio 1 59 equipped with various 25-percent chord plain fla.pdf NASA NACA-TN-2169-1950 Wind-tunnel investigation at low speed of a 45 degree sweptback untapered semispan wing of aspect ratio 1 59 equipped with various 25-percent chord plain fla.pdf
  • NASA NACA-TN-2175-1950 Effect of an unswept wing on the contribution of unswept-tail configuration to the low-speed static and rolling-stability derivatives of a midwing airplane m.pdf NASA NACA-TN-2175-1950 Effect of an unswept wing on the contribution of unswept-tail configuration to the low-speed static and rolling-stability derivatives of a midwing airplane m.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