BS 2G 215-1-1985 Nickel-chromium and nickel-aluminium thermocouple extension cables for aircraft Specification for conductors《飞机镍-铬和镍-铝热电偶延伸电缆 第1部分 导线规范》.pdf
《BS 2G 215-1-1985 Nickel-chromium and nickel-aluminium thermocouple extension cables for aircraft Specification for conductors《飞机镍-铬和镍-铝热电偶延伸电缆 第1部分 导线规范》.pdf》由会员分享,可在线阅读,更多相关《BS 2G 215-1-1985 Nickel-chromium and nickel-aluminium thermocouple extension cables for aircraft Specification for conductors《飞机镍-铬和镍-铝热电偶延伸电缆 第1部分 导线规范》.pdf(12页珍藏版)》请在麦多课文档分享上搜索。
1、BRITISH STANDARD AEROSPACE SERIES BS2G215-1: 1985 ISO8056-1: 1985 (Superseding British Standard G215:1972) Nickel-chromium and nickel-aluminium thermocouple extension cables for aircraft Part 1: Specification for conductors ISO title: Aircraft Nickel-chromium and nickel-aluminium thermocouple extens
2、ion cables Part1: Conductors General requirements and tests UDC 629.7:621.315.2 034.245:621.362.1BS2G215-1:1985 This British Standard, having been prepared under the directionof the Aerospace Standards Committee, was published under the authority ofthe Board of BSI and comesintoeffect on 31 December
3、1985 BSI 10-1999 The following BSI references relate to the work on this standard: Committee reference ACE/6 Draft for comment84/72756DC ISBN 0 580 14848 3 Committees responsible for this British Standard The preparation of this British Standard was entrusted by the Aerospace Standards Committee (AC
4、E/-) to Technical Committee ACE/6 upon which the following bodies were represented: BEAMA Ltd. British Rubber Manufacturers Association Civil Aviation Authority Electric Cable Makers Confederation Electronic Components Industry Federation Electronic Engineering Association Ministry of Defence Nation
5、al Supervising Inspectorate Society of British Aerospace Companies Limited Amendments issued since publication Amd. No. Date of issue CommentsBS2G215-1:1985 BSI 10-1999 i Contents Page Committees responsible Inside front cover National foreword ii 1 Scope and field of application 1 2 References 1 3
6、Conductor materials 1 4 Conductor construction 1 5 Tests 1 Annex Methods for determining thermo-e.m.f. ofconductorwiresagainstplatinum 3 Figure 1 E.M.F. measurement by method of direct comparison against platinum 5 Figure 2 E.M.F. measurement by method using a substandard 6 Table 1 Details of nickel
7、-chromium and nickel-aluminium conductors 2 Table 2 Thermo-electric characteristics of nickel-chromium and nickel-aluminium conductors against platinum 2 Table 3 D.C. resistances of nickel-chromium and nickel-aluminium 2 Publications referred to Inside back coverBS2G215-1:1985 ii BSI 10-1999 Nationa
8、l foreword This British Standard, has been prepared under the direction of the Aerospace Standards Committee. It is identical with ISO8056-1:1975 “Aircraft Nickel-chromium and nickel-aluminium thermocouple extension cables Part1:Conductors General requirements and tests” published by the Internation
9、al Organization for Standardization (ISO). It supersedes British Standard G215:1972 which is withdrawn, and takes account of international agreement by Technical Committee ISO/TC20 in relation to the requirements of nickel-chromium and nickel-aluminium thermocouple extension cables for aircraft. Thi
10、s standard is restricted to the requirements for the conductors for the cables whereas British Standard G215:1972 used to cover the conductor and the insulation requirements for the complete cables. It is intended to cover the complete cable requirements by amendments to the British Standard Aerospa
11、ce cable standards using this standard as a cross-reference to cover the conductors for thermocouple extension cables. Terminology and conventions. The text of the International Standard has been approved as suitable for publication as a British Standard without deviation. Some terminology and certa
12、in conventions are not identical with those used in British Standards; attention is drawn especially to the following. The comma has been used as a decimal marker. In British Standards it is current practice to use a full point on the baseline as the decimal marker. Where the words “part of ISO8056”
13、 appear, referring to this standard, they should be read as “Part of British Standard2G215”. IPTS68 International Practical Temperature Scale of1968 is obtainable from HMSO. A British Standard does not purport to include all the necessary provisions of a contract. Users of British Standards are resp
14、onsible for their correct application. Compliance with a British Standard does not of itself confer immunity from legal obligations. Cross-references International Standard Corresponding British Standard IEC Publication564:1977 BS5764:1979 Specification for d.c. bridges for measuring resistance (Ide
15、ntical) Summary of pages This document comprises a front cover, an inside front cover, pagesi andii, pages1 to6, an inside back cover and a back cover. This standard has been updated (see copyright date) and may have had amendments incorporated. This will be indicated in the amendment table on the i
16、nside front cover.BS2G215-1:1985 BSI 10-1999 1 1 Scope and field of application This part of ISO8056 specifies the design requirements and tests for the conductors of thermocouple extension cables, using nickel-chromium and nickel-aluminium, for installation in aircraft temperature indicator and con
17、trol systems. Methods for determining the thermo-e.m.f. of conductor wires against platinum are given in the Annex . 2 References IEC Publication564, D.C. bridges for measuring resistance. IPTS68, International Practical Temperature Scale of1968. 3 Conductor materials Conductors for use in the const
18、ruction of thermocouple extension cables for aircraft shall be manufactured from bright, annealed, nickel-chromium (non-magnetic) wires and bright, annealed, nickel-aluminium (magnetic) wires. They shall comply with the requirements specified in Table 1 in terms of d.c. resistance and those in Table
19、 2 in terms of thermo-e.m.f. characteristics against platinum over the appropriate temperature range. Table 3 shows the resistances which have been assumed for nickel-chromium and nickel-aluminium wires in the calculation of d.c. conductor resistances. A maximum increase in length of4%, as a result
20、of stranding, has been assumed for the wires of each conductor. Each reel or coil of wire to be used in the manufacture of the conductors shall be tested in accordance with5.1 and5.2. Finished conductors shall be tested in accordance with5.3 and5.4. Each reel or coil of wire to be used in the manufa
21、cture of the conductors shall be tested in accordance with5.1 and5.2. Finished conductors shall be tested in accordance with5.3 and5.4. 4 Conductor construction The positive conductor shall consist of stranded, bright, annealed, nickel-chromium alloy wires complying with the requirements of clause3.
22、 The negative conductor shall consist of stranded, bright, annealed, nickel-aluminium alloy wires complying with the requirements of clause3. Joints in single wires shall be welded, brazed or silver-soldered, but the complete conductor shall not be joined. There shall be no kinks, broken wires or ot
23、her irregularities in the conductors. 5 Tests 5.1 Thermo-electric tests on conductor wires All wires, before stranding, shall be shown to comply with the requirements specified in Table 2 with respect to thermo-e.m.f. against platinum 1)over the range of temperature appropriate to the cable under ma
24、nufacture. Measurements shall be made on sample lengths taken from both ends of each reel or coil of wire. Amethod of direct comparison against platinum, as described in clauseA.1, shall be used where single samples are to be tested. Where large numbers of samples are to be tested, a differential me
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