EN 61823-2003 en Electrical installations for lighting and beaconing of aerodromes AGL series transformers《机场照明和信标导航用电气设备 AGL系列变压器 IEC 61823 2002修改件》.pdf

《EN 61823-2003 en Electrical installations for lighting and beaconing of aerodromes AGL series transformers《机场照明和信标导航用电气设备 AGL系列变压器 IEC 61823 2002修改件》.pdf》由会员分享，可在线阅读，更多相关《EN 61823-2003 en Electrical installations for lighting and beaconing of aerodromes AGL series transformers《机场照明和信标导航用电气设备 AGL系列变压器 IEC 61823 2002修改件》.pdf（26页珍藏版）》请在麦多课文档分享上搜索。

1、BRITISH STANDARD BS EN 61823:2003 Electrical installations for lighting and beaconing of aerodromes AGL series transformers The European Standard EN 61823:2003 has the status of a British Standard ICS 29.140.50; 93.120 BS EN 61823:2003 This British Standard was published under the authority of the S

2、tandards Policy and Strategy Committee on 14 August 2003 BSI 14 August 2003 ISBN 0 580 42437 5 National foreword This British Standard is the official English language version of EN 61823:2003. It was derived by CENELEC from IEC 61823:2002. The CENELEC common modifications have been implemented at t

3、he appropriate places in the text and are indicated by tags . The UK participation in its preparation was entrusted to Technical Committee EPL/97, Aeronautical ground lighting, which has the responsibility to: A list of organizations represented on this committee can be obtained on request to its se

4、cretary. Cross-references The British Standards which implement international or European publications referred to in this document may be found in the BSI Catalogue under the section entitled “International Standards Correspondence Index”, or by using the “Search” facility of the BSI Electronic Cat

5、alogue or of British Standards Online. This publication does not purport to include all the necessary provisions of a contract. Users are responsible for its correct application. Compliance with a British Standard does not of itself confer immunity from legal obligations. aid enquirers to understand

6、 the text; present to the responsible international/European committee any enquiries on the interpretation, or proposals for change, and keep the UK interests informed; monitor related international and European developments and promulgate them in the UK. Summary of pages This document comprises a f

7、ront cover, an inside front cover, the EN title page, pages 2 to 23 and a back cover. The BSI copyright notice displayed in this document indicates when the document was last issued. Amendments issued since publication Amd. No. Date CommentsEUROPEAN STANDARD EN 61823 NORME EUROPENNE EUROPISCHE NORM

8、June 2003 CENELEC European Committee for Electrotechnical Standardization Comit Europen de Normalisation Electrotechnique Europisches Komitee fr Elektrotechnische Normung Central Secretariat: rue de Stassart 35, B - 1050 Brussels 2003 CENELEC - All rights of exploitation in any form and by any means

9、 reserved worldwide for CENELEC members. Ref. No. EN 61823:2003 E ICS 29.140.50; 93.120 English version Electrical installations for lighting and beaconing of aerodromes - AGL series transformers (IEC 61823:2002, modified) Installations lectriques pour le balisage et lclairage des arodromes - Transf

10、ormateurs sries AGL (CEI 61823:2002, modifie) Elektrische Anlagen fr Beleuchtung und Befeuerung von Flugpltzen - Serienstromtransformatoren (IEC 61823:2002, modifiziert) This European Standard was approved by CENELEC on 2003-02-01. CENELEC members are bound to comply with the CEN/CENELEC Internal Re

11、gulations which stipulate the conditions for giving this European Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such national standards may be obtained on application to the Central Secretariat or to any CENELEC member.

12、This European Standard exists in three official versions (English, French, German). A version in any other language made by translation under the responsibility of a CENELEC member into its own language and notified to the Central Secretariat has the same status as the official versions. CENELEC mem

13、bers are the national electrotechnical committees of Austria, Belgium, Czech Republic, Denmark, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Luxembourg, Malta, Netherlands, Norway, Portugal, Slovakia, Spain, Sweden, Switzerland and United Kingdom. Foreword The text of document

14、 97/94/FDIS, future edition 1 of IEC 61823, prepared by IEC TC 97, Electrical installations for lighting and beaconing of aerodromes, was submitted to the IEC-CENELEC parallel vote and was approved by CENELEC as EN 61823 on 2003-02-01 together with common modifications prepared by the Technical Comm

15、ittee CENELEC TC 97. The following dates were fixed: latest date by which the EN has to be implemented at national level by publication of an identical national standard or by endorsement (dop) 2004-01-01 latest date by which the national standards conflicting with the EN have to be withdrawn (dow)

16、2006-02-01 Annexes designated “normative“ are part of the body of the standard. In this standard, annexes A and ZA are normative. Annex ZA has been added by CENELEC. _ Endorsement notice The text of the International Standard IEC 61823:2002 was approved by CENELEC as a European Standard with agreed

17、common modifications. Page2 EN61823:2003CONTENTS 1 Scope.5 2 Normative references.5 3 Definitions and abbreviated terms 5 3.1 Definitions.5 3.2 Abbreviated terms.6 4 General requirements.7 4.1 Classification.7 4.2 Rated current7 4.3 Earthing7 4.4 AGL construction.7 4.5 Encapsulation8 4.6 Earthing8 4

18、.7 Service conditions .8 4.8 Electrical characteristics8 4.9 Temperature rise.9 5 Type and routine tests10 5.1 Type tests.10 5.2 Routine tests.11 6 Test requirements11 6.1 Introduction to electrical testing.11 6.2 Tests under load .12 6.3 Short circuit current.13 6.4 Open circuit voltage13 6.5 AC le

19、akage current test.13 6.6 DC leakage current cycling test .15 6.7 Shock tests.16 6.8 Temperature rise.17 6.9 Gas tightness test .18 6.10 Physical size demonstration18 7 Routine tests18 7.1 Ratio test.18 7.2 Earth continuity test18 7.3 Leakage current test18 8 Marking19 Annex A (normative) Connector

20、descriptions and interface dimensions20 Annex ZA (normative) Normative references to international publications with their corresponding European publications .22 Bibliography23 Figure 1 Tests under load 12 Figure 2 Primary a.c. leakage current test14 Figure 3 Secondary a.c. leakage current test .14

21、 Figure 4 Primary d.c. leakage current 16 Page3 EN61823:2003Figure 5 Secondary d.c. leakage current16 Figure 6 Lead rigidity test 17 Figure A.1 Style 2 primary plug20 Figure A.2 Style 9 primary receptacle 20 Figure A.3 Style 8 secondary receptacle 21 Figure A.4 Style 7 secondary receptacle 21 Table

22、1 Transformer characteristics.9 Table 2 Encapsulation method type tests .10 Table 3 Electrical characteristic type tests .11 Table 4 Routine tests.11 Table 5 DC leakage current test limits15 Table A.1 Interface dimensions for Figures A.1 and A.2.20 Table A.2 Interface dimensions for Figures A.3 and

23、A.4.21 Page4 EN61823:2003ELECTRICAL INSTALLATIONS FOR LIGHTING AND BEACONING OF AERODROMES AGL SERIES TRANSFORMERS 1 Scope This standard specifies the characteristics of aeronautical ground lighting series transformers (AGLST) used in aeronautical ground lighting for 6,6 A series circuits, at a serv

24、ice voltage of up to 5 kV, supplied by constant current regulators up to 30 kVA in rating. AGL series transformers provide power to airport lighting luminaires or other loads (resistive) from their secondary circuits. The AGL series transformers provide continuity of the series circuit in the event

25、of a loss of the load on the transformer, and electrical isolation between the primary circuit supplied by a constant current regulator, and the secondary circuit connected to the load under conditions defined in this standard. An AGL series transformer is be able to withstand a permanent short or o

26、pen-circuit secondary series circuit. Specifications for similar series transformers intended for any primary or secondary currents other than 6,6 A, or to supply alternative voltages, constant power, reactive loads, etc., are not included in this standard. 2 Normative references The following refer

27、enced documents are indispensable for the application of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. IEC 60085, Thermal evaluation and classification of electrical insul

28、ation IEC 61822, Electrical installations for lighting and beaconing of aerodromes Constant current regulators ISO 48, Rubber, vulcanised or thermoplastic Determination of hardness (hardness between 10 IRHD and 100 IRHD) 3 Definitions and abbreviated terms 3.1 Definitions For the purposes of this st

29、andard the following definitions apply. Where the terms voltage and current are used, they shall be r.m.s. values unless otherwise stated. 3.1.1 AGL series transformer aeronautical ground lighting series transformer, as specified in this standard 3.1.2 ambient temperature the temperature of the air

30、or other medium surrounding the AGL series transformer; for testing purposes, a temperature of (20 5) C unless otherwise stated Page5 EN61823:20033.1.3 nominal power arbitrarily selected values of power used in this standard for convenience to refer to AGL series transformers with different characte

31、ristics 3.1.4 rated frequency the frequency or frequency range for which the AGL series transformer is designed to operate 3.1.5 rated power the range of powers for which each AGL series transformer is suitable. NOTE The low and high values of these ranges are given in Table 1. 3.1.6 rated primary c

32、urrent the current at which the primary of the AGL series transformer is designed to operate 3.1.7 rated secondary current the current at which the secondary of the AGL series transformer is designed to operate 3.1.8 routine test test for the purpose of checking manufactured products for compliance

33、with this standard 3.1.9 service voltage the maximum primary or secondary voltage at which the AGL series transformer is designed to operate 3.1.10 type test a test to confirm that the product design and production processes are capable of providing products that meet the requirements of this standa

34、rd 3.1.11 type test sample a sample consisting of one or more similar samples used for a type test 3.2 Abbreviated terms AC1 Source of mains power AC2 High voltage a.c. source AGLST AGL series transformer DC1 Source of d.c. power CCR Constant current regulator as specified in IEC 61822 I 1 , I 2Prim

35、ary and secondary currents respectively, as measured by ammeters or equivalent devices U 1 , U 2Primary and secondary voltages respectively, as measured by voltmeters or equivalent devices P 1 , P 2Active power measurements or calculations of respectively the primary and secondary circuits of an AGL

36、 series transformer Page6 EN61823:20034 General requirements 4.1 Classification There are seven types of AGL series transformers specified in this standard, defined by their nominal power, namely 30 W, 45 W, 65 W, 100 W, 150 W, 200 W and 300 W. See Table 1 for the required characteristics. 4.2 Rated

37、 current The rated primary and secondary currents shall be 6,6 A. 4.3 Earthing AGL series transformers may be provided with or without an earthing connection. 4.4 AGL construction The AGL series transformers shall have two electrically and physically separate windings, one primary and one secondary,

38、 wound on a magnetic core. The polarity of the windings shall be such that the primary plug corresponds to the large socket of the secondary receptacle (See Annex A.). All internal electrical connections shall be permanent, e.g. by compression high-pressure crimping, high-temperature soldering, weld

39、ing, etc. The shapes of the transformers are optional provided they meet all the requirements of this standard. Sharp edges shall be avoided. The AGL series transformer including all connector leads shall be able to be inserted through the open end of a cylinder 20 cm in diameter by 25 cm long, and

40、shall easily and totally fit inside such a cylinder. The transformers shall be designed so that they may be installed and will perform to the requirements of this standard in any orientation. The AGL series transformers shall be provided with two single-conductor primary leads and a two-conductor se

41、condary lead. 4.4.1 Primary connection leads The AGL series transformers shall be connected to the AGL primary series circuit cable by two insulated, multi-stranded, copper conductors, with at least a 6 mm 2cross section, and a length measured from the transformer housing to the face of the connecto

42、r of 60 10 0 + cm. The service voltage for the leads shall be 5 kV. One lead shall have a style 2 male plug at its end. The other lead shall have a style 9 female receptacle at its end. Unless otherwise agreed between the manufacturer and supplier, the connectors shall be provided with disposable sh

43、ipping caps. 4.4.2 Secondary connection lead The secondary lead shall consist of two insulated, multi-stranded, copper conductors with an overall jacket, each core of minimum cross section 2,5 mm 2 , minimum service voltage 600 V, and a length measured from the transformer housing to the face of the

44、 connector of 120 10 0 +cm. The lead shall have a type 2, class A, style 7 or style 8 female receptacle at its end. Unless otherwise agreed between the manufacturer and supplier, the connector shall be provided with a disposable shipping cap. Page7 EN61823:20034.5 Encapsulation The AGL series transf

45、ormer body, the connectors and the connection leads sheaths, shall be made of compatible materials. The case shall be composed of material formed directly on the core and coil assembly, or by compound filling a container. The transformer shall be permanently encapsulated without cracks, holes, or in

46、ternal voids as far as practical. The encapsulation of the transformer must form a watertight casing, and must bond with its connection leads so as to provide a completely waterproof assembly. The encapsulation material shall have a durometer hardness IRHD (Shore A) of not less than 55 as measured i

47、n accordance with the test method of ISO 48. The minimum thickness of the encapsulation over the internal components shall be 6,5 mm at all points of the surface, for any type of encapsulant. The encapsulation materials shall be capable of withstanding acid and alkaline soils, as well as limited exp

48、osure to chemicals typically present on the aerodrome, including but not limited to oil, gasoline, and de-icing fluids. The encapsulating materials must resist limited UV exposure. These characteristics may be confirmed by testing material samples (only). The characteristics may be confirmed by test

49、s sponsored by the transformer manufacturer, or by test results supplied by the materials manufacturer. These results may be applied to all AGL series transformers using the encapsulation material. If a transformer manufacturer uses more than one material for encapsulation, each such material shall meet these requirements. 4.6 Earthing The magnetic core shall not be connected to earth or to either of the primary or secondar