BS 3G 100-2 3 5-1972 Specification for general requirements for equipment for use in aircraft - All equipment - Environmental conditions - Explosion-proofness《航空器设备的一般要求规范 第2部分 全部设.pdf
《BS 3G 100-2 3 5-1972 Specification for general requirements for equipment for use in aircraft - All equipment - Environmental conditions - Explosion-proofness《航空器设备的一般要求规范 第2部分 全部设.pdf》由会员分享,可在线阅读,更多相关《BS 3G 100-2 3 5-1972 Specification for general requirements for equipment for use in aircraft - All equipment - Environmental conditions - Explosion-proofness《航空器设备的一般要求规范 第2部分 全部设.pdf(14页珍藏版)》请在麦多课文档分享上搜索。
1、BRITISH STANDARD AEROSPACE SERIES BS 3G 100-2.3.5:1972 Specification for General requirements for equipment in aircraft Part 2: All equipment Section 3: Environmental conditions Subsection 3.5: Explosion-proofness UDC 629.7.05/.06:629.7.067.8.001.4BS 3G 100-2.3.5:1972 This British Standard, having b
2、een approved by the Aerospace Industry Standards Committee, was published under the authority of the Executive Board of the Institution on 14 June 1972 BSI 12-1999 The following BSI references relate to the work on this standard: Committee reference ACE/58 Draft for comment 70/26885 ISBN 0 580 07163
3、 4 Amendments issued since publication Amd. No. Date of issue CommentsBS3G100-2.3.5:1972 BSI 12-1999 i Contents Page Foreword ii 1 Scope 1 2 Definitions and terms 1 2.1 Explosion proof 1 2.2 Enclosure 1 2.3 Intrinsically safe 1 3 Equipment design 1 3.1 Equipment design and construction 1 3.2 Integri
4、ty of protection 1 4 Categories of equipment and enclosure for various environments 1 4.1 General 1 4.2 Environments 1 4.3 Categories 2 5 Explosion-proofness requirements 2 5.1 Environment I 2 5.2 Environment IIa 2 5.3 Environment IIb 2 5.4 Environment III 2 5.5 Environment IV 2 5.6 Alternative requ
5、irements 2 6 Tests 2 6.1 General requirements 2 6.2 Test specimens 2 6.3 Test mixtures 2 6.4 Acceptance tests 2 6.5 Test equipment and test procedures 3 7 Information to be stated in the relevant specification 4 Appendix A Recommendations for installations in areas where an explosion hazard may aris
6、e 8 Appendix B Numerical procedure for Category X enclosures 8 Figure 1 Apparatus for testing in explosive atmospheres 7 Table 1 Basic requirements for explosion-proof equipment 5 Table 2 Acceptable flange and hole dimensions for enclosure Categories C and D 7 Table 3 Composition of test mixtures 7B
7、S3G 100-2.3.5:1972 ii BSI 12-1999 Foreword This British Standard is part of a composite standard in the Aerospace Series of British Standards that specifies general requirements for equipment in aircraft. An introduction to the complete British Standard is given in BS 3G 100-0. This subsection of BS
8、 3G 100 replaces the explosion-proofness requirements specified in Clauses 221 and 222 of BS 2G 100-2. It details explosion-proofness requirements and in Appendix A the relevant installation recommendations, against which aircraft equipment should be designed for use in various environments. It also
9、 defines tests to demonstrate that the equipment complies with these explosion-proofness requirements. This standard makes reference to the following British Standards: BS 2G 100, General requirements for electrical equipment and indicating instruments for aircraft Part 2: Environmental and operatin
10、g conditions. BS 3G.100, General requirements for equipment in aircraft Part0:Introduction Part 1: Identification, declaration and construction Part2.3X: Sealing requirements 1) . BS 1259, Intrinsically safe electrical apparatus for use in explosive atmospheres. BS 4683, Electrical apparatus for exp
11、losive atmospheres Part: The construction and test of intrinsically safe electrical apparatus 1) . NOTEInformation concerning metric (SI) units is given in BS 350, “Conversion factors and tables”, and BS3763, “The International System of units (SI)”. A British Standard does not purport to include al
12、l the necessary provisions of a contract. Users of British Standards are responsible for their correct application. Compliance with a British Standard does not of itself confer immunity from legal obligations. Summary of pages This document comprises a front cover, an inside front cover, pages i and
13、 ii, pages 1 to 8 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 inside front cover. 1) In course of preparation.BS3G100-2.3.5:1972 BSI 12-1999 1 1 Scope This British Standard specif
14、ies design requirements for aircraft equipment that may come into contact with flammable fluids and vapours. It also specifies test requirements to demonstrate that the equipment meets these requirements. The standard does not relate to potentially dangerous environments occurring as a result of lea
15、kage from goods carried on board by passengers or as part of their baggage, or cargo, which may be the subject of separate regulations. It refers to normal and fault conditions occurring in categories of equipment in five types of environment. The standard should also be read in conjunction with BS
16、3G 100-0. 2 Definitions and terms For the purposes of this British Standard the following apply: 2.1 explosion proof equipment is explosion proof when there is negligible risk that it will cause an explosion of a flammable gas or vapour within the declared environment 2.2 enclosure a box or casing,
17、including any ducting, which is part of the equipment and not an aircraft compartment 2.3 intrinsically safe equipment is intrinsically safe when any spark or thermal effect produced normally (e.g. by. making or breaking a circuit) or accidentally (e.g. by a short circuit or earth fault) is incapabl
18、e, under prescribed test conditions, of causing ignition or a prescribed gas or vapour 3 Equipment design 3.1 Equipment design and construction. Equipment that may come into contact with flammable fluids or vapours and which 1) in normal operation 2)may produce arcs, sparks or hot surfaces, shall be
19、 so designed, having regard to its likely manner of installation, as to be explosion proof; 2) under fault conditions 2)may produce arcs, electrical sparks, friction sparks or hot surfaces, shall be so designed and installed as to reduce to an acceptable minimum the overall risk of a fault occurring
20、 such as to ignite the flammable vapours. 3.2 Integrity of protection. The required degree of protection under any condition of operation shall be achieved by means that are not dangerously affected by wear of the equipment and are not unduly dependent upon dimensional tolerances or accuracy of asse
21、mbly. NOTEAppendix A gives recommendations for the installation of electrical wiring and cennections, and the ventilation of equipment in areas that may be contaminated with flammable vapours. 4 Categories of equipment and enclosure for various environments 4.1 General. This clause details the basic
22、 requirements for explosion-proof equipment, discusses the risk of explosion in different environments and provides for various categories of enclosure (see Table 1). 4.2 Environments. The five environments. recognized by this standard are as follows: 1) Environment I. An atmosphere in a space in, w
23、hich uncovered flammable fluids or vapours exist, or can exist either continuously or intermittently by intention: e.g. in fuel tanks or within fuel systems. 2) Environment IIa. An atmosphere in which flammable mixtures can be expected to occur only as a result of spillage or leakage, and where an e
24、xplosive environment is likely to occur at a rate greater than one hour per hundred thousand flying hours; e.g. in the vicinity, of fuel systems. 3) Environment IIb. An atmosphere in which flammable mixtures can be expected to occur as a result of spillage or leakage, and when an explosive environme
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