EN 4199-003-2014 en Aerospace series - Bonding straps for aircraft - Part 003 Bonding strap assemblies with flat braided conductor copper tin plated - 65 up to 150 and copper nicke.pdf

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1、BSI Standards PublicationBS EN 4199-003:2014Aerospace series Bondingstraps for aircraftPart 003: Bonding strap assemblies with flatbraided conductor copper, tin plated 65C up to 150 C and copper, nickel plated 65 C up to 260 C Product standardBS EN 4199-003:2014 BRITISH STANDARDNational forewordThis

2、 British Standard is the UK implementation of EN 4199-003:2014. It supersedes BS EN 4199-003:2009 which is withdrawn.The UK participation in its preparation was entrusted to Technical Committee ACE/6, Aerospace avionic electrical and fibre optic technology.A list of organizations represented on this

3、 committee can be obtained on request to its secretary.This publication does not purport to include all the necessary provisions of a contract. Users are responsible for its correct application. The British Standards Institution 2014. Published by BSI Standards Limited 2014ISBN 978 0 580 83459 2 ICS

4、 49.060 Compliance with a British Standard cannot confer immunity from legal obligations.This British Standard was published under the authority of the Standards Policy and Strategy Committee on 31 May 2014.Amendments issued since publicationDate T e x t a f f e c t e dBS EN 4199-003:2014EUROPEAN ST

5、ANDARD NORME EUROPENNE EUROPISCHE NORM EN 4199-003 April 2014 ICS 49.060 Supersedes EN 4199-003:2009English Version Aerospace series - Bonding straps for aircraft - Part 003: Bonding strap assemblies with flat braided conductor copper, tin plated - 65 C up to 150 C and copper, nickel plated - 65 C u

6、p to 260 C - Product standard Srie arospatiale - Tresses de mtallisation pour avion - Partie 003: Tresses assembles conducteur plat pour utilisation de - 65 C 150 C en cuivre tam et de - 65 C 260 C en cuivre nickel - Norme de produit Luft- und Raumfahrt - Masseverbinder fr Luftfahrzeuge - Teil 003:

7、Masseverbinder, konfektioniert, flache Geflechtleiter Kupfer, verzinnt - 65 C bis 150 C und Kupfer, vernickelt - 65 C bis 260 C - Produktnorm This European Standard was approved by CEN on 12 October 2013. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the c

8、onditions 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 CEN-CENELEC Management Centre or to any CEN member. This European Standard ex

9、ists in three official versions (English, French, German). A version in any other language made by translation under the responsibility of a CEN member into its own language and notified to the CEN-CENELEC Management Centre has the same status as the official versions. CEN members are the national s

10、tandards bodies of Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia,

11、 Slovenia, Spain, Sweden, Switzerland, Turkey and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG CEN-CENELEC Management Centre: Avenue Marnix 17, B-1000 Brussels 2014 CEN All rights of exploitation in any form and by any means res

12、erved worldwide for CEN national Members. Ref. No. EN 4199-003:2014 EBS EN 4199-003:2014EN 4199-003:2014 (E) 2 Contents Page Foreword 3 1 Scope 4 2 Normative references 4 3 Terms and definitions .4 4 Characteristics .4 5 Dimensions, mass and resistance .5 6 Quality assurance 7 7 Designation 8 8 Mark

13、ing .8 9 Packaging .8 BS EN 4199-003:2014EN 4199-003:2014 (E) 3 Foreword This document (EN 4199-003:2014) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN). After enquiries and votes carried out in accordance with the rules of this Associati

14、on, this Standard has received the approval of the National Associations and the Official Services of the member countries of ASD, prior to its presentation to CEN. This European Standard shall be given the status of a national standard, either by publication of an identical text or by endorsement,

15、at the latest by October 2014, and conflicting national standards shall be withdrawn at the latest by month year of October 2014. Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. CEN and/or CENELEC shall not be held responsible for

16、 identifying any or all such patent rights. This document supersedes EN 4199-003:2009. According to the CEN-CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech

17、Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and the United Kingdom.

18、BS EN 4199-003:2014EN 4199-003:2014 (E) 4 1 Scope This European Standard defines the characteristics of bonding straps with flat braided copper conductors tin or nickel plated and terminal lugs tin or nickel plated, crimped on both ends for use on aircraft. This standard shall be used together with

19、EN 4199-001. 2 Normative references The following documents, in whole or in part, are normatively referenced in this document and are indispensable for its application. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (includ

20、ing any amendments) applies. EN 2424, Aerospace series - Marking of aerospace products EN 3373-001, Aerospace series - Terminal lugs and in-line splices for crimping on electric conductors - Part 001: Technical specification EN 4199-001, Aerospace series - Bonding straps for aircraft - Part 001: Tec

21、hnical specification EN 4199-005, Aerospace series - Bonding straps for aircraft - Part 005: Flat braid conductors copper, tin plated -65 C up to 150 C and copper, nickel plated, -65 C up to 260 C - Product standard 3 Terms and definitions For the purposes of this document, the terms and definitions

22、 given in EN 4199-001 apply. 4 Characteristics 4.1 Temperature rating Flat braid copper conductors for bonding straps. Tin plated copper braid conductor and tin plated copper terminal lugs 65 C up to 150 C. Nickel plated copper braid conductor and nickel plated copper terminal lugs 65 C up to 260 C.

23、 4.2 Material and finish For flat braid copper conductor, see EN 4199-005. Flat braid copper conductor and terminal lugs shall have the same finish. The finish shall be either tin or nickel using the designation T or N. See designation in Clause 7. 4.3 Length restrictions For the electrical bonding

24、of structural elements likely to conduct lightening, braids longer than 220 mm are not generally approved and should not be used without the prior consent of the departments dealing with system studies and standardisation. BS EN 4199-003:2014EN 4199-003:2014 (E) 5 When using bonding straps on equipm

25、ent or installations generating or processing frequencies greater than 100 kHz, care shall be taken not to exceed a length to width ratio of 5 to 1 for reasons of electromagnetic compatibility. 4.4 Cross sectional area The nominal cross sectional area, plus the associated test currents and tensile s

26、trength requirements of the straps shall be in accordance with Table 1. Test currents and tensile strength figures are derived from EN 3373-001 Table 2. Table 1 Cross sectional area Cross section code Nominal braid cross sectional area Test current Tensile strength lug to lug mm2Amps N A 04 50 600 B

27、 06 60 800 C 10 80 1 200 D 16 110 1 700 E 25 150 2 200 5 Dimensions, mass and resistance 5.1 General Dimensions and tolerances are in millimetres. For length L and tolerances, see 5.2. For nominal braid width, see Table 3 and EN 4199-005. For mass and resistance, see Table 3. For d max. see Table 2.

28、 Figure 1 BS EN 4199-003:2014EN 4199-003:2014 (E) 6 5.2 Length Length shall be defined as the measurement between terminal hole centres as shown in Figure 1. Standard lengths shall be called up in multiples of 25 mm. Preferred lengths shall range from 50 mm up to 300 mm. Longer, non-preferred length

29、s are allowable as long as they are approved by the relevant design authority. A three or four digit length code is to be entered into the designation (see Clause 7). The following standard tolerances to length shall apply: 05+mm for lengths up to 100 mm; 010+mm for lengths 125 mm to 975 mm; 025+mm

30、for lengths of 1 000 mm and above. Nominal resistance and mass values for straps of 100 mm length are shown in Table 3. 5.3 Terminal selection Terminal variant availability is in accordance with Table 2. Only aerospace approved terminals shall be used. BS EN 4199-003:2014EN 4199-003:2014 (E) 7 Table

31、 2 Terminal selection Cross sectional area Terminal availability Terminal variant code Stud/Hole size Hole mm 4 6 10 16 25 A No. 8 4,34 X X X B No. 10 5,00 X X C 1/4 6,73 X D 5/16 8,33 X E 3/8 9,91 X X X Terminal barrel size AWG 12/10 8 6 4 2 d max. (see Figure 1) mm 13,8 14,6 16,2 16,2 16,2 5.4 Mas

32、s and resistance See Table 3. Table 3 Mass and resistance Braid x-section Nominal braid width Nominal resistance 100 mm strap Braid resistance Nominal mass 100 mm strap Braid mass mm2mm m m per 25 mm g g per 25 mm 4 8,2 0,4 0,112 6,3 1,1 6 10,0 0,24 0,075 10,7 1,63 10 14,0 0,14 0,046 18,4 2,9 16 17,

33、5 0,09 0,03 28,9 3,93 25 21,0 0,06 0,015 43,2 7,85 The figures shown in Table 3 are for nickel plated straps. For tin plated straps, resistance figures will be slightly lower. Mass figures will be comparable. For lengths other than 100m m, nominal resistance and mass can be calculated by adding or s

34、ubtracting multiples of the 25 mm braid figures quoted in Table 3. EXAMPLE 1 Resistance for a 10 mm2. 250 mm long strap = 0,14 m + (6 0,046) m = 0,416 m total nominal resistance. EXAMPLE 2 Mass for a 4 mm2. 50 mm long strap = 6,3 g 1,1 g = 5,2 g total nominal mass. For maximum figures, an additional

35、 10 % should be applied to the nominal values. Nominal values of mass are based on the use of typical terminals for each x-sectional area. BS EN 4199-003:2014EN 4199-003:2014 (E) 8 6 Quality assurance 6.1 Qualification See EN 4199-001, 7.2. Number of cycles for mechanical fatigue shall be 50 000 cyc

36、les. 6.2 Acceptance Tests See EN 4199-001, 7.4, Table 7. Test currents shall be in accordance with Table 1 above. Resistance and mass shall be in accordance with Table 3 above. Resistance is calculated from the millivolt drop readings measured from terminal palm to terminal palm using the method spe

37、cified in EN 4199-001, see 6.3. All measurements shall be taken at an ambient temperature of (20 5) C. 7 Designation EXAMPLE Description block STRAP BONDING Identity block EN 4199-003-X-XXX-XX-X Number of this standard Cross sectional area code (see Table 1) Length code in mm (I.E. 125) (In multiple

38、s of 25 mm. Four digits to be used if length exceeds 975 mm, see 5.2) Terminal variant code end 1 and 2 (see Table 2) Finish T = tin / N = nickel NOTE If necessary, the code I9005 shall be placed between the description block and the identity block. 8 Marking The marking of the bonding strap by labe

39、l on the packaging shall include: the designation as defined in this product standard; date of manufacture; the manufacturers name or monogram in accordance with EN 2424, style F. BS EN 4199-003:2014EN 4199-003:2014 (E) 9 9 Packaging Bonding straps shall be packed so as to avoid any damage. This pag

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