1、BS EN 6081:2016Aerospace series Rivet,universal head, close tolerance Inch seriesBSI Standards PublicationWB11885_BSI_StandardCovs_2013_AW.indd 1 15/05/2013 15:06BS EN 6081:2016 BRITISH STANDARDNational forewordThis British Standard is the UK implementation of EN 6081:2016.The UK participation in it
2、s preparation was entrusted to TechnicalCommittee ACE/12, Aerospace fasteners and fastening systems.A list of organizations represented on this committee can beobtained on request to its secretary.This publication does not purport to include all the necessaryprovisions of a contract. Users are respo
3、nsible for its correctapplication. The British Standards Institution 2016.Published by BSI Standards Limited 2016ISBN 978 0 580 92080 6ICS 49.030.60Compliance with a British Standard cannot confer immunity fromlegal obligations.This British Standard was published under the authority of theStandards
4、Policy and Strategy Committee on 30 September 2016.Amendments/corrigenda issued since publicationDate T e x t a f f e c t e dBS EN 6081:2016EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 6081 September 2016 ICS 49.030.60 English Version Aerospace series - Rivet, universal head, close tolerance
5、 - Inch series Srie arospatiale - Rivets de prcision, tte universelle - Srie en inches Luft- und Raumfahrt - Vollniet, Universalkopf, enge Toleranz - Zoll-Reihe This European Standard was approved by CEN on 2 January 2016. CEN members are bound to comply with the CEN/CENELEC Internal Regulations whi
6、ch 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 CEN-CENELEC Management Centre or to any CEN member. This Eu
7、ropean Standard exists 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
8、are the national standards 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,
9、Romania, Slovakia, 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 2016 CEN All rights of exploitation in any form an
10、d by any means reserved worldwide for CEN national Members. Ref. No. EN 6081:2016 EBS EN 6081:2016EN 6081:2016 (E) 2 Contents Page European foreword 3 1 Scope 4 2 Normative references 4 3 Requirements 5 3.1 Configuration, dimensions, tolerances and mass 5 3.2 Material and surface treatment 5 4 Desig
11、nation 7 5 Marking . 8 5.1 Material identification . 8 5.2 Manufacturers identification 8 6 Technical specification 8 6.1 Titanium alloy rivet 8 6.2 Aluminium alloy rivet 8 BS EN 6081:2016EN 6081:2016 (E) 3 European foreword This document (EN 6081:2016) has been prepared by the Aerospace and Defence
12、 Industries Association of Europe - Standardization (ASD-STAN). After enquiries and votes carried out in accordance with the rules of this Association, this European Standard has received the approval of the National Associations and the Official Services of the member countries of ASD, prior to its
13、 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, at the latest by March 2017, and conflicting national standards shall be withdrawn at the latest by March 2017. Attention is drawn to the possi
14、bility 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 identifying any or all such patent rights. According to the CEN-CENELEC Internal Regulations, the national standards organizations of the following countries ar
15、e bound to implement this European Standard: 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, Po
16、rtugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and the United Kingdom. BS EN 6081:2016EN 6081:2016 (E) 4 1 Scope This European Standard specifies the dimensions, tolerances and mass of rivets with universal head, close tolerance, inch series, for aerospace application. 2 Nor
17、mative 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 (including any amendments
18、) applies. EN 2115, Aerospace series Aluminium alloy 2117-T42 Wire for solid rivets D 10 mm 1) EN 2116, Aerospace series Aluminium alloy 2017A-T42 Wire for solid rivets D 10 mm 2)EN 2117, Aerospace series Aluminium alloy AL-P5056A (5056A)-H32 Wire for solid rivets D 10 mm 2)EN 2424, Aerospace series
19、 Marking of aerospace products EN 3115, Aerospace series Aluminium alloy 7050-T73 Wire for solid rivets D 10 mm 3) EN 6104, Aerospace series Rivets, solid, in aluminium or aluminium alloy Inch series Technical specification 3)EN 6118, Aerospace series Process specification Aluminium base protection
20、for fasteners 1)ISO 8080, Aerospace Anodic treatment of titanium and titanium alloys Sulfuric acid process SAE AMS 4982, Titanium alloy wire 44.5 Cb 4) MIL-C-5541, Chemical conversion coatings on aluminium and aluminium alloys 5)NASM 5674, Rivets, structural, aluminium alloy, titanium columbium allo
21、y, general specification for 6) 1)In preparation at the date of publication of this European Standard. 2)Published as ASD-STAN standard at the date of publication of this European Standard. 3)Published as ASD-STAN Prestandard at the date of publication of this European Standard. 4)Published by: Soci
22、ety of Automotive Engineers (SAE), 400 Commonwealth Drive, Warrendale, PA 15096-0001. 5)Published by: Department of Defense (DoD), the Pentagon, Washington, D.C. 20301. 6)Published by: Aerospace Industries Association of America, Inc. (AIA), 1250 Eye Street, N.W., Washington, D.C. 20005-3924, USA BS
23、 EN 6081:2016EN 6081:2016 (E) 5 3 Requirements 3.1 Configuration, dimensions, tolerances and mass The configuration shall conform with Figure 1. The dimensions, tolerances and mass shall conform with Figure 1 and Tables 1, 2 and 3. Dimensions and tolerances are expressed in millimetres. 3.2 Material
24、 and surface treatment See Table 3. Key 1 marking (see Clause 5) a0,025 mm shank diameter increase is permissible within 2,54 mm of the base of the head. bChamfered ends with radius to the R3dimensions or a 20 chamfer to “S” dimension. cMaximum head diameters are to theoretical sharp corners as meas
25、ured by projection. Figure 1 Configuration Table 1 Diameter code D Nominal diameter A B e R1 R2 R3 S + 0,03 0,03 max. min. + 0,25 0 Ref. null 0,25 null 0,25 2 1,60 3,35 3,05 0,7 0,4 1,4 0,1 to 0,15 0,48 0,41 3 2,38 4,95 4,65 1,0 0,6 2,1 0,74 0,58 4 3,18 6,58 6,22 1,4 0,8 2,7 0,99 0,79 5 3,97 8,18 7,
26、82 1,7 1,0 3,4 1,24 0,99 6 4,76 9,78 9,42 2 1,2 4,2 1,5 1,19 7 5,56 11,41 10,99 2,4 1,4 4,9 1,75 1,37 8 6,36 13,01 12,59 2,7 1,6 5,5 1,98 1,57 10 7,93 16,21 15,79 3,4 2,0 6,9 2,49 1,98 12 9,53 19,51 18,59 4,1 2,4 8,3 2,97 2,39 BS EN 6081:2016EN 6081:2016 (E) 6 Table 2 Length code and masses Lengtha,
27、bDiameter code 2 3 4 5 6 7 8 10 12 codeL null 0,25 Mass c kg/ 1 000 parts 03 4,76 0,04 0,08 0,15 04 6,35 0,04 0,10 0,19 0,31 05 7,94 0,05 0,12 0,22 0,37 0,54 0,96 06 9,53 0,06 0,14 0,26 0,42 0,62 1,07 1,45 07 11,11 0,07 0,16 0,29 0,48 0,70 1,18 1,59 2,19 08 12,70 0,08 0,18 0,33 0,53 0,78 1,29 1,74 2
28、,41 3,67 09 14,29 0,09 0,20 0,37 0,59 0,86 1,39 1,88 2,63 3,99 10 15,88 0,10 0,22 0,40 0,65 0,94 1,50 2,02 2,85 4,31 12 19,05 0,12 0,26 0,47 0,76 1,10 1,72 2,31 3,29 4,95 14 22,23 0,14 0,30 0,55 0,87 1,26 1,94 2,59 3,73 5,59 16 25,40 0,16 0,34 0,62 0,98 1,42 2,16 2,87 4,17 6,23 18 28,58 0,69 1,09 1,
29、58 2,37 3,16 4,61 6,87 20 31,75 0,72 1,15 1,66 2,48 3,30 4,83 7,19 22 34,93 0,76 1,20 1,74 2,59 3,44 5,05 7,51 24 38,10 0,80 1,26 1,82 2,70 3,58 5,27 7,83 28 44,45 1,31 1,90 2,81 3,73 5,50 8,15 32 50,80 1,37 1,98 2,92 3,87 5,72 8,47 40 63,50 3,03 4,01 5,94 8,79 48 76,20 4,15 6,16 9,11 aIntermediate
30、lengths can be created, e.g. 11/16 inch (11,2 mm) corresponds to length code 11. bAdditional 0,8 mm (1/32 inch) length increments may be obtained by adding code 5 after the last digit of part number cMass = 2,79 kg/dm3BS EN 6081:2016EN 6081:2016 (E) 7 Table 3 Diameter code Surface treatment Density
31、kg/dm3Multiplicator of mass (see Table 2) Material code 2 3 4 5 6 7 8 10 12 Material Aluminium alloy 2117-T4 per EN 2115 Yellow chromated per MIL-C-5541, class 1A 2,75 0,98 AD Aluminium alloy 2017A-H13 per EN 2116 2,79 1 D Aluminium alloy 5056A-H32 per EN 2117 2,64 0,95 B Aluminium alloy AL-P7050 pe
32、r EN 3115 2,82 1,01 KE Titanium alloy 44.5 Cb heat treat: annealed per AMS 4982 Anodized per ISO 8080 5,8 2,08 T IVD per EN 6118 V 4 Designation EXAMPLE Description block RIVET Identity block EN6081D6-06-5 Number of this standard Material code (see Table 3) Diameter code (see Table 1) Length code (s
33、ee Table 2) (1/16 of an inch)* Additional length code (see Table 2) (1/16 of an inch plus 1/32 inch)* * For supplying purpose only, see footnotes aand bin Table 2. NOTE If necessary, the code I9005 shall be placed between the description block and the identity block. BS EN 6081:2016EN 6081:2016 (E)
34、8 5 Marking 5.1 Material identification Symbol on the head see Figure 2. EN 2115 EN 2116 EN 2117 AMS 4982 indented embossed embossed indented 0,2 mm max. 0,2 mm max. 0,2 mm max. 0,2 mm max. EN 3115 embossed 0,2 mm max. Figure 2 Material identification 5.2 Manufacturers identification EN 2424, style
35、F to be embossed or indented on rivet head. Manufacturers identification is required on rivet heads for diameter code 4 and larger. 6 Technical specification 6.1 Titanium alloy rivet TiCb rivets shall conform with the requirements of NASM 5674 except for the finish as stated. 6.2 Aluminium alloy riv
36、et Aluminium alloy rivets shall conform with the requirements of EN 6104. This page deliberately left blankBSI is the national body responsible for preparing British Standards and other standards-related publications, information and services.BSI is incorporated by Royal Charter. British Standards a
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