1、BS EN 6080:2016Aerospace series Rivet,100 normal flush head, closetolerance Inch seriesBSI Standards PublicationWB11885_BSI_StandardCovs_2013_AW.indd 1 15/05/2013 15:06BS EN 6080:2016 BRITISH STANDARDNational forewordThis British Standard is the UK implementation of EN 6080:2016.The UK participation
2、 in its 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
3、 responsible for its correctapplication. The British Standards Institution 2016.Published by BSI Standards Limited 2016ISBN 978 0 580 92079 0ICS 49.030.60Compliance with a British Standard cannot confer immunity fromlegal obligations.This British Standard was published under the authority of theStan
4、dards 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 6080:2016EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 6080 September 2016 ICS 49.030.60 English Version Aerospace series - Rivet, 100 normal flush head, cl
5、ose tolerance - Inch series Srie arospatiale - Rivets de prcision, 100 tte fraise normale - Srie en inches Luft- und Raumfahrt - Vollniet, 100 Normaler Senkkopf, enge Toleranz - Zoll-Reihe This European Standard was approved by CEN on 2 January 2016. CEN members are bound to comply with the CEN/CENE
6、LEC Internal Regulations 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 CEN-CENELEC Management Centre o
7、r to any CEN member. 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 CEN member into its own language and notified to the CEN-CENELEC Management Centre has the same status as the off
8、icial versions. CEN members 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
9、, Norway, Poland, Portugal, 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
10、 exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 6080:2016 EBS EN 6080:2016EN 6080:2016 (E) 2 Contents Page European foreword 3 1 Scope 4 2 Normative references 4 3 Requirements 5 3.1 Configuration, dimensions, tolerances and masses 5 3.2 Material a
11、nd surface treatment 5 4 Designation 8 5 Marking . 8 5.1 Material identification . 8 5.2 Manufacturers identification . 9 6 Technical specification 10 6.1 Aluminium alloy rivet 10 6.2 Heat resisting alloy NI-PD9001 (NiCu31) rivets 10 6.3 Titanium alloy rivet 10 BS EN 6080:2016EN 6080:2016 (E) 3 Euro
12、pean foreword This document (EN 6080:2016) 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 Association, this European Standard has received the approval of the Nat
13、ional 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, at the latest by March 2017, and conflicting national
14、standards shall be withdrawn at the latest by March 2017. 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 identifying any or all such patent rights. According to the CEN-CENELEC
15、 Internal Regulations, the national standards organizations of the following countries are 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, Icela
16、nd, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and the United Kingdom. BS EN 6080:2016EN 6080:2016 (E) 4 1 Scope This European Standard specifies the dimensions, tolerances and masses of
17、 rivets with 100 normal flush head, close tolerance, inch series, for aerospace application. 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 applie
18、s. For undated references, the latest edition of the referenced document (including any amendments) 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 serie
19、s Aluminium alloy AL-P5056A (5056A)-H32 Wire for solid rivets D 10 mm 2)EN 2424, Aerospace series Marking of aerospace products EN 2941, Aerospace series Nickel alloy rivets Technical specification 3)EN 3115, Aerospace series Aluminium alloy 7050-T73 Wire for solid rivets D 10 mm 3) EN 4372, Aerospa
20、ce series Heat resisting nickel alloy with copper NI-PD9001 (NiCu31) Wire for solid rivets D 10 mm3) EN 6101, Aerospace series Rivet, 100 medium flush head, close tolerance Inch series3)EN 6104, Aerospace series Rivets, solid, in aluminium or aluminium alloy Inch series Technical specification 3)EN
21、6118, Aerospace series Process specification Aluminium base protection 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-A-8625, Anodic coatings for aluminum and aluminum alloys 5)MIL-C-5541, Ch
22、emical conversion coatings on aluminium and aluminium alloys 5)NAS 527, Inspection procedure for flush fasteners 6)NASM 5674, Rivets, structural, aluminium alloy, titanium columbium alloy, general specification for 6) 1)In preparation at the date of publication of this European Standard. 2)Published
23、 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: Society of Automotive Engineers (SAE), 400 Commonwealth Drive, Warrendale, PA 15096-0001. 5)Published by: Department o
24、f 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 EN 6080:2016EN 6080:2016 (E) 5 3 Requirements 3.1 Configuration, dimensions, tolerances and masses The configurat
25、ion shall conform with Figure 1. The dimensions, tolerances and masses shall conform with Figure 1 and Tables 1, 2 and 3. Dimensions and tolerances are expressed in millimetres. Key 1 marking (see Clause 5) a 0,025 mm increase of shank diameter is permissible within 2,54 mm of the base of the head.
26、b Chamfered ends with radius R1dimensions or a 20 chamfer to dimensions S. c Maximum head diameters are to theoretical sharp corners as measured by projection. d Head protrusion shall be tested in accordance with NAS 527. Figure 1 Configuration 3.2 Material and surface treatment See Table 4. BS EN 6
27、080:2016EN 6080:2016 (E) 6 Table 1 Dimensions and tolerances Diameter code D A A1 B C E F P R1 S W +0,03 0,03 max. min. min. Ref. +0,05 0 null0,13 max. min. null0,25 null0,25 max. min. 2 Use rivets according to EN 6101 3 4 5 3,97 7,25 7,15 6,79 1,35 0,08 0,08 to 0,15 5,29 0,706 0,650 1,24 0,99 5,588
28、 5,583 6 4,76 8,95 8,85 8,49 1,74 0,10 6,55 0,899 0,839 1,50 1,19 6,833 6,827 7 5,56 10,55 10,45 10,09 2,07 7,73 1,068 1,005 1,75 1,37 8,033 8,027 8 6,36 12,10 12,00 11,64 2,39 8,88 1,227 1,161 1,98 1,57 9,208 9,202 10 7,93 14,35 14,25 13,89 2,67 10,54 1,371 1,302 2,49 1,98 11,119 11,111 12 9,53 17,
29、65 17,55 17,19 3,39 13,05 1,682 1,608 2,97 2,39 13,684 13,676 Table 2 Length code and masses Lengtha,bDiameter code 2 3 4 5 c6 7 8 10 12 codeL null 0,254 Mass d kg/ 1 000 parts 03 4,76 Use rivets according to EN 6101 04 6,35 05 7,94 0,32 0,47 06 9,53 0,37 0,55 0,77 07 11,11 0,43 0,63 0,88 1,17 08 12
30、,70 0,49 0,71 0,99 1,32 09 14,29 0,54 0,79 1,10 1,46 2,31 10 15,88 0,60 0,87 1,21 1,60 2,53 3,82 12 19,05 0,71 1,03 1,42 1,88 2,98 4,46 14 22,23 0,82 1,19 1,64 2,17 3,42 5,10 16 25,40 0,93 1,35 1,86 2,45 3,86 5,74 18 28,58 1,04 1,51 2,08 2,74 4,30 6,38 20 31,75 1,15 1,67 2,29 3,02 4,74 7,02 22 34,93
31、 1,26 1,83 2,51 3,30 5,18 7,66 24 38,10 1,38 1,99 2,73 3,59 5,62 8,30 28 44,45 1,60 2,31 3,16 4,16 6,50 9,58 32 50,80 1,82 2,63 3,60 4,72 7,38 10,86 40 63,50 4,47 5,86 9,16 13,42 48 76,20 7,00 10,91 15,98 aIntermediate lengths can be created, e.g. 11/16 inch (11,2 mm) corresponds to length code 11.
32、bAdditional 0,8 mm (1/32 inch) length increments may be obtained by adding code 5 after last digit of part number. cValid also for 5X dMass based on aluminium alloy with a density of 2,79 kg/dm, refer to Table 3 for conversion factors. BS EN 6080:2016EN 6080:2016 (E) 7 Table 3 Oversize Diameter code
33、 aD Nominal diameter A A1 B C E F P R1 S W +0,03 0,03 max. min. min. Ref. +0,05 0 Ref. null0,13 max. min. null0,25 null0,25 max. min. 5X 4,37 7,25 7,15 6,79 1,19 0,8 0,08 to 0,15 5,29 0,706 0,650 1,24 0,99 5,588 5,583 a(.015625 inch oversize shank 0,396 mm) Table 4 Material code Diameter code Surfac
34、e treatment (Code see Clause 4) Density kg/dm3Multiplicator of mass (see Table 2) Material code 2 3 4 5 6 7 8 10 12 Material Use rivets according to EN 6101 Aluminium alloy 2117-T4 per EN 2115 Yellow chromated per MIL-C-5541, class 1A Anodized per MIL-A-8625, type II, class 1, clear a 2,75 0,98 AD A
35、luminium alloy 2017A-H13 per EN 2116 2,79 1 D Aluminium alloy 5056A-H32 per EN 2117 2,64 0,95 B aAluminium alloy AL-P7050 per EN 3115 2,82 1,01 KE Heat resisting alloy NI-PD9001 (NiCu31) per EN 4372, annealed at T 860 C, for 10 min / air none 8,85 3,17 N Titanium alloy 44.5 Cb heat treat: annealed p
36、er AMS 4982 anodized per ISO 8080 5,8 2,08 T IVD per EN 6118 V aNot for new design. BS EN 6080:2016EN 6080:2016 (E) 8 4 Designation EXAMPLE Description block RIVET Identity block EN6080 D6-06A5 Number of this standard Material code (see Table 4) Diameter code (see Tables 1 or 3 for oversize) Length
37、code (see Table 2) (1/16 of an inch)* Surface treatment for aluminium alloy (see Table 3): No code indicates yellow chromated, Code “A” indicates anodized (not for new design) Additional length code (see Table 2) (1/16 of an inch plus 1/32 inch)* * For supplying purpose only, see footnotes aand bin
38、Table 2. NOTE If necessary, the code I9005 shall be placed between the description block and the identity block. 5 Marking 5.1 Material identification Symbol on rivet head, see Figure 2. BS EN 6080:2016EN 6080:2016 (E) 9 EN 2115 EN 2116 EN 2117 Indented 0,2 mm max. Embossed 0,2 mm max. Embossed 0,2
39、mm max. EN 3115 EN 4372 AMS 4982 Embossed 0,2 mm max. Embossed 0,2 mm max. Indented 0,25 mm max. Figure 2 Material identification Symbol on rivet end shank end, see Figure 3. Key 1 dimple (0,2 mm max.) on shank end for oversize rivets Figure 3 Repair diameter identification 5.2 Manufacturers identif
40、ication EN 2424, style F to be embossed or indented on rivet head. Manufacturers identification is required on rivet heads for diameter code 4 and larger. BS EN 6080:2016EN 6080:2016 (E) 10 6 Technical specification 6.1 Aluminium alloy rivet Aluminium alloy rivets shall conform with the requirements
41、 of EN 6104. 6.2 Heat resisting alloy NI-PD9001 (NiCu31) rivets NiCu31 (Monel 400) rivets shall conform with the requirements of EN 2941. Shear strength Rc: 340 MPa to 450 MPa. 6.3 Titanium alloy rivet Titanium alloy 44.5 Cb rivets shall conform with the requirements of NASM 5674 except for the fini
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