1、BS EN 6069:2009ICS 49.030.60NO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBRITISH STANDARDAerospace series Rivet, 100reduced flush head, close tolerance Inch seriesThis British Standardwas published under theauthority of the StandardsPolicy and StrategyCommittee on 31 March20
2、10 BSI 2010ISBN 978 0 580 61662 4Amendments/corrigenda issued since publicationDate CommentsBS EN 6069:2009National forewordThis British Standard is the UK implementation of EN 6069:2009.The UK participation in its preparation was entrusted to TechnicalCommittee ACE/12, Aerospace fasteners and faste
3、ning systems.A list of organizations represented on this committee can be obtained onrequest to its secretary.This publication does not purport to include all the necessary provisionsof a contract. Users are responsible for its correct application.Compliance with a British Standard cannot confer imm
4、unityfrom legal obligations.BS EN 6069:2009EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 6069 November 2009 ICS 21.060.40 English Version Aerospace series - Rivet, 100 reduced flush head, close tolerance - Inch series Srie arospatiale - Rivets de prcision, 100 tte fraise - Srie en inches Luft
5、- und Raumfahrt - Vollniet, 100 Reduzierter Senkkopf, enge Toleranz - Zoll-Reihe This European Standard was approved by CEN on 6 October 2009. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Standard the status of a na
6、tional standard without any alteration. Up-to-date lists and bibliographical references concerning such national standards may be obtained on application to the CEN Management Centre or to any CEN member. This European Standard exists in three official versions (English, French, German). A version i
7、n any other language made by translation under the responsibility of a CEN member into its own language and notified to the CEN Management Centre has the same status as the official versions. CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark
8、, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATIO
9、N EUROPISCHES KOMITEE FR NORMUNG Management Centre: Avenue Marnix 17, B-1000 Brussels 2009 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 6069:2009: EBS EN 6069:2009EN 6069:2009 (E) 2 Contents Page Foreword 31 Scope 42 Normative r
10、eferences 43 Requirements . 54 Designation 85 Marking . 96 Technical specification . 10BS EN 6069:2009EN 6069:2009 (E) 3 Foreword This document (EN 6069:2009) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN). After enquiries and votes carri
11、ed out in accordance with the rules of this Association, 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
12、 publication of an identical text or by endorsement, at the latest by May 2010, and conflicting national standards shall be withdrawn at the latest by May 2010. 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 sh
13、all 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 are bound to implement this European Standard: Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Es
14、tonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. BS EN 6069:2009EN 6069:2009 (E) 4 1 Scope This European Standard spe
15、cifies the dimensions, tolerances and mass of rivets with 100 reduced flush head, close tolerance, inch series, for aerospace application. 2 Normative references The following referenced documents are indispensable for the application of this document. For dated references, only the edition cited ap
16、plies. 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 EN 2116, Aerospace series Aluminium alloy 2017A-T42 Wire for solid rivets D 10 mm EN 2117, Aerospace serie
17、s Aluminium alloy AL-P5056A (5056A)-H32 Wire for solid rivets D 10 mm EN 2424:2008, Aerospace series Marking of aerospace products EN 2941, Aerospace series Nickel alloy rivets Technical specification EN 3115, Aerospace series Aluminium alloy 7050- T73 Wire for solid rivets D 10mmEN 4372, Aerospace
18、series Heat resisting nickel alloy with copper NI-PD9001 (NiCu31) Wire for solid rivets D 10 mm EN 6104, Aerospace series Rivets, solid, in aluminium or aluminium alloy Inch series Technical specification1)EN 6118, Aerospace series Process specification Aluminium base protection for fasteners1)ISO 8
19、080, Aerospace Anodic treatment of titanium and titanium alloys Sulfuric acid process AMS 4982, Titanium alloy wire 44.5 Cb2)MIL-DTL-5541, Military specification, Chemical conversion coatings on aluminium and aluminium alloys3)MIL-A-8625, Military specification, Anodic coatings for aluminium and alu
20、minium alloys3)NASM5674, Rivets, structural, aluminium alloy, titanium columbium alloy, general specification for4)NAS9800, Head protrusion gaging, 100 flush head fasteners, gage block, gage diameters and stylus4) 1) Published as ASD-STAN Prestandard at the date of publication of this standard by Ae
21、rospace and Defence Industries Association of Europe-Standardization (ASD-STAN), (www.asd-stan.org). 2) Published by: Society of Automotive Engineers (SAE), (www.sae.org). 3) Published by: American Society for Testing and Materials (ASTM), (www.astm.org). 4) Published by: Aerospace Industries Associ
22、ation/ National Aerospace Standards (AIA/NAS), (www.aia.aerospace.org). BS EN 6069:2009EN 6069:2009 (E) 5 3 Requirements 3.1 Configuration, dimensions, tolerances and mass The configuration shall conform to Figure 1. The dimensions, tolerances and mass shall conform to Figure 1 and Tables 1 and 3. D
23、imensions and tolerances of oversizes (for repair purposes only) shall conform to Figure 1 and Tables 2 and 3. Dimensions and tolerances are expressed in millimetres. Marking ( see 5 ) D1)AS2)2) F A3)10030EC WPB3)L 0,254Head-cocking angelrelative to axisof rivet 1/2 max. 0,254 max. rad. 0,127 A A1R1
24、4)Key 1 Angular misalignment of rivet head to rivet shank axis 0,5 max. 2 Marking (see Clause 5). a0,025 mm shank diameter increase is permissible within 2,54 mm of the based of the head. bChamfered ends with radius to the R1dimensions or a 20 chamfer to dimension “S”. cMaximum head diameters are to
25、 theoretical sharp corners as measured by projection. dMeasurement method for inspection of head characteristics in accordance with NAS9800. Figure 1 Configuration 0,051a b c d 2 1 R1b c 1000,50,254 max. rad. BS EN 6069:2009EN 6069:2009 (E) 6 Table 1 Dimensions and tolerances Diameter code D Nominal
26、 diameter A A1B C E F P R1S W 0,03 max. min. min. Ref. + 0,050 0,13 max. min. 0,25 0,25 max. min. 3 2,38 3,709 3,623 3,263 0,540,08 0,08to 0,15 2,31 0,291 0,248 0,74 0,58 3,028 3,0234 3,18 4,923 4,835 4,475 0,71 3,53 0,336 0,291 0,99 0,79 4,135 4,1305 3,97 6,226 6,141 5,781 0,93 4,83 0,457 0,412 1,2
27、4 0,99 5,151 5,1466 4,76 7,635 7,543 7,183 1,190,10 5,15 0,610 0,559 1,50 1,19 6,200 6,1957 5,56 8,880 8,790 8,430 1,38 7,00 0,670 0,612 1,75 1,37 7,310 7,3058 6,36 10,014 9,907 9,547 1,51 8,15 0,677 0,618 1,98 1,57 8,420 8,415Table 2 Dimensions and tolerances for oversize rivets Diameter code D A A
28、1B C E F P R1S W 0,03 max. min. min. Ref. + 0,050 0,13 max. min. 0,25 0,25 max. min. 5X 4,37 6,630 6,540 6,18 0,93 0,08 0,08to 0,15 5,10 0,628 0,578 1,24 0,99 5,151 5,1466X 5,16 8,040 7,950 7,59 1,190,10 6,25 0,781 0,728 1,50 1,19 6,200 6,1957X 5,96 9,280 9,190 8,83 1,38 7,25 0,836 0,782 1,75 1,37 7
29、,310 7,305BS EN 6069:2009EN 6069:2009 (E) 7 Table 3 Length code and mass Lengtha,bDiameter code 3 4 5 6 7 8 codeL 0,254 Mass c kg/ 1 000 parts 03 4,76 0,06 0,11 04 6,35 0,08 0,15 0,24 05 7,94 0,10 0,18 0,29 0,43 06 9,52 0,12 0,22 0,35 0,51 0,71 07 11,11 0,14 0,25 0,40 0,59 0,81 1,07 08 12,70 0,16 0,
30、29 0,46 0,67 0,92 1,21 09 14,29 0,18 0,32 0,51 0,75 1,03 1,35 10 15,87 0,20 0,36 0,57 0,83 1,14 1,49 11 17,46 0,22 0,40 0,62 0,90 1,24 1,63 12 19,05 0,24 0,43 0,68 0,98 1,35 1,77 13 20,64 0,26 0,47 0,73 1,06 1,46 1,91 14 22,22 0,28 0,50 0,79 1,14 1,57 2,05 15 23,81 0,30 0,54 0,84 1,22 1,67 2,19 16 2
31、5,40 0,32 0,57 0,90 1,30 1,78 2,34 17 26,99 0,61 0,95 1,38 1,89 2,48 18 28,57 0,64 1,01 1,46 2,00 2,62 20 31,75 0,71 1,11 1,61 2,21 2,90 22 34,92 0,78 1,22 1,77 2,43 3,18 24 38,10 0,85 1,33 1,93 2,64 3,46 28 44,45 1,55 2,24 3,07 4,02 32 50,80 1,77 2,56 3,50 4,59 40 63,50 4,36 5,71 aLength missing in
32、 table can be created in 1/16 inch (1,59 mm) steps, e.g. length code 19 corresponds to: 19/16 inch (30,16 mm). b1/32 inch (0,79 mm) length increments may be obtained by adding code 5 after the last digit of part number, e.g. length code 06-5 corresponds to: 6/16 inch (9,53 mm) + 1/32 inch (0,79 mm)
33、= 13/32 inch (10,32 mm). cMass based on aluminium alloy with a density of 2,79 kg/dm3,refer to Table 4 for conversion factors. BS EN 6069:2009EN 6069:2009 (E) 8 3.2 Material and surface treatment See Table 4. Table 4 Material code Material code Diameter code Surface treatment (code see Clause 4) Den
34、sity kg/dm3Multiplicatorof mass (see Table 3) 3 4 5 5X 6 6X 7 7X 8 AD Aluminium alloy 2117-T42 per EN 2115 Yellow chromated per MIL-DTL-5541,class 1A Anodized per MIL-A-8625, type II, class 1, clear a 2,75 0,98 D Aluminium alloy 2017A-T42 per EN 2116 2,79 1 B a Aluminium alloy AL-P5056A (5056A)-H32
35、per EN 2117 2,64 0,95 KE Aluminium alloy 7050-T73 per EN 3115 2,82 1,01 N Heat resisting nickel alloy NI-PD9001 (NiCu31) per EN 4372, annealed None 8,85 3,17 T Titanium alloy 44.5 Cb, heat treat: annealed per AMS 4982 Anodized per ISO 8080 5,8 2,08 V IVD per EN 6118 aNot for new design. 4 Designatio
36、n EXAMPLE Description block RIVET Identity block EN6069D6X06A5 Number of this standard Material code (see Table 4) Diameter code (see Tables 1 and 2) Length code in 1/16 inch* (see Table 3). When the diameter code has no letter add between diameter code and length code a dash “-“. Surface treatment
37、for Al alloy (see Table 4): - No code indicates yellow chromate; - Code “A“ indicates anodized (not for new design). Additional length code (see Table 3) (1/16 of an inch plus 1/32 inch)*. When surface treatment has no letter code add between length code and additional length code a dash “-“. *For s
38、upplying purpose only, see footnotes aand bin Table 3. BS EN 6069:2009EN 6069:2009 (E) 9 5 Marking 5.1 Material identification Symbol on head, see Figure 2. Dimensions in millimetres EN 2115 EN 2116 EN 2117 Indented 0,2 mm max. Embossed 0,2 mm max. Embossed 0,2 mm max. EN 3115 EN 4372 AMS 4982 Embos
39、sed 0,2 mm max. Embossed 0,2 mm max. Indented 0,25 mm max. Figure 2 Material identification 5.2 Manufacturers identification EN 2424:2008, style F to be embossed or indented on rivet head. Manufacturers identification is required on rivet heads for diameter code 4 and larger. 0,8 max.0,8 max.0,8 max
40、.0,8 max.1,020 min.1,780 max.0,762 min. 1,270 max.0,8 max.BS EN 6069:2009EN 6069:2009 (E) 10 5.3 Identification of oversize rivets Symbol on rivet shank end, see Figure 3. Triangular shape indented 0,2 mm max. Figure 3 Identification of oversize rivets (the criteria being legibility) 6 Technical spe
41、cification 6.1 Aluminium alloy rivets Aluminium alloy rivets shall conform with the requirements of EN 6104. 6.2 Heat resting nickel alloy NI-PD9001 (NiCu31) rivets NI-PD9001 (NiCu31) rivets shall conform with the requirements of EN 2941. Shear strength Rc= 340 MPa to 407 MPa. NOTE Rivets manufactur
42、ed prior to 1 August 2005 with a maximum shear strength of 450 MPa may be procured and used until stocks are depleted. 6.3 Titanium alloy rivets Titanium alloy 44.5 Cb rivets shall conform with the requirements of NASM5674 except for the finish as stated. 0,8 mmmax.max. 0,5 D This page deliberately
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