1、BRITISH STANDARD AEROSPACE SERIES BS EN 3642:1997 Rivets, solid, 100 countersunk normal head, with dome, in titanium TI-PO2, anodized, inch based series The European Standard EN 3642:1996 has the status of a British Standard ICS 49.030.99BSEN 3642:1997 This British Standard, having been prepared und
2、er the direction of the Engineering Sector Board, was published under the authority of the Standards Board and comes into effect on 15 January 1997 BSI 11-1998 The following BSI references relate to the work on this standard: Committee reference ACE/12 Draft for comment 90/76227 DC ISBN 0 580 27030
3、0 Committees responsible for this British Standard The preparation of this British Standard was entrusted to Technical Committee ACE/12, Aerospace fasteners and fastening systems, upon which the following bodies were represented: Association of Electronics, Telecommunications and Business Equipment
4、Industries British Industrial Fasteners Federation Ministry of Defence Society of British Aerospace Companies Ltd. Amendments issued since publication Amd. No. Date CommentsBSEN 3642:1997 BSI 11-1998 i Contents Page Committees responsible Inside front cover National foreword ii Foreword 2 1 Scope 3
5、2 Normative references 3 3 Required characteristics 3 4 Designation 6 5 Marking 6 6 Technical specification 6 Figure 1 4 Table 1 3 Table 2 5 List of references Inside back coverBSEN 3642:1997 ii BSI 11-1998 National foreword This British Standard has been prepared by Technical Committee ACE/12 and i
6、s the English language version of EN 3642:1996 Aerospace series Rivets, solid,100 countersunk normal head with dome, in titanium TI-PO2, anodized, inch based series, published by the European Committee for Standardization (CEN). EN 3642:1996 was produced as a result of international discussions in w
7、hich the United Kingdom took an active part. A British Standard does not purport to include all 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 obligatio
8、ns. Cross-references Publication referred to Corresponding British Standard EN 2424:1995 BS EN 2424:1995 Marking of aerospace products ISO 8080:1985 BS M 58:1986 Specification for anodic coating of titanium and titanium alloys by the sulphuric acid process Summary of pages This document comprises a
9、front cover, an inside front cover, pages i and ii, theEN title page, pages 2 to 6, an inside back cover 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 theinside front cover.EUROPEAN STA
10、NDARD NORME EUROPENNE EUROPISCHE NORM EN 3642 September 1996 ICS 49.040.20 Descriptors: Aircraft industry, rivet, countersunk head rivet, titanium, characteristic, dimension, dimensional tolerance, designation English version Aerospace series Rivets, solid, 100 countersunknormalhead with dome, in ti
11、tanium TI-PO2, anodized, inch based series Srie arospatiale Rivets ordinaires, tte fraise 100 normale avec dme, en titane TI-PO2, anodiss, srie base inches Luft- und Raumfahrt Vollniete, mit 100 normalem Senkkopf mit Dom, aus Titan TI-PO2, anodisiert, Zoll-Reihe This European Standard was approved b
12、y CEN on 1996-06-29. 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 national standard without any alteration. Up-to-date lists and bibliographical references concerning such national standards
13、 may be obtained on application to the Central Secretariat or to any CEN member. The European Standards exist 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 C
14、entral Secretariat has the same status as the official versions. CEN members are the national standards bodies of Austria, Belgium, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and United Kingdom. CEN Europe
15、an Committee for Standardization Comit Europen de Normalisation Europisches Komitee fr Normung Central Secretariat: rue de Stassart 36, B-1050 Brussels 1996 Copyright reserved to CEN members Ref. No. EN 3642:1996 EEN3642:1996 BSI 11-1998 2 Foreword This European Standard has been prepared by the Eur
16、opean Association of Aerospace Manufacturers (AECMA). After inquiries and votes carried 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 AECMA, prior to its presentation to
17、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 1997, and conflicting national standards shall be withdrawn at the latest by March 1997. According to the CEN/CENELEC Internal Regulation
18、s, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and the United Kingdom.EN3642:
19、1996 BSI 11-1998 3 1 Scope This standard specifies the characteristics of solid rivets, with 100 countersunk normal head with dome, in titanium TI-PO2, anodized, inch based series, for maximum operating temperature 315 C. 2 Normative references This European Standard incorporates by dated or undated
20、 reference provisions from other publications. These normative references are cited at the appropriate places in the text and the publications are listed hereafter. For dated references, subsequent amendments to or revisions of any of these publications apply to this European Standard only when inco
21、rporated in it by amendment or revision. For undated references the latest edition of the publication referred to applies. ISO 8080, Aerospace Anodic treatment of titanium and titanium alloys Sulfuric acid process. ISO 10299, Aerospace Identification marking of solid rivets 1) . EN 2424, Aerospace s
22、eries Marking of aerospace products. EN 3378, Aerospace series Titanium TI-PO2 Annealed 330 # R c# 410 MPa Wire for rivet 1,6 # d # 10 mm 2) . EN 3627, Aerospace series Titanium solid rivets Technical specification 1) . 3 Required characteristics 3.1 Configuration Dimensions Masses See Figure 1 and
23、Table 1 and Table 2. Dimensions and tolerances are expressed in millimetres and apply after surface treatment. 3.2 Material EN 3378 3.3 Surface treatment ISO 8080 Table 1 1) In preparation at the date of publication of this standard 2) Published as AECMA Prestandard at the date of publication of thi
24、s standard Diameter code D 1 a D 2 b D 3 D 4 D 5 D 6 L 2 L 3 L 4 L 5 L 6 R max. min. min. max. min. max. min. min. max. min. 0,08 024 2,45 2,35 4,45 4 3,2 2,4 3,54 1,9 1,6 0,9 0,05 0,38 2,4 0,8 0,5 0,15 032 3,25 3,15 5,95 5,35 4,3 3,2 4,82 2,6 2,3 1,1 0,06 0,47 2,6 1 0,7 036 3,65 3,55 6,7 6 4,8 3,6
25、5,46 2,9 2,5 1,3 0,07 0,52 2,9 1,1 0,25 040 4,05 3,94 7,4 6,6 5,3 4 5,79 3,2 2,8 1,4 0,08 0,68 3 1,2 0,8 048 4,85 4,73 8,9 7,95 6,4 4,8 7,39 3,8 3,3 1,8 0,1 0,63 3,8 1,5 1 a D 1max. may increase by 0,03, over length (L 5 L 2 ). b Maximum condition 0 0,08 EN3642:1996 4 BSI 11-1998 Figure 1EN3642:1996
26、 BSI 11-1998 5 Table 2 Diameter code 024 032 036 040 048 Length a Mass b a Mass b a Mass b a Mass b a Mass b code N R N R N R N R N R 004 4 0,106 0,203 0,258 005 5 0,126 0,239 0,302 006 6 0,147 0,276 0,344 0,455 007 7 0,167 0,312 0,385 0,511 008 8 0,188 0,349 0,427 0,567 0,848 009 9 0,208 0,383 0,46
27、9 0,623 0,929 010 10 0,228 0,420 0,512 0,679 1,010 011 11 0,249 0,456 0,553 0,735 1,091 012 12 0,269 0,493 0,595 0,792 1,173 013 13 0,290 0,529 0,637 0,848 1,254 014 14 0,310 0,565 0,678 0,905 1,336 015 15 0,330 0,601 0,720 0,961 1,417 016 16 0,351 0,637 0,764 1,017 1,499 017 17 0,371 0,673 0,805 1,
28、074 1,580 018 18 0,392 0,709 0,848 1,130 1,662 019 19 0,412 0,745 0,890 1,187 1,743 020 20 0,432 0,782 0,932 1,244 1,824 022 22 0,855 1,015 1,357 1,987 024 24 0,928 1,100 1,470 2,150 026 26 1,183 1,583 2,313 028 28 1,270 1,696 2,476 030 30 1,810 2,638 032 32 1,923 2,801 035 35 2,964 040 40 3,127 a T
29、ail end code (see Figure 1) b Approximate values (kg/1 000 pieces), calculated on the basis of 4,45 kg/dm 3 , given for information purposes only L 1 + 0,5 0EN3642:1996 6 BSI 11-1998 4 Designation EXAMPLE: NOTEIf necessary, the code I9005 shall be placed between the description block and the identit
30、y block. 5 Marking 5.1 Rivet EN 2424, style G 5.2 Material ISO 10299 6 Technical specification EN 3627BSEN 3642:1997 BSI 11-1998 List of references See national foreword.BSI 389 Chiswick High Road London W4 4AL | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | |
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