BS EN 3643-1997 Rivets solid 100 countersunk normal head in titanium TI-PO2 anodized inch based series《阳极氧化TI-PO2钛制100标准埋头实心铆钉 英制系列》.pdf

1、BRITISH STANDARD AEROSPACE SERIES BS EN 3643:1997 Rivets, solid, 100 countersunk normal head, in titanium TI-PO2, anodized, inch based series The European Standard EN 3643:1996 has the status of a British Standard ICS 49.030.99BSEN3643:1997 This British Standard, having been prepared under the direc

2、tion 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 90/76226 DC ISBN 0 580 27026 2 Committees

3、 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 Industries B

4、ritish Industrial Fasteners Federation Ministry of Defence Society of British Aerospace Companies Ltd. Amendments issued since publication Amd. No. Date CommentsBSEN3643:1997 BSI 11-1998 i Contents Page Committees responsible Inside front cover National foreword ii Foreword 2 1 Scope 3 2 Normative r

5、eferences 3 3 Required characteristics 3 4 Designation 6 5 Marking 6 6 Technical specification 6 Figure 1 4 Table 1 4 Table 2 5 List of references Inside back coverBSEN3643:1997 ii BSI 11-1998 National foreword This British Standard has been prepared by Technical Committee ACE/12 and is the English

6、language version of EN3643:1996 Aerospace series Rivets, solid,100 countersunk normal head, in titanium TI-PO2, anodized, inch based series, published by the European Committee for Standardization (CEN). EN 3643:1996 was produced as a result of international discussions in which the United Kingdom t

7、ook 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 obligations. Cross-references Publ

8、ication 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 front cover, an inside fr

9、ont 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 STANDARD NORME EUROPENNE EUR

10、OPISCHE NORM EN 3643 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 countersunk normal head, in titanium TI-PO2, anodized, inch bas

11、ed series Srie arospatiale Rivets ordinaires, tte fraise 100 normale, en titane TI-PO2; anodiss, srie base inches Luft- und Raumfahrt Vollniete, mit 100 normalem Senkopf, aus Titan TI-PO2, anodisiert, Zoll-Reihe This European Standard was approved by CEN on 1996-06-29. CEN members are bound to compl

12、y 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 may be obtained on application to the Central Secr

13、etariat 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 Central Secretariat has the same status as the offic

14、ial 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 European Committee for Standardization Comit Europen de N

15、ormalisation Europisches Komitee fr Normung Central Secretariat: rue de Stassart 36, B-1050 Brussels 1996 Copyright reserved to CEN members Ref. No. EN 3643:1996 EEN3643:1996 2 BSI 11-1998 Foreword This European Standard has been prepared by the European Association of Aerospace Manufacturers (AECMA

16、). 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 CEN. This European Standard shall be given the stat

17、us of a national standard, either by publication of an identical text or by endorsement, at the latest by March1997, and conflicting national standards shall be withdrawn at the latest by March1997. According to the CEN/CENELEC Internal Regulations, the national standards organizations of the follow

18、ing 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.EN3643:1996 BSI 11-1998 3 1 Scope This standard specifies th

19、e characteristics of solid rivets, with 100 countersunk normal head, 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 reference provisions from other publications. These normative

20、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 incorporated in it by amendment or revision. For undated references

21、 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 series Marking of aerospace products. EN 3378, Aerospace series

22、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 Table 1 and Table 2. Dimensions and tolerances are expressed in

23、millimetres and apply after surface treatment. 3.2 Material EN 3378 3.3 Surface treatment ISO 8080 1) In preparation at the date of publication of this standard 2) Published as AECMA Prestandard at the date of publication of this standardEN3643:1996 4 BSI 11-1998 Table 1 Figure 1 Diameter code D 1 a

24、 D 2b D 3 D 4 D 5 L 2 L 3 L 4 L 5 L 6 R max. min. min. max. min. min. max. min. 0,08 024 2,45 2,35 4,45 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 4,82 2,6 2,3 1,1 0,06 0,47 2,6 1 0,7 036 3,65 3,55 6,7 6 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 5,79 3,

25、2 2,8 1,4 0,08 0,68 3 1,2 0,8 048 4,85 4,73 8,9 7,95 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 condition00,08 EN3643:1996 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

26、 R N R N R N R 004 4 X X 0,101 X X 0,191 X X 0,257 005 5 X X 0,121 X X 0,227 X X 0,302 006 6 X X 0,142 X X 0,263 X X 0,344 X X 0,432 007 7 X X 0,162 X X 0,299 X X 0,384 X X 0,488 008 8 X X 0,183 X X 0,335 X X 0,427 X X 0,544 X X 0,808 009 9 X X 0,203 X X 0,371 X X 0,469 X X 0,600 X X 0,889 010 10 X

27、X 0,223 X X 0,408 X X 0,511 X X 0,656 X X 0,970 011 11 X X 0,244 X X 0,444 X X 0,552 X X 0,712 X X 1,051 012 12 X X 0,264 X X 0,480 X X 0,595 X X 0,769 X X 1,134 013 13 X X 0,285 X X 0,516 X X 0,637 X X 0,825 X X 1,215 014 14 X X 0,305 X X 0,552 X X 0,678 X X 0,882 X X 1,297 015 15 X X 0,325 X X 0,5

28、89 X X 0,720 X X 0,938 X X 1,378 016 16 X X 0,346 X X 0,625 X X 0,764 X X 0,995 X X 1,460 017 17 X 0,366 X X 0,661 X X 0,805 X X 1,051 X X 1,541 018 18 X 0,387 X X 0,697 X X 0,847 X X 1,108 X X 1,623 019 19 X 0,407 X 0,733 X X 0,890 X X 1,164 X X 1,704 020 20 X 0,427 X 0,770 X X 0,932 X X 1,221 X X

29、1,785 022 22 X 0,842 X 1,015 X X 1,334 X X 1,949 024 24 X 0,914 X 1,100 X X 1,447 X X 2,111 026 26 X 1,183 X 1,560 X X 2,274 028 28 X 1,270 X 1,673 X X 2,437 030 30 X 1,787 X 2,599 032 32 X 1,900 X 2,762 035 35 X 2,925 040 40 X 3,088 a Tail end code (see Figure 1) b Approximate values (kg/1000 piece

30、s), calculated on the basis of 4,45 kg/dm 3 , given for information purposes only L 1+ 0,5 0EN3643:1996 6 BSI 11-1998 4 Designation EXAMPLE: NOTEIf necessary, the code 19005 shall be placed between the description block and the identity block. 5 Marking 5.1 Rivet EN 2424, style G 5.2 Material ISO 10

31、299 6 Technical specification EN 3627BSEN3643:1997 BSI 11-1998 List of references See national foreword.BSI 389 Chiswick High Road London W4 4AL | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | |

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