BS EN 2146-1993 Rivets solid universal head in aluminium alloy 2017A inch based series《2017A型铝制通用头型实心铆钉 英制系列》.pdf

1、BRITISH STANDARD AEROSPACE SERIES BS EN 2146:1993 Rivets, solid, universal head, in aluminium alloy 2017A, inch based series The European Standard EN 2146:1992 has the status of a British Standard UDC 621.884.2-034.715:629.7BSEN2146:1993 This British Standard, having been prepared under the directio

2、nof the Aerospace Standards Policy Committee, waspublished under the authorityof the Standards Boardand comes intoeffecton 15February 1993 BSI 11-1999 The following BSI references relate to the work on this standard: Committee reference ACE/12 Draft for comment 89/79410 DC ISBN 0 580 21974 7 Coopera

3、ting organizations The European Committee for Standardization (CEN), under whose supervision this European Standard was prepared, comprises the national standards organizations of the following countries: Austria Oesterreichisches Normungsinstitut Belgium Institut belge de normalisation Denmark Dans

4、k Standardiseringsraad Finland Suomen Standardisoimisliito, r.y. France Association franaise de normalisation Germany Deutsches Institut fr Normung e.V. Greece Hellenic Organization for Standardization Iceland Technological Institute of Iceland Ireland National Standards Authority of Ireland Italy E

5、nte Nazionale Italiano di Unificazione Luxembourg Inspection du Travail et des Mines Netherlands Nederlands Normalisatie-instituut Norway Norges Standardiseringsforbund Portugal Instituto Portugus da Qualidade Spain Asociacin Espaola de Normalizacin y Certificacin Sweden Standardiseringskommissionen

6、 i Sverige Switzerland Association suisse de normalisation United Kingdom British Standards Institution Amendments issued since publication Amd. No. Date CommentsBSEN2146:1993 BSI 11-1999 i Contents Page Cooperating organizations Inside front cover National foreword ii Foreword 2 1 Scope 3 2 Normati

7、ve references 3 3 Required characteristics 3 4 Designation 4 5 Marking 4 6 Technical specification 7 7 Heat treatment prior to setting 7 National annex NA (informative) Committees responsible Inside back cover National annex NB (informative) Cross-references Inside back cover Figure 1 3 Figure 2 5 T

8、able 1 4 Table 2 6 Table 3 5BSEN2146:1993 ii BSI 11-1999 National foreword This British Standard has been prepared under the direction of the Aerospace Standards Policy Committee and is the English language version ofEN2146:1992 Aerospace series Rivets, solid, universal head, in aluminium alloy 2017

9、A, inch based series, published by the European Committee for Standardization (CEN). EN 2146:1992 was produced as a result of international discussions in which the United Kingdom took an active part. A British Standard does not purport to include all the necessary provisions of a contract. Users of

10、 British Standards are responsible for their correct application. Compliance with a British Standard does not of itself confer immunity from legal obligations. Summary of pages This document comprises a front cover, an inside front cover, pages i and ii, theEN title page, pages 2 to 8, an inside bac

11、k 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 the inside front cover.EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 2146 November 1992 UDC 621.884.2-034.715:629.7 Descript

12、ors: Aircraft industry, full rivet, round head rivet, aluminium alloy, dimension, designation, marking English version Aerospace series Rivets, solid, universal head, in aluminium alloy 2017A, inch based series Srie arospatiale Rivets ordinaires, tte ronde aplatie, en alliage daluminium 2017A, srie

13、base inches Luft- und Raumfahrt Vollniete, mit Universalkopf, aus Aluminiumlegierung2017A, Inch-Reihe This European Standard was approved by CEN on 1992-11-16. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Standard t

14、he 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 Secretariat or to any CEN member. This European Standard exists in three official versions (English, French, Germa

15、n). 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 official versions. CEN members are the national standards bodies of Austria, Belgium, Denmark, Finland, France, Ge

16、rmany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and United Kingdom. CEN European Committee for Standardization Comit Europen de Normalisation Europisches Komitee fr Normung Central Secretariat: rue de Stassart 36, B-1050 Brussels 1992 Cop

17、yright reserved to CEN members Ref. No. EN 2146:1992 EEN2146:1992 BSI 11-1999 2 Foreword This European Standard has been prepared by the European Association of Aerospace Manufacturers (AECMA). After inquiries and votes carried out in accordance with the rules of this Association, this standard has

18、successively 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 status of a national standard, either by publication of an identical text or by endorsement, at the

19、latest by May 1993, and conflicting national standards shall be withdrawn at the latest by May 1993. According to the CEN/CENELEC Internal Regulations, the following countries are bound to implement this European Standard: Austria, Belgium, Denmark, Finland, France, Germany, Greece, Iceland, Ireland

20、, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and the UnitedKingdom.EN2146:1992 BSI 11-1999 3 1 Scope This standard specifies the characteristics of solid rivets, with universal head, inch based series, in aluminium alloy, for maximum operating temperature120 C. 2 No

21、rmative references This European Standard incorporates by dated or undated 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

22、of any of these publications apply to this European Standard only when incorporated in it by amendment or revision. For undated references the latest edition of the publication referred to applies. EN 2000, Aerospace series Quality assurance EN aerospace products Approval of the Quality system of ma

23、nufacturers. EN 2116, Aerospace series Aluminium alloy 2017A-H13 wire for solid rivets D k 10mm 1) . EN 2345, Aluminium and aluminium alloy rivets Technical specification Aerospace series 1) . EN 2424, Aerospace series Identification marking of standard fasteners 1) . 3 Required characteristics 3.1

24、Configuration Dimensions Masses SeeFigure 1 andTable 1 andTable 2. Dimensions and tolerances are expressed in millimetres. 3.2 Material EN 2116 The rivet shall be delivered in T4 condition. 1) Published as AECMA standard at the date of publication of the present standard 1) The length range is limit

25、ed (seeTable 2). Figure 1 EN2146:1992 4 BSI 11-1999 Table 1 4 Designation Example: NOTEIf necessary, the originator code19005shall be placed between the description block and the identity block. 5 Marking 5.1 Rivet identification EN 2424, style G 5.2 Material identification SeeFigure 2 andTable 3. S

26、ymbol at manufacturers option Diameter code D 1 a D 2 D 3 D 4 L 2 L 3 L 4 R 1 R 2 0,08 max. min. max. min. max. min. max. min. max. min. 024 2,45 2,35 5 4,5 2,4 1,8 1,9 1,6 1 1,45 0,8 0,5 2,9 0,15 032 3,25 3,15 6,7 6 3,2 2,4 2,6 2,3 1,4 1 0,7 3,9 040 4,05 3,94 8,3 7,5 4 3 3,2 2,8 1,7 1,95 1,2 0,8 4,

27、9 0,25 048 4,85 4,73 10 9 4,8 3,6 3,8 3,3 2 1,5 1 5,9 056 5,65 5,53 11,7 10,5 5,6 4,2 4,5 3,9 2,4 1,8 1,2 6,8 064 6,45 6,33 13,3 12,1 6,4 4,8 5,1 4,5 2,7 2,1 1,4 7,8 080 8,03 7,9 16,7 15,1 8 6 6,4 5,6 3,4 2,4 1,6 9,8 096 9,63 9,5 20 18,1 9,6 7,2 7,7 6,7 4,1 3 2 11,7 a D 1max. may increase by 0,03, o

28、ver length L 3 . +0,2 0EN2146:1992 BSI 11-1999 5 Table 3 Figure 2 Diameter code 024 032 040 048 056 064 080 096 T 0,05 0,13 0,15 0,2 S max. 0,8 D 5max. D 6max. = D 1max. (see Table 1)EN 2146:1992 6 BSI 11-1999 Table 2 Diameter code 024 032 040 048 056 064 080 096 Length a Mass a Mass a Mass a Mass a

29、 Mass a Mass a Mass a Mass Code N R kg/1 000 pieces b N R kg/1 000 pieces b N R kg/1 000 pieces b N R kg/1 000 pieces b N R kg/1 000 pieces b N R kg/1 000 pieces b N R kg/1 000 pieces b N R kg/1 000 pieces b 004 4 0,083 0,176 005 5 0,095 0,198 006 6 0,107 0,220 0,373 007 7 0,119 0,242 0,408 008 8 0,

30、131 0,264 0,443 0,664 009 9 0,143 0,286 0,478 0,714 010 10 0,155 0,308 0,513 0,764 1,137 011 11 0,167 0,330 0,548 0,814 1,205 012 12 0,179 0,352 0,583 0,864 1,273 1,734 014 14 0,203 0,396 0,653 0,964 1,409 1,912 3,266 016 16 0,227 0,440 0,723 1,064 1,545 2,090 3,544 018 18 0,251 0,484 0,793 1,164 1,

31、681 2,268 3,822 5,868 020 20 0,275 0,528 0,863 1,264 1,817 2,446 4,100 6,266 022 22 0,299 0,572 0,933 1,364 1,953 2,624 4,378 6,664 024 24 0,323 0,616 1,003 1,464 2,089 2,802 4,656 7,062 026 26 0,347 0,660 1,073 1,564 2,225 2,980 4,934 7,460 028 28 0,371 0,704 1,143 1,664 2,361 3,158 5,212 7,858 030

32、 30 0,395 0,748 1,213 1,764 2,497 3,336 5,490 8,256 032 32 0,419 0,792 1,283 1,864 2,633 3,514 5,768 8,654 035 35 0,455 0,858 1,388 2,014 2,837 3,781 6,185 9,251 040 40 0,968 1,563 2,264 3,177 4,226 6,880 10,246 045 45 1,738 2,514 3,517 4,671 7,575 11,241 050 50 1,913 2,764 3,857 5,116 8,270 12,236

33、055 55 3,014 4,197 5,561 8,965 13,231 060 60 3,264 4,537 6,006 9,660 14,226 a Tail end code (see Figure 1) b Approximate values, calculated on the basis of 2,76 kg/dm 3 , given for information purpose only L 1 + 0,5 0EN2146:1992 BSI 11-1999 7 6 Technical specification EN 2345 except for approval of

34、manufacturers, seeEN2000. 7 Heat treatment prior to setting Those rivets shall be installed within two hours of solution treatment by the user, unless other appropriate measures are taken to extend this time. The solution treatment is performed at a temperature of495 C 5 C and quenching in water at

35、a temperature not exceeding40 C.8 blankBSEN2146:1993 BSI 11-1999 National annex NA (informative) Committees responsible The United Kingdom participation in the preparation of this European Standard was entrusted by the Aerospace Standards Policy Committee (ACE/-) to Technical Committee ACE/12, upon

36、which the following bodies were represented: Association of Electronics, Telecommunications and Business Equipment Industries British Industrial Fasteners Federation Ministry of Defence Society of British Aerospace Companies Ltd. National annex NB (informative) Cross-references The British Standards

37、 corresponding to the European Standards referred to in the text are identical in number and title with those given in clause2, with the exception ofEN2116,EN2345 and EN2424 for which no corresponding British Standards exist.BS EN 2146:1993 BSI 389 Chiswick High Road London W4 4AL BSIBritishStandard

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