BS EN 2553-1993 Rivets solid 100 normal countersunk head with dome in aluminium alloy 2017A inch based series《2017A型铝合金制100标准埋头圆顶实心铆钉 英制系列》.pdf

1、BRITISH STANDARD AEROSPACE SERIES BS EN 2553:1993 Rivets, solid, 100 normal countersunk head with dome, in aluminium alloy2017A, inch based series The European Standard EN2553:1992 has the status of a British Standard UDC 629.7:621.884.091.6-034.71BSEN2553:1993 This British Standard, having been pre

2、pared under the directionof the Aerospace Standards Policy Committee, waspublished under the authorityof the Standards Boardand comes into effect on 15February1993 BSI 09-1999 The following BSI references relate to the work on this standard: Committee reference ACE/12 Draft for comment 89/79436 DC I

3、SBN 0 580 21980 1 Cooperating 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 n

4、ormalisation Denmark Dansk 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 Aut

5、hority of Ireland Italy Ente 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 Sta

6、ndardiseringskommissionen i Sverige Switzerland Association suisse de normalisation United Kingdom British Standards Institution Amendments issued since publication Amd. No. Date CommentsBSEN2553:1993 BSI 09-1999 i Contents Page Cooperating organizations Inside front cover National foreword ii Forew

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

8、r Figure 1 4 Figure 2 6 Table 1 4 Table 2 5 Table 3 6BSEN2553:1993 ii BSI 09-1999 National foreword This British Standard has been prepared under the direction of the Aerospace Standards Policy Committee and is the English language version of EN2553:1992 Aerospace series Rivets, solid, 100 normal co

9、untersunk head with dome, in aluminium alloy2017A, inch based series, published by the European Committee for Standardization (CEN). EN2553:1992 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 t

10、he 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. Summary of pages This document comprises a front cover, an inside front cover, pages i and ii

11、, 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 the inside front cover.EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 2553 Nov

12、ember 1992 UDC 629.7:621.884.091.6-034.71 Descriptors: Aircraft industry, full rivet, countersunk head rivet, aluminium alloy, dimension, designation, marking English version Aerospace series Rivets, solid, 100 normal countersunk head with dome, in aluminium alloy2017A, inch based series Srie arospa

13、tiale Rivets ordinaires, tte fraise100 normal, en alliage daluminium2017A, srie base inches Luft- und Raumfahrt Vollniete, mit100 normalem Senkkopf, aus Aluminium legerierung2017A, Inch-Reihe This European Standard was approved by CEN on1992-11-16. CEN members are bound to comply with the CEN/CENELE

14、C 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 Secretariat or to any CEN

15、 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 Central Secretariat has the same status as the official versions. CEN me

16、mbers 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 Normalisation Europis

17、ches Komitee fr Normung Central Secretariat: rue de Stassart 36, B-1050 Brussels 1992 Copyright reserved to CEN members Ref. No. EN 2553:1992 EEN2553:1992 BSI 09-1999 2 Foreword This European Standard has been prepared by the European Association of Aerospace Manufacturers (AECMA). After inquiries a

18、nd votes carried out in accordance with the rules of this Association, this standard has 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

19、 national standard, either by publication of an identical text or by endorsement, at the latest byMay1993, and conflicting national standards shall be withdrawn at the latest byMay1993. According to the CEN/CENELEC Internal Regulations, the following countries are bound to implement this European St

20、andard: Austria, Belgium, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and the UnitedKingdom.EN2553:1992 BSI 09-1999 3 1 Scope This standard specifies the characteristics of solid rivets, with100 normal coun

21、tersunk head with dome, inch based series, in aluminium alloy, for maximum operating temperature120 C. 2 Normative 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 t

22、ext 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 the latest edition of the publication referred to appl

23、ies. EN 2000, Aerospace series Quality assurance EN aerospace products Approval of the quality system of manufacturers. EN 2116, Aerospace series Aluminium alloy2017A-H13 wire for solid rivetsDk 10mm 1) . EN 2345, Aluminium and aluminium alloy rivets Technical specification Aerospace series 1) . EN

24、2424, Aerospace series Identification marking of standard fasteners 1) . 3 Required characteristics 3.1 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 inT4 condition. 1) Publ

25、ished as AECMA standard at the date of publication of the present standardEN2553:1992 4 BSI 09-1999 Table 1 1)The length range is limited (seeTable 2). 2)Shape optional (except concave) within limiting dimensions 3)Blended convex form permissible within limiting dimensions Figure 1 Diameter code D 1

26、 a D 2 b D 3 D 4 D 5 D 6 H 1 H 2 H 3 L 2 L 3 R max min. min. max. min. max. min. min. max. min. max. min. 0,08 024 2,45 2,35 4,65 4,2 3,6 2,4 3,84 1,9 1,6 0,9 0,05 0,44 0,36 2,4 0,8 0,5 0,15 032 3,25 3,15 5,8 5,3 4,8 3,2 4,88 2,6 2,3 1,1 0,06 0,49 0,41 2,6 1 0,7 040 4,05 3,94 7,35 6,8 6 4 6,17 3,2 2

27、,8 1,4 0,08 0,6 0,52 3 1,2 0,8 048 4,85 4,73 9,05 8,4 7,2 4,8 7,57 3,8 3,3 1,8 0,72 0,64 3,8 1,5 1 056 5,65 5,33 10,65 10,1 8,4 5,6 8,89 4,5 3,9 2,1 0,84 0,76 4,1 1,8 1,2 0,25 064 6,45 6,33 12,2 11,55 9,6 6,4 10,19 5,1 4,5 2,4 0,1 0,95 0,87 4,4 2,1 1,4 080 8,03 7,9 14,45 13,65 12 8 12,19 6,4 5,6 2,7

28、 1,05 0,97 4,7 2,4 1,6 096 9,63 9,5 17,7 16,75 14,4 9,6 14,94 7,7 6,7 3,4 1,26 1,18 5,4 3 2 a D 1max may increase by0,03, over length (L 2 H 1 ). b Maximum conditionEN 2553:1992 BSI 09-1999 5 Table 2 Diameter code 024 032 040 048 056 064 080 096 Length a Mass bkg/1000 pieces a Mass bkg/1000 pieces a

29、 Mass bkg/1000 pieces a Mass bkg/1000 pieces a Mass bkg/1000 pieces a Mass bkg/1000 pieces a Mass bkg/1000 pieces a Mass bkg/1000 pieces Code L 1+ N R N R N R N R N R N R N R N R 003 3 004 4 0,080 0,147 005 5 0,093 0,170 006 6 0,106 0,193 0,323 007 7 0,119 0,216 0,358 008 8 0,132 0,239 0,394 0,615 0

30、09 9 0,145 0,261 0,430 0,666 010 10 0,158 0,284 0,465 0,717 1,020 011 11 0,171 0,307 0,500 0,768 1,089 012 12 0,184 0,330 0,536 0,819 1,158 1,570 014 14 0,210 0,376 0,607 0,921 1,296 1,750 2,741 016 16 0,236 0,422 0,678 1,023 1,434 1,930 3,019 8,933 018 18 0,262 0,467 0,750 1,125 1,572 2,110 3,297 9

31、,335 020 20 0,288 0,513 0,820 1,227 1,710 2,290 3,575 9,737 022 22 0,314 0,559 0,891 1,329 1,848 2,470 3,853 10,139 024 24 0,340 0,605 0,962 1,431 1,986 2,650 4,131 10,541 026 26 0,366 0,651 1,033 1,533 2,124 2,830 4,409 10,943 028 28 0,392 0,696 1,105 1,635 2,262 3,010 4,687 11,345 030 30 0,418 0,7

32、42 1,176 1,737 2,400 3,190 4,965 11,747 032 32 0,444 0,788 1,247 1,839 2,538 3,370 5,243 12,149 035 35 0,483 0,856 1,353 1,992 2,745 3,640 5,660 12,752 040 40 0,971 1,531 2,247 3,090 4,090 6,355 13,757 045 45 1,085 1,709 2,502 3,435 4,540 7,050 14,762 050 50 1,886 2,757 3,780 4,990 7,745 15,767 055

33、55 3,012 4,125 5,440 8,440 16,772 060 60 3,267 4,470 5,890 9,135 17,777 a Tail end code (seeFigure 1) b Approximate values, calculated on the basis of2,76kg/dm 3 , given for information purpose only 0,5 0EN2553:1992 6 BSI 09-1999 4 Designation Example: NOTEIf necessary, the originator code19005 shal

34、l 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. Symbol at manufacturers option Table 3 6 Technical specification EN 2345 except for approval of manufacturers, seeEN2000. 7 Heat t

35、reatment 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 a temperature not exceeding40 C. F

36、igure 2 Diameter code 024 032 040 048 056 064 080 096 T 0,05 0,13 0,15 0,2 D 7max. 0,8 D 8 max. = D 1max. (see Table 1)BSEN2553:1993 BSI 09-1999 National annex NA (informative) Committees responsible The United Kingdom participation in the preparation of this European Standard was entrusted by the A

37、erospace Standards Policy Committee (ACE/-) to Technical Committee ACE/12, upon 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 Compa

38、nies Ltd. National annex NB (informative) Cross-references The British Standards corresponding to the European Standards referred to in the text are identical in number and title with those given inclause2, with the exception of EN2116, EN2345 and EN2424 for which no corresponding British Standards

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