BS EN 2551-1993 Rivets solid 100 normal countersunk head with dome in aluminium alloy 2117 inch based series《2117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 2551:1993 Rivets, solid, 100 normal countersunk head with dome, in aluminium alloy2117, inch based series The European Standard EN2551:1992has the status of a British Standard UDC 629.7:621.884.091.6-034.71BSEN2551:1993 This British Standard, having been prepa

2、red under the directionof the Aerospace Standards Policy Committee, waspublished under the authorityof the Standards Boardand comes intoeffecton 15February1993 BSI 11-1999 The following BSI references relate to the work on this standard: Committee reference ACE/12 Draft for comment 88/71828 DC ISBN

3、0 580 21978 X 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 norma

4、lisation 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 Authori

5、ty 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 Standar

6、diseringskommissionen i Sverige Switzerland Association suisse de normalisation United Kingdom British Standards Institution Amendments issued since publication Amd. No. Date CommentsBSEN2551:1993 BSI 11-1999 i Contents Page Cooperating organizations Inside front cover National foreword ii Foreword

7、2 1 Scope 3 2 Normative references 3 3 Required characteristics 3 4 Designation 5 5 Marking 6 6 Technical specification 6 National annex NA (informative) Committees responsible Inside back cover National annex NB (informative) Cross-references Inside back cover Figure 1 4 Figure 2 6 Table 1 4 Table

8、2 5 Table 3 6BSEN2551:1993 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 of EN2551:1992 Aerospace series Rivets, solid, 100 normal countersunk head with dome, in aluminium a

9、lloy2117, inch based series, published by the European Committee for Standardization (CEN). EN2551:1992was produced as a result of international discussions in which the UnitedKingdom took an active part. A British Standard does not purport to include all the necessary provisions of a contract. User

10、s 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, the EN title page, pages 2to 6, an inside

11、 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 2551 November 1992 UDC 629.7:621.884.091.6-034.71 D

12、escriptors: Aircraft industry, full rivet, countersunk head rivet, aluminium alloy, dimensions, designation, marking English version Aerospace series Rivets, solid, 100 normal countersunk head with dome, in aluminium alloy2117, inch based series Srie arospatiale Rivets ordinaires, tte fraise100 norm

13、al, avec dme, en alliage daluminium2117, srie base inches Luft- und Raumfahrt Vollniete, mit100 normalem Senkkopf mit Dom, aus Aluminiumlegierung2117, Inch-Reihe This European Standard was approved by CEN on1992-11-16. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which s

14、tipulate 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 member. This European Standar

15、d 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 members are the national standar

16、ds bodies of Austria, Belgium, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and UnitedKingdom. CEN European Committee for Standardization Comit Europen de Normalisation Europisches Komitee fr Normung Central

17、 Secretariat: rue de Stassart 36, B-1050 Brussels 1992Copyright reserved to CEN members Ref. No. EN 2551:1992EEN2551:1992 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 accordanc

18、e 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 national standard, either by pub

19、lication of an identical text or by endorsement, at the latest by May1993, and conflicting national standards shall be withdrawn at the latest by May1993. According to the CEN/CENELEC Internal Regulations, the following countries are bound to implement this European Standard: Austria, Belgium, Denma

20、rk, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and the UnitedKingdom.EN2551:1992 BSI 11-1999 3 1 Scope This standard specifies the characteristics of solid rivets, with100 normal countersunk head with dome, inch ba

21、sed 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 text and the publications are li

22、sted 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 applies. EN 2000, Aerospace series

23、Quality assurance EN aerospace products Approval of the quality system of manufacturers. EN 2345, Aluminium and aluminium alloy rivets Technical specification Aerospace series 1) . EN 2424, Aerospace series Identification marking of standard fasteners 1) . FED QQ-A-430, Federal specification Identif

24、ication alloy rod and wire For rivets and cold heading 2) . 3 Required characteristics 3.1 Configuration Dimensions Masses See Figure 1 and Table 1 and Table 2. Dimensions and tolerances are expressed in millimetres. 3.2 Material Aluminium alloy2117-H13according to QQ-A-430 (1,6mm k D k 10mm). The r

25、ivet shall be delivered in T4condition. 1) Published as AECMA standard at the date of publication of the present standard 2) This specification is published by Superintendent of Documents, US Government Printing office, Washigton, DC20402, United States.EN2551:1992 4 BSI 11-1999 Table 1 1)The length

26、 range is limited (see Table 2). 2)Shape optional (except concave) within limiting dimensions 3)Blended convex form permissible within limiting dimensions Figure 1 Diameter code D 1 a D 2 b D 3 D 4 D 6 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. 0,08 016 1,6

27、5 1,55 3 2,65 2,4 1,6 2,46 0,6 0,03 0,33 0,25 2,1 0,15 024 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 0,5 032 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 2,8 1,4 0,08 0,6 0,52 3 1,2 0,8 0,25 a D 1max may increase by0

28、,03, over length (L 2 H 1 ). b Maximum conditionEN2551:1992 BSI 11-1999 5 Table 2 4 Designation Example: Diameter code 016 024 032 040 Length a Mass b a Mass b a Mass b a Mass b Code L 1 N R kg/1000 pieces N R kg/1000 pieces N R kg/1000 pieces N R kg/1000 pieces 003 3 0,026 004 4 0,032 0,080 0,147 0

29、05 5 0,038 0,093 0,170 006 6 0,044 0,106 0,193 0,323 007 7 0,050 0,119 0,216 0,358 008 8 0,056 0,132 0,239 0,394 009 9 0,062 0,145 0,261 0,430 010 10 0,067 0,158 0,284 0,465 011 11 0,073 0,171 0,307 0,500 012 12 0,079 0,184 0,330 0,536 014 14 0,091 0,210 0,376 0,607 016 16 0,103 0,236 0,422 0,678 01

30、8 18 0,262 0,467 0,750 020 20 0,288 0,513 0,820 022 22 0,314 0,559 0,891 024 24 0,340 0,605 0,962 026 26 0,366 0,651 1,033 028 28 0,392 0,696 1,105 030 30 0,418 0,742 1,176 032 32 0,444 0,788 1,247 035 35 0,483 0,856 1,353 040 40 0,971 1,531 045 45 1,085 1,709 050 50 1886 a Tail end code (see Figure

31、 1) b Approximate values, calculated on the basis of2,76kg/dm 3 , given for information purpose only + 0,5 0EN2551:1992 6 BSI 11-1999 NOTEIf necessary, the originator code19005shall be placed between the description block and the identity block. 5 Marking 5.1 Rivet identification EN2424, style G 5.2

32、 Material identification See Figure 2 and Table 3. Symbol at manufacturers option Table 3 6 Technical specification EN 2345except for approval of manufacturers, see EN2000. Figure 2 Diameter code 016 024 032 040 T = 0,05 0,13 0,15 D 7max. 0,8BSEN2551:1993 BSI 11-1999 National annex NA (informative)

33、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 which the following bodies were represented: Association of Electronics, Telecommunications and B

34、usiness Equipment Industries British Industrial Fasteners Federation Ministry of Defence Society of British Aerospace Companies 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 titl

35、e with those given in clause 2, with the exception of EN2345and EN2424for which no corresponding British Standards exist.BS EN 2551:1993 BSI 389 Chiswick High Road London W4 4AL BSIBritishStandardsInstitution BSI is the independent national body responsible for preparing BritishStandards. It present

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