BS EN 3141-1996 Rivets solid universal head in heat resisting nickel base alloy NI-P11 cadmium plated inch based series《耐高温镍基合金NI-P11镀镉通用头实心铆钉 英制系列》.pdf

《BS EN 3141-1996 Rivets solid universal head in heat resisting nickel base alloy NI-P11 cadmium plated inch based series《耐高温镍基合金NI-P11镀镉通用头实心铆钉 英制系列》.pdf》由会员分享，可在线阅读，更多相关《BS EN 3141-1996 Rivets solid universal head in heat resisting nickel base alloy NI-P11 cadmium plated inch based series《耐高温镍基合金NI-P11镀镉通用头实心铆钉 英制系列》.pdf（12页珍藏版）》请在麦多课文档分享上搜索。

1、BRITISH STANDARD AEROSPACE SERIES BS EN 3141:1996 Rivets, solid, universal head, in heat resisting nickel base alloy NI-P11, cadmium plated, inch based series The European Standard EN3141:1996 has the status of a BritishStandard ICS49.040.20BSEN3141:1996 This BritishStandard, having been prepared un

2、der the directionof the Engineering SectorBoard, was published underthe authority of the Standards Board and comesintoeffect on 15June1996 BSI 12-1999 The following BSI references relate to the work on this standard: Committee referenceACE/12 Draft for comment90/76230DC ISBN 0 580 25939 0 Committees

3、 responsible for this BritishStandard The preparation of this BritishStandard was entrusted to Technical Committee ACE/12, Aerospace fasteners and fastening systems, upon which the following bodies were represented: Association of Electronic, Telecommunications and Business Equipment Industries Brit

4、ish Industrial Fasteners Federation Ministry of Defence Society of British Aerospace Companies Amendments issued since publication Amd. No. Date CommentsBSEN3141:1996 BSI 12-1999 i Contents Page Committees responsible Inside front cover National foreword ii Foreword 2 1 Scope 3 2 Normative reference

5、s 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 coverBSEN3141:1996 ii BSI 12-1999 National foreword This BritishStandard has been prepared by Technical CommitteeACE/12 and is the English language v

6、ersion of EN3141:1996 Aerospace series Rivets, solid, universal head, in heat resisting nickel base alloy NI-P11, cadmium plated, inch based series, published by the European Committee for Standardization (CEN). EN3141:1996 was produced as a result of international discussions in which theUnited Kin

7、gdom 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 obligations. Cross-reference

8、s Publication referred to Corresponding BritishStandard EN2000:1991 BS EN2000:1992 Quality assurance. EN aerospace products. Approval of the quality system of manufacturers EN2424:1995 BS EN2424:1995 Marking of aerospace products Summary of pages This document comprises a front cover, an inside fron

9、t cover, pagesi andii, theEN title page, pages2 to6, 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 EUROPISC

10、HE NORM EN3141 March1996 ICS49.040.20 Descriptors: Aircraft industry, rivet, round head rivet, flat head rivet, nickel alloy, heat resistant material, cadmium plating, dimension, surface treatment, designation English version Aerospace series Rivets, solid, universal head, in heat resisting nickel b

11、ase alloy NI-P11, cadmium plated, inchbased series Srie arospatiale Rivets ordinaires, tte ronde aplatie, en alliage rsistant chaud base de nickel NI-P11, cadmis, srie base inches Luft- und Raumfahrt Vollniete, mit Universalkopf, aus hochwarmfester Nickelbasislegierung NI-P11, verkadmet, Zoll-Reihe

12、This European Standard was approved by CEN on1995-08-31. 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 reference

13、s 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, German). A version in any other language made by translation under the responsibility of a CEN member into i

14、ts 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, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switz

15、erland 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 1996 Copyright reserved to CEN members Ref. No. EN3141:1996EEN3141:1996 BSI 12-1999 2 Foreword This European St

16、andard 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 successively received the approval of the National Associations and the Official Services of the members

17、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 latest by September1996, and conflicting national standards shall be withdrawn at the latest by Septembe

18、r1996. According to the CEN/CENELEC Internal Regulations, 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, Sp

19、ain, Sweden, Switzerland and United Kingdom.EN3141:1996 BSI 12-1999 3 1 Scope This standard specifies the characteristics of solid rivets, with universal head, in heat resisting nickel base alloy NI-P11, cadmium plated, inch based series, for maximum operating temperature235 C. 2 Normative reference

20、s 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 of any of these pu

21、blications 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. ISO10299, Aerospace Identification marking of solid rivets 1) . EN2000, Aerospace series Quality assurance EN aerospace

22、products Approval of the quality system of manufacturers. EN2133, Aerospace series Cadmium plating of steels, with maximum specified tensile strength equal to or less than1450MPa, copper, copper alloys and nickel alloys 2) . EN2305, Nickel base alloy NI-P11 540MPak R m k 620MPa Bars and wires for ri

23、vets Aerospace series 2) . EN2424, Aerospace series Marking of aerospace products. EN2941, Aerospace series Nickel alloy rivets Technical specification 3) . 3 Required characteristics 3.1 Configuration Dimensions Masses SeeFigure 1 andTable 1 andTable 2. Dimensions and tolerances are expressed in mi

24、llimetres and apply after surface treatment. 3.2 Material EN2305 3.3 Surface treatment EN2133, 8m to14m 1) In preparation at the date of publication of this standard 2) Published as AECMA Standard at the date of publication of this standard 3) Published as AECMA Prestandard at the date of publicatio

25、n of this standardEN3141:1996 4 BSI 12-1999 Table 1 Figure 1 Diameter code D 1 a D 2 D 3 D 4 L 2 +0,2 0 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 1,4 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 3,9 036 3,65 3,55 7,

26、5 6,8 3,6 2,7 2,9 2,5 1,6 1,6 1,1 4,4 0,25 040 4,05 3,94 8,3 7,5 4 3 3,2 2,8 1,7 1,2 0,8 4,9 048 4,85 4,73 10 9 4,8 3,6 3,8 3,3 2 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 a D 1 max. may increase by0,03, over length L

27、3 .EN 3141:1996 BSI 12-1999 5 Table 2 Diameter code 024 032 036 040 048 056 064 Length a Mass b a Mass b a Mass b a Mass b a Mass b a Mass b a Mass b code L 1 +0,5 0 N R N R N R N R N R N R N R 004 4 0,237 0,478 0,727 005 5 0,279 0,552 0,814 006 6 0,321 0,622 0,897 1,036 007 7 0,362 0,696 0,981 1,14

28、8 008 8 0,401 0,766 1,064 1,260 1,873 009 9 0,442 0,840 1,147 1,376 2,036 010 10 0,481 0,911 1,231 1,488 2,200 3,171 4,227 011 11 0,523 0,984 1,314 1,600 2,360 3,392 4,517 012 12 0,564 1,055 1,398 1,712 2,527 3,614 4,807 013 13 0,605 1,132 1,481 1,826 2,687 3,834 5,097 014 14 0,645 1,199 1,564 1,940

29、 2,847 4,053 5,387 015 15 0,683 1,276 1,651 2,052 3,043 4,274 5,676 016 16 0,721 1,344 1,734 2,164 3,239 4,496 5,964 017 17 0,762 1,418 1,818 2,276 3,369 4,717 6,301 018 18 0,802 1,491 1,901 2,389 3,489 4,938 6,637 019 19 0,842 1,561 1,984 2,503 3,660 5,173 6,880 020 20 0,882 1,635 2,068 2,617 3,822

30、 5,409 7,122 022 22 1,780 2,234 2,841 4,146 5,820 7,699 024 24 1,924 2,401 3,126 4,473 6,262 8,282 026 26 2,571 3,293 4,797 6,641 8,856 028 28 2,738 3,518 5,121 7,147 9,434 030 30 3,745 5,445 7,587 10,010 032 32 3,970 5,769 8,026 10,588 035 35 6,288 8,690 11,454 040 40 7,163 9,793 12,897 a Tail end

31、code (seeFigure 1) b Approximate values (kg/1000pieces), calculated on the basis of8,85kg/dm 3 , given for information purposes onlyEN3141:1996 6 BSI 12-1999 4 Designation EXAMPLE: NOTEIf necessary, the code19005 shall be placed between the description block and the identity block. 5 Marking 5.1 Riv

32、et EN2424, style G 5.2 Material ISO10299 6 Technical specification EN2941 plus EN2000 for the approval of manufacturersBSEN3141:1996 BSI 12-1999 List of references See national foreword.BS EN 3141:1996 BSI 389 Chiswick High Road London W4 4AL BSIBritishStandardsInstitution BSI is the independent nat

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