1、BRITISH STANDARD AEROSPACE SERIES BS A 341:1999 ISO/TR 12198:1998 Rivets, solid Materials ICS 49.030.60BSA 341:1999 This British Standard, having been prepared under the directionof the Engineering SectorCommittee, was publishedunder the authority ofthe Standards Committee andcomes into effect on 15
2、 February 1999 BSI 05-1999 ISBN 0 580 32091 X National foreword This British Standard reproduces verbatim ISO/TR 12198:1998 and implements it as the UK national standard. The UK participation in its preparation was entrusted by Technical Committee ACE/12, Aerospace fasteners and fastening systems, t
3、o Subcommittee ACE/12/1, Aerospace fasteners and fastening systems (International), which has the responsibility to: aid enquirers to understand the text; present to the responsible international/European committee any enquiries on the interpretation, or proposals for change, and keep the UK interes
4、ts informed; monitor related international and European developments and promulgate them in the UK. A list of organizations represented on this subcommittee can be obtained on request to its secretary. Cross-references The British Standards which implement international or European publications refe
5、rred to in this document may be found in the BSI Standards Catalogue under the section entitled “International Standards Correspondence Index”, or by using the “Find” facility of the BSI Standards Electronic Catalogue. A British Standard does not purport to include all the necessary provisions of a
6、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, theISO/TR title page, pages
7、 ii to iv, pages 1 to 5 and abackcover. 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. Amendments issued since publication Amd. No. Date CommentsBSA341:1999 BSI 05-1999 i Contents
8、Page National foreword Inside front cover Foreword iii Text of ISO/TR 12198 1ii blankBS A 341:1999 ii BSI 05-1999 Contents Page Foreword iii 1 Scope 1 2 Aluminium alloys 1 3 Corrosion resisting steels 3 4 Nickel base alloys 4 5 Titanium alloys 5 Table 1 2 Table 2 3 Table 3 4 Table 4 5BS A 341:1999 B
9、SI 05-1999 iii Foreword ISO (the International Organization for Standardization) is a worldwide federation of national standards bodies (ISO member bodies). The work of preparing International Standards is normally carried out through ISO technical committees. Each member body interested in a subjec
10、t for which a technical committee has been established has the right to be represented on that committee. International organizations, governmental and non-governmental, in liaison with ISO, also take part in the work. ISO collaborates closely with the International Electrotechnical Commission (IEC)
11、 on all matters of electrotechnical standardization. The main task of technical committees is to prepare International Standards, but in exceptional circumstances a technical committee may propose the publication of a Technical Report of one of the following types: type 1, when the required support
12、cannot be obtained for the publication of an International Standard, despite repeated efforts; type 2, when the subject is still under technical development or where for any other reason there is the future but not immediate possibility of an agreement on an International Standard; type 3, when a te
13、chnical committee has collected data of a different kind from that which is normally published as an International Standard (“state of the art”, for example). Technical Reports of types 1 and 2 are subject to review within three years of publication, to decide whether they can be transformed into In
14、ternational Standards. Technical Reports of type 3 do not necessarily have to be reviewed until data they provide are considered to be no longer valid or useful. ISO/TR 12198, which is a Technical Report of type 3, was prepared by Technical Committee ISO/TC 20, Aircraft and space vehicles, Subcommit
15、tee SC 4, Aerospace fastener systems. Descriptors: Aircraft industry, fasteners, rivets, full rivets, specifications, material specifications, interchangeability.BSA 341:1999 iv BSI 05-1999 Avant-propos LISO (Organisation internationale de normalisation) est une fdration mondiale dorganismes nationa
16、ux de normalisation (comits membres de lISO). Llaboration des Normes internationales est en gnral confie aux comits techniques de lISO. Chaque comit membre intress par une tude a le droit de faire partie du comit technique cr cet effet. Les organisations internationales, gouvernementales et non gouv
17、ernementales, en liaison avec lISO, participent galement aux travaux. LISO collabore troitement avec la Commission lectrotechnique internationale (CEI) en ce qui concerne la normalisation lectrotechnique. La tche principale des comits techniques est dlaborer les Normes internationales. Exceptionnell
18、ement, un comit technique peut proposer la publication dun rapport technique de lun des types suivants: type 1, lorsque, en dpit de maints efforts, laccord requis ne peut tre ralis en faveur de la publication dune Norme internationale; type 2, lorsque le sujet en question est encore en cours de dvel
19、oppement technique ou lorsque, pour toute autre raison, la possibilit dun accord pour la publication dune Norme internationale peut tre envisage pour lavenir mais pas dans limmdiat; type 3, lorsquun comit technique a runi des donnes de nature diffrente de celles qui sont normalement publies comme No
20、rmes internationales (ceci pouvant comprendre des informations sur ltat de la technique, par exemple). Les rapports techniques des types 1 et 2 font lobjet dun nouvel examen trois ans au plus tard aprs leur publication afin de dcider ventuellement de leur transformation en Normes internationales. Le
21、s rapports techniques de type 3 ne doivent pas ncessairement tre rviss avant que les donnes fournies ne soient plus juges valables ou utiles. LISO/TR 12198, rapport technique du type 3, a t labor par le comit technique ISO/TC 20, Aronautique et espace, sous-comit SC4, lments de fixation pour constru
22、ctions arospatiales. Descripteurs: Industrie aronautique, lment de fixation, rivet, rivet plein, spcification, spcification de matire, interchangeabilit.BSA341:1999 BSI 05-1999 1 1 Scope 1 Domaine dapplication This Technical Report gives, for each material family and for each minimum shear stress, t
23、he material(s) to be used for the manufacture of solid rivets. Le prsent Rapport technique indique, pour chaque famille de matriaux et chaque contrainte minimale de cisaillement, le ou les matriaux utiliser pour la fabrication des rivets ordinaires. These materials ensure interchangeability of the p
24、roducts concerned. Ces matriaux assurent linterchangeabilit des produits concerns. This Technical Report applies when referenced in the relevant standard. Le prsent Rapport technique sapplique chaque fois quil est cit dans la norme concerne. 2 Aluminium alloys 2 Alliages daluminium See Table 1. Voir
25、 Tableau 1. Previous or other designations are given in parentheses. Entre parenthses, danciennes ou autres dsignations.BSA 341:1999 2 BSI 05-1999 Table 1 Minimum shear stress Contrainte minimale de cisaillement MPa Material designation Dsignation du matriau Control document Document de contrle Desi
26、gnation origin Origine de la dsignation Al99-5 AL-P1050A (1050A) EN 2114 AECMA 1100 QQ-A-430 U.S.A./tats-Unis A5 NF A 50-411 France 3.0255.26 Germany/Allemagne L36 BS L100 U.K./Royaume-Uni 260 Al4Cu0,7Mg0,7Mn AL-P2017A (2017A) EN 2116 AECMA 2017 QQ-A-430 U.S.A./tats-Unis AU4G AIR 9150 France 3.1324.
27、4 Germany/Allemagne L37 BS L100 U.K./Royaume-Uni 260 Al4,4Cu1,5Mg0,6Mn 2024 QQ-A-430 U.S.A./tats-Unis AU4G1 NF A 50-411 France 3.1354.4 Germany/Allemagne 195 Al2.6Cu0,3Mg 2117 QQ-A-430 U.S.A./tats-Unis AU2G AIR 9150 France 3.1124.4 Germany/Allemagne L86 BS L100 U.K/Royaume-Uni 170 Al5Mg0,3Mn AL-P505
28、6A (5056A) EN 2117 AECMA 5056 QQ-A-430 U.S.A./tats-Unis AG5 MC AIR 9150 France 3.3354.2 Germany/Allemagne L58 BS L100 U.K./Royaume-Uni 283 Al6,2Zn2,3Cu2,2Mg0,1Zr 7050 QQ-A-430 U.S.A./tats-Unis 3.4144 Germany/Allemagne 210 Al6,3Cu0,3Mn0,06Ti 2219 QQ-A-430 U.S.A./tats-Unis 240 Al4Cu0.4Mn0.2Mg V65 Russ
29、ia/RussieBSA341:1999 BSI 05-1999 3 Table 2 3 Corrosion resisting steels 3 Aciers rsistant la corrosion See Table 2. Voir Tableau 2. Previous or other designations are given in parentheses. Entre parenthses, danciennes ou autres dsignations. Minimum shear stress Contrainte minimale de cisaillement MP
30、a Material designation Dsignation du matriau Control document Document de contrle Designation origin Origine de la dsignation 330 Fe18Cr12Ni (AISI 304 L) FE-PA3901 (FE-PA11) EN 2470 AECMA UNS S0500 AMS 5686 U.S.A./tats-Unis Z2 CN 18-10 AIR 9150 France 1.4544 Germany/Allemagne DTD 5036 BS S100 U.K./R
31、oyaume-Uni 550 Fe25Ni15Cr2Ti1,3Mo0,3V (A286) FE-PA2601 (FE-PA92HT) EN 2119 AECMA UNS S66286 AMS 5734 U.S.A./tats-Unis E Z6 NCT 25 NF A 50-411 France 1.4944 Germany/Allemagne HR650 BS HR100 U.K./Royaume-UniBSA 341:1999 4 BSI 05-1999 Table 3 4 Nickel base alloys 4 Alliages base de nickel See Table 3.
32、Voir Tableau 3. Previous or other designations are given in parentheses. Entre parenthses, danciennes ou autres dsignations. Minimum shear stress Contrainte minimale de cisaillement MPa Material designation Dsignation du matriau Control document Document de contrle Designation origin Origine de la d
33、signation 340 Ni30Cu (Monel 400) NI-PD9201 (NI-P11) EN 2305 AECMA UNS N04400 QQ-N-281 U.S.A./tats-Unis N-U 30 NF L 21-203 France 2.4360 Germany/Allemagne DTD 204 BS HR100 U.K./Royaume-Uni 440 Ni19Cr0,4Ti (Nimonic 75) NI-PH1201 (NI-P91HT) EN 2402 AECMA N-C 20 T NF A 50-411 France 2.4630 Germany/Allem
34、agne HR 504 BS HR100 U.K./Royaume-Uni 440 UNS N06600 AS 7232 U.S.A./tats-Unis 440 Ni16Cr7Fe3TiNb1AI (Inconel X750) NI-PH2801 (NI-P901) AECMA AMS 5687 U.S.A./tats-Unis N-C 15 Fe France 440 NiCr21Fe18Mo9 (Hasteloy X) NI-PH2301 (NI-P93HT) AECMA N-C 22 FeD FranceBSA341:1999 BSI 05-1999 5 Table 4 5 Titan
35、ium alloys 5 Alliages de titane See Table 4. Voir Tableau 4. Previous or other designations are given in parentheses. Entre parenthses, danciennes ou autres dsignations. Minimum shear stress Contrainte minimale de cisaillement MPa Material designation Dsignation du matriau Control document Document
36、de contrle Designation origin Origine de la dsignation 350 TI-P99002 (TI-P02) EN 3378 AECMA U.S.A./tats-Unis T 40 NF L 21-110 France 3.7024 Germany/Allemagne T40 U.K./Royaume-Uni 345 Ti44,5Cb AMS 4982 U.S.A./tats-UnisBS A 341:1999 ISO/TR 12198:1998 BSI 389 Chiswick High Road London W4 4AL BSIBritish
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