ISO TR 12198-1998 Aerospace - Rivets solid - Materials《航空航天 实心铆钉 材料》.pdf

1、AReference numberNumro de rfrenceISO/TR 12198:1998(E/F)TECHNICALREPORTRAPPORTTECHNIQUEISO/TR12198First editionPremire dition1998-11-01Aerospace Rivets, solid MaterialsAronautique et espace Rivets ordinaires MatriauxCopyright International Organization for Standardization Provided by IHS under licens

2、e with ISONot for ResaleNo reproduction or networking permitted without license from IHS-,-,-ISO/TR 12198:1998(E/F) ISO 1998All rights reserved. Unless otherwise specified, no part of this publication may be reproducedor utilized in any form or by any means, electronic or mechanical, including photo

3、copying andmicrofilm, without permission in writing from the publisher. / Droits de reproduction rservs.Sauf prescription diffrente, aucune partie de cette publication ne peut tre reproduite niutilise sous quelque forme que ce soit et par aucun procd, lectronique ou mcanique, ycompris la photocopie

4、et les microfilms, sans laccord crit de lditeur.International Organization for StandardizationCase postale 56 CH-1211 Genve 20 SwitzerlandInternet isoiso.chPrinted in Switzerland/Imprim en SuisseiiForewordISO (the International Organization for Standardization) is a worldwidefederation of national s

5、tandards bodies (ISO member bodies). The work ofpreparing International Standards is normally carried out through ISOtechnical committees. Each member body interested in a subject for whicha technical committee has been established has the right to be representedon that committee. International orga

6、nizations, governmental and non-governmental, in liaison with ISO, also take part in the work. ISOcollaborates closely with the International Electrotechnical Commission(IEC) on all matters of electrotechnical standardization.The main task of technical committees is to prepare InternationalStandards

7、, but in exceptional circumstances a technical committee maypropose the publication of a Technical Report of one of the following types: type 1, when the required support cannot be obtained for thepublication of an International Standard, despite repeated efforts; type 2, when the subject is still u

8、nder technical development or wherefor any other reason there is the future but not immediate possibility ofan agreement on an International Standard; type 3, when a technical committee has collected data of a differentkind from that which is normally published as an International Standard(“state of

9、 the art”, for example).Technical Reports of types 1 and 2 are subject to review within three yearsof publication, to decide whether they can be transformed into InternationalStandards. Technical Reports of type 3 do not necessarily have to bereviewed until data they provide are considered to be no

10、longer valid oruseful.ISO/TR 12198, which is a Technical Report of type 3, was prepared byTechnical Committee ISO/TC 20, Aircraft and space vehicles,Subcommittee SC 4, Aerospace fastener systems.Copyright International Organization for Standardization Provided by IHS under license with ISONot for Re

11、saleNo reproduction or networking permitted without license from IHS-,-,-ISO ISO/TR 12198:1998(E/F)iiiAvant-proposLISO (Organisation internationale de normalisation) est une fdrationmondiale dorganismes nationaux de normalisation (comits membres delISO). Llaboration des Normes internationales est en

12、 gnral confie auxcomits techniques de lISO. Chaque comit membre intress par unetude a le droit de faire partie du comit technique cr cet effet. Lesorganisations internationales, gouvernementales et non gouvernementales,en liaison avec lISO, participent galement aux travaux. LISO collaboretroitement

13、avec la Commission lectrotechnique internationale (CEI) ence qui concerne la normalisation lectrotechnique.La tche principale des comits techniques est dlaborer les Normesinternationales. Exceptionnellement, un comit technique peut proposer lapublication dun rapport technique de lun des types suivan

14、ts: type 1, lorsque, en dpit de maints efforts, laccord requis ne peut treralis en faveur de la publication dune Norme internationale; type 2, lorsque le sujet en question est encore en cours dedveloppement technique ou lorsque, pour toute autre raison, lapossibilit dun accord pour la publication du

15、ne Norme internationalepeut tre envisage pour lavenir mais pas dans limmdiat; type 3, lorsquun comit technique a runi des donnes de naturediffrente de celles qui sont normalement publies comme Normesinternationales (ceci pouvant comprendre des informations sur ltatde la technique, par exemple).Les r

16、apports techniques des types 1 et 2 font lobjet dun nouvel examentrois ans au plus tard aprs leur publication afin de dcider ventuellementde leur transformation en Normes internationales. Les rapports techniquesde type 3 ne doivent pas ncessairement tre rviss avant que lesdonnes fournies ne soient p

17、lus juges valables ou utiles.LISO/TR 12198, rapport technique du type 3, a t labor par le comittechnique ISO/TC 20, Aronautique et espace, sous-comit SC 4,lments de fixation pour constructions arospatiales.Copyright International Organization for Standardization Provided by IHS under license with IS

18、ONot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Copyright International Organization for Standardization Provided by IHS under license with ISONot for ResaleNo reproduction or networking permitted without license from IHS-,-,-TECHNICAL REPORTRAPPORT TECHNIQUEISO I

19、SO/TR 12198:1998(E/F)1Aerospace Rivets, solid MaterialsAronautique et espace Rivets ordinaires Matriaux1 ScopeThis Technical Report gives, for each material familyand for each minimum shear stress, the material(s) tobe used for the manufacture of solid rivets.These materials ensure interchangeabilit

20、y of the prod-ucts concerned.This Technical Report applies when referenced in therelevant standard.2 Aluminium alloysSee table 1.Previous or other designations are given in parenth-eses.1 Domaine dapplicationLe prsent Rapport technique indique, pour chaquefamille de matriaux et chaque contrainte min

21、imale decisaillement, le ou les matriaux utiliser pour lafabrication des rivets ordinaires.Ces matriaux assurent linterchangeabilit des pro-duits concerns.Le prsent Rapport technique sapplique chaque foisquil est cit dans la norme concerne.2 Alliages daluminiumVoir tableau 1.Entre parenthses, dancie

22、nnes ou autres dsigna-tions.Copyright International Organization for Standardization Provided by IHS under license with ISONot for ResaleNo reproduction or networking permitted without license from IHS-,-,-ISO/TR 12198:1998(E/F)ISO2Table 1/Tableau 1Minimum shear stress Material designation Control d

23、ocument Designation originContrainte minimalede cisaillementDsignation du matriau Document de contrle Originede la dsignationMPaAl99-5 AL-P1050A (1050A) EN 2114 AECMA 1100 QQ-A-430 U.S.A./tats-UnisA5 NF A 50-411 France3.0255.26 Germany/AllemagneL36 BS L100 U.K./Royaume-UniAl4Cu0,7Mg0,7Mn AL-P2017A (

24、2017A) EN 2116 AECMA260 2017 QQ-A-430 U.S.A./tats-UnisAU4G AIR 9150 France3.1324.4 Germany/AllemagneL37 BS L100 U.K./Royaume-UniAl4,4Cu1,5Mg0,6Mn 260 2024 QQ-A-430 U.S.A./tats-UnisAU4G1 NF A 50-411 France3.1354.4 Germany/AllemagneAl2,6Cu0,3Mg 2117 QQ-A-430 U.S.A./tats-Unis195 AU2G AIR 9150 France3.1

25、124.4 Germany/AllemagneL86 BS L100 U.K./Royaume-UniAl5Mg0,3Mn AL-P5056A (5056A) EN 2117 AECMA170 5056 QQ-A-430 U.S.A./tats-UnisAG5 MC AIR 9150 France3.3354.2 Germany/AllemagneL58 BS L100 U.K./Royaume-UniAl6,2Zn2,3Cu2,2Mg0,1Zr 283 7050 QQ-A-430 U.S.A./tats-Unis3.4144 Germany/Allemagne210Al6,3Cu0,3Mn0

26、,06Ti2219QQ-A-430U.S.A./tats-Unis240Al4Cu0.4Mn0.2MgV65Russia/RussieCopyright International Organization for Standardization Provided by IHS under license with ISONot for ResaleNo reproduction or networking permitted without license from IHS-,-,-ISO ISO/TR 12198:1998(E/F)33 Corrosion resisting steels

27、See table 2.Previous or other designations are given in parenth-eses.3 Aciers rsistant la corrosionVoir tableau 2.Entre parenthses, danciennes ou autres dsigna-tions.Table 2/Tableau 2Minimum shear stress Material designation Control document Designation originContrainte minimalede cisaillementDsigna

28、tion du matriau Document de contrle Originede la dsignationMPaFe18Cr12Ni (AISI 304 L) FE-PA3901 (FE-PA11) EN 2470 AECMA330 UNS S0500 AMS 5686 U.S.A./tats-UnisZ2 CN 18-10 AIR 9150 France1.4544 Germany/AllemagneDTD 5036 BS S100 U.K./Royaume-UniFe25Ni15Cr2Ti1,3Mo0,3V(A286)FE-PA2601 (FE-PA92HT) EN 2119

29、AECMA550 UNS S66286 AMS 5734 U.S.A./tats-UnisE Z6 NCT 25 NF A 50-411 France1.4944 Germany/AllemagneHR650 BS HR100 U.K./Royaume-UniCopyright International Organization for Standardization Provided by IHS under license with ISONot for ResaleNo reproduction or networking permitted without license from

30、IHS-,-,-ISO/TR 12198:1998(E/F)ISO44 Nickel base alloysSee table 3.Previous or other designations are given in parenth-eses.4 Alliages base de nickelVoir tableau 3.Entre parenthses, danciennes ou autres dsigna-tions.Table 3/Tableau 3Minimum shear stress Material designation Control document Designati

31、on originContrainte minimalede cisaillementDsignation du matriau Document de contrle Originede la dsignationMPaNi30Cu (Monel 400) NI-PD9201 (NI-P11) EN 2305 AECMA340 UNS N04400 QQ-N-281 U.S.A./tats-UnisN-U 30 NF L 21-203 France2.4360 Germany/AllemagneDTD 204 BS HR100 U.K./Royaume-UniNi19Cr0,4Ti (Nim

32、onic 75) NI-PH1201 (NI-P91HT) EN 2402 AECMA440 N-C 20 T NF A 50-411 France2.4630 Germany/AllemagneHR 504 BS HR100 U.K./Royaume-Uni440 UNS N06600 AS 7232 U.S.A./tats-UnisNi16Cr7Fe3TiNb1Al(Inconel X750)440 NI-PH2801 (NI-P901) AECMAAMS 5687 U.S.A./tats-UnisN-C 15 Fe FranceNiCr21Fe18Mo9 (Hasteloy X) 440

33、 NI-PH2301 (NI-P93HT) AECMAN-C 22 FeD FranceCopyright International Organization for Standardization Provided by IHS under license with ISONot for ResaleNo reproduction or networking permitted without license from IHS-,-,-ISO ISO/TR 12198:1998(E/F)55 Titanium alloysSee table 4.Previous or other desi

34、gnations are given in parenth-eses.5 Alliages de titaneVoir tableau 4.Entre parenthses, danciennes ou autres dsigna-tions.Table 4/Tableau 4Minimum shear stress Material designation Control document Designation originContrainte minimalede cisaillementDsignation du matriau Document de contrle Origined

35、e la dsignationMPaTI-P99002 (TI-P02) EN 3378 AECMA350 U.S.A./tats-UnisT 40 NF L 21-110 France3.7024 Germany/AllemagneT40 U.K./Royaume-Uni345Ti44,5CbAMS 4982U.S.A./tats-UnisCopyright International Organization for Standardization Provided by IHS under license with ISONot for ResaleNo reproduction or

36、networking permitted without license from IHS-,-,-ISO/TR12198:1998(E/F)ISOICS 49.030.99Descriptors: aircraft industry, fasteners, rivets, full rivets, specifications, material specifications, interchangeability. / Descripteurs:industrie aronautique, lment de fixation, rivet, rivet plein, spcification, spcification de matire, interchangeabilit.Price based on 5 pages / Prix bas sur 5 pagesCopyright International Organization for Standardization Provided by IHS under license with ISONot for ResaleNo reproduction or networking permitted without license from IHS-,-,-