ISO-3230-1998.pdf

A Reference number ISO 3230:1998(E) INTERNATIONAL STANDARD ISO 3230 First edition 1998-03-15 Aerospace Rivets, solid, 100° normal countersunk head with dome, metallic material, with or without surface treatment Dimensions Aeronautique et espace Rivets ordinaires, à tête fraisée 100° normale avec dôme, en matériau métallique, avec ou sans traitement de surface Dimensions Copyright International Organization for Standardization Provided by IHS under license with ISO Licensee=NASA Technical Standards 1/9972545001 Not for Resale, 04/25/2007 23:16:13 MDTNo reproduction or networking permitted without license from IHS -,-,- ISO 3230:1998(E) © ISO 1998 All rights reserved. Unless otherwise specified, no part of this publication may be reproduced or utilized in any form or by any means, electronic or mechanical, including photocopying and microfilm, without permission in writing from the publisher. International Organization for Standardization Case postale 56 CH-1211 Genève 20 Switzerland Internetcentraliso.ch X.400c=ch; a=400net; p=iso; o=isocs; s=central Printed in Switzerland ii 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 subject 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) on all matters of electrotechnical standardization. Draft International Standards adopted by the technical committees are circulated to the member bodies for voting. Publication as an International Standard requires approval by at least 75 % of the member bodies casting a vote. International Standard ISO 3230 was prepared by Technical 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 ISO Licensee=NASA Technical Standards 1/9972545001 Not for Resale, 04/25/2007 23:16:13 MDTNo reproduction or networking permitted without license from IHS -,-,- INTERNATIONAL STANDARD © ISOISO 3230:1998(E) 1 Aerospace Rivets, solid, 100°normal countersunk with dome, metallic material, with or without surface treatment Dimensions 1 Scope This International Standard specifies the dimensions of solid rivets, 100° normal countersunk head with dome, in metallic material, with or without surface treatment. It is intended for the drawing up of aerospace product standards. 2 Normative reference The following standard contains provisions which, through reference in this text, constitute provisions of this International Standard. At the time of publication, the edition indicated was valid. All standards are subject to revision, and parties to agreements based on this International Standard are encouraged to investigate the possibility of applying the most recent edition of the standard indicated below. Members of IEC and ISO maintain registers of currently valid International Standards. ISO 286-2:1988, ISO system of limits and fits Part 2: Tables of standard tolerance grades and limit deviations for holes and shafts. 3Configuration and dimensions See figure 1 and tables 1 to 3. Dimensions and tolerances are expressed in millimetres. They are applicable after any surface treatment. Copyright International Organization for Standardization Provided by IHS under license with ISO Licensee=NASA Technical Standards 1/9972545001 Not for Resale, 04/25/2007 23:16:13 MDTNo reproduction or networking permitted without license from IHS -,-,- ISO 3230:1998(E) © ISO 2 1) The length range is limited (see tables 2 and 3). 2) Drill start optional, only for corrosion-resistant steels, nickel alloys, commercially pure titanium, titanium alloys. 3) Area of this datum shall be included between L5 and L5 + 1. Figure 1 Table 1 Dimensions (except length L1) DiameterD1 1)D2 3)D3D4D5D6D7L2L3L4L5L6R code 0 d11 2)min.max.min.max.min.max.min.min. - 0,08 max. min.± 0,08 0161,632,72,72,22,21,62,25 _ 0,590,030,412 _ 02023,73,33,32,62,62,02,89 _ 0,720,040,442,2 _ 0,15 0252,54,654,154,153,303,32,53,862,01,70,910,050,432,40,80,5 03035,554,954,954,00434,52,42,11,070,060,542,50,90,6 0353,56,55,85,84,64,63,55,142,80 2,451,260,070,672,81,050,70 04047,46,66,65,35,34,05,783,22,81,430,080,7831,20,8 05059,258,258,256,606,65,07,714,03,51,80,753,81,51,00,25 060611,19,99,98,08694,84,22,150,10,984,11,81,2 080814,813,613,610,810,88,012,216,45,62,871,194,82,41,6 1001018,517,317,313,613,610,015,43873,591,395,532 1) Over length (L5 - L2), D1 max. may increase by 0,03. 2) In accordance with ISO 286-2 3) Maximum condition Copyright International Organization for Standardization Provided by IHS under license with ISO Licensee=NASA Technical Standards 1/9972545001 Not for Resale, 04/25/2007 23:16:13 MDTNo reproduction or networking permitted without license from IHS -,-,- © ISO ISO 3230:1998(E) 3 Table 2 Lengths L1 for rivets in aluminium and aluminium alloys Diameter code016020025030035040050060080100 Length Shape of tail end 1) codeL1 +0,5 L1 +0,5 AAABABABABABABABAB 0033XX 0044XXXXXXXX 0055XXXXXXXX 0066XXXXXXXXXX 0077XXXXXXXXXX 0088XXXXXXXXXXXX 0099XXXXXXXXXXXX 01010XXXXXXXXXXXXXX 01111XXXXXXXXXXXXXX 01212XXXXXXXXXXXXXX 01313XXXXXXXXXXXXXXXXXX 01414XXXXXXXXXXXXXXXXXX 01515XXXXXXXXXXXXXXXXXX 01616XXXXXXXXXXXXXXXXXX 01717XXXXXXXXXXXXXXXX 01818XXXXXXXXXXXXXXXX 01919XXXXXXXXXXXXXXX 02020XXXXXXXXXXXXXXX 02222XXXXXXXXXXXXXX 02424XXXXXXXXXXXXXX 02626XXXXXXXXXXXX 02828XXXXXXXXXXXX 03030XXXXXXXXXXX 03232XXXXXXXXXXX 03535XXXXXXXXXX 04040XXXXXXX 04545XXXXXX 05050XXXXX 05555XXXX 06060XXXX 1) Form A : non-radiused tail end (see figure 1) 1) Form B : radiused tail end (see figure 1) Copyright International Organization for Standardization Provided by IHS under license with ISO Licensee=NASA Technical Standards 1/9972545001 Not for Resale, 04/25/2007 23:16:13 MDTNo reproduction or networking permitted without license from IHS -,-,- ISO 3230:1998(E) © ISO 4 Table 3 Lengths L1 for rivets in nickel alloys, corrosion-resistant steels, commercially pure titanium and titanium alloys Diameter code016020025030035040050060 Length Shape of tail end 1) codeL1 +0,5 L1 +0,5 AAABABABABABAB 0033XX 0044XXXXXXXX 0055XXXXXXXX 0066XXXXXXXXXX 0077XXXXXXXXXX 0088XXXXXXXXXXXX 0099XXXXXXXXXXXX 01010XXXXXXXXXXXXXX 01111XXXXXXXXXXXXXX 01212XXXXXXXXXXXXXX 01313XXXXXXXXXXXXXX 01414XXXXXXXXXXXXXX 01515XXXXXXXXXXXXXX 01616XXXXXXXXXXXXXX 01717XXXXXXXXXXXX 01818XXXXXXXXXXXX 01919XXXXXXXXXX 02020XXXXXXXXXX 02222XXXXXXXX 02424XXXXXXXX 02626XXXXXX 02828XXXXXX 03030XXXX 03232XXXX 03535XX 04040XX 1) Form A : non-radiused tail end (see figure 1) 1) Form B : radiused tail end (see figure 1) Copyright International Organization for Standardization Provided by IHS under license with ISO Licensee=NASA Technical Standards 1/9972545001 Not for Resale, 04/25/2007 23:16:13 MDTNo reproduction or networking permitted without license from IHS -,-,- Copyright International Organization for Standardization Provided by IHS under license with ISO Licensee=NASA Technical Standards 1/9972545001 Not for Resale, 04/25/2007 23:16:13 MDTNo reproduction or networking permitted without license from IHS -,-,- ISO 3230:1998(E) © ISO ICS 49.030.99 Descriptors: aircraft industry, fasteners, rivets, countersunk head rivets, form specifications, dimensions, dimensional tolerances. Price based on 4 pages Copyright International Organization for Standardization Provided by IHS under license with ISO Licensee=NASA Technical Standards 1/9972545001 Not for Resale, 04/25/2007 23:16:13 MDTNo reproduction or networking permitted without license from IHS -,-,-