SANS 1700-2-21-2004 Fasteners Part 2 Screw threads Section 21 Aerospace - MJ threads - General requirements《紧固件 第2部分 螺纹 第21节 航空-MJ螺纹 一般要求》.pdf
《SANS 1700-2-21-2004 Fasteners Part 2 Screw threads Section 21 Aerospace - MJ threads - General requirements《紧固件 第2部分 螺纹 第21节 航空-MJ螺纹 一般要求》.pdf》由会员分享,可在线阅读,更多相关《SANS 1700-2-21-2004 Fasteners Part 2 Screw threads Section 21 Aerospace - MJ threads - General requirements《紧固件 第2部分 螺纹 第21节 航空-MJ螺纹 一般要求》.pdf(41页珍藏版)》请在麦多课文档分享上搜索。
1、 Collection of SANS standards in electronic format (PDF) 1. Copyright This standard is available to staff members of companies that have subscribed to the complete collection of SANS standards in accordance with a formal copyright agreement. This document may reside on a CENTRAL FILE SERVER or INTRA
2、NET SYSTEM only. Unless specific permission has been granted, this document MAY NOT be sent or given to staff members from other companies or organizations. Doing so would constitute a VIOLATION of SABS copyright rules. 2. Indemnity The South African Bureau of Standards accepts no liability for any
3、damage whatsoever than may result from the use of this material or the information contain therein, irrespective of the cause and quantum thereof. ICS 49.030.10 ISBN 0-626-15257-7 SANS 1700-2-21:2004 Edition 1 ISO 5855-1:1999 Edition 3 SOUTH AFRICAN NATIONAL STANDARD Fasteners Part 2: Screw threads
4、Section 21: Aerospace MJ threads General requirements This national standard is the identical implementation of ISO 5855-1:1999 and is adopted with the permission of the International Organization for Standardization. Published by Standards South Africa 1 dr lategan road groenkloof ! private bag x19
5、1 pretoria 0001 tel: 012 428 7911 fax: 012 344 1568 international code + 27 12 www.stansa.co.za Standards South Africa 2004 SANS 1700-2-21:2004 Edition 1 ISO 5855-1:1999 Edition 3 Table of changes Change No. Date Scope Abstract Specifies the general requirements for MJ threads used in aerospace cons
6、truction. Determines the basic triangular profile for MJ threads and gives a system for designating the diameter and pitch combinations. Keywords aerospace construction, fasteners, specifications. National foreword This South African standard was approved by National Committee StanSA TC 5120.01, Scr
7、ew threads and fasteners, in accordance with procedures of Standards South Africa, in compliance with annex 3 of the WTO/TBT agreement. AReference numberISO 5855-1:1999(E)INTERNATIONALSTANDARDISO5855-1Third edition1999-10-15Aerospace MJ threads Part 1:General requirementsAronautique et espace Fileta
8、ge MJ Partie 1: Exigences gnralesISO 5855-1:1999(E) ISO 1999All rights reserved. Unless otherwise specified, no part of this publication may be reproduced or utilized in any form or by any means, electronicor mechanical, including photocopying and microfilm, without permission in writing from the pu
9、blisher.International Organization for StandardizationCase postale 56 CH-1211 Genve 20 SwitzerlandInternet isoiso.chPrinted in SwitzerlandiiForewordISO (the International Organization for Standardization) is a worldwide federation of national standards bodies (ISOmember bodies). The work of preparin
10、g International Standards is normally carried out through ISO technicalcommittees. Each member body interested in a subject for which a technical committee has been established hasthe right to be represented on that committee. International organizations, governmental and non-governmental, inliaison
11、 with ISO, also take part in the work. ISO collaborates closely with the International ElectrotechnicalCommission (IEC) on all matters of electrotechnical standardization.International Standards are drafted in accordance with the rules given in the ISO/IEC Directives, Part 3.Draft International Stan
12、dards 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 5855-1 was prepared by Technical Committee ISO/TC 20, Aircraft and space
13、 vehicles,Subcommittee SC 4, Aerospace fastener systems.This third edition cancels and replaces the second edition (ISO 5855-1:1988), of which it constitutes a technicalrevision.ISO 5855 consists of the following parts, under the general title Aerospace MJ threads:Part 1: General requirementsPart 2:
14、 Limit dimensions for bolts and nutsPart 3: Limit dimensions for fittings for fluid systemsINTERNATIONAL STANDARD ISO ISO 5855-1:1999(E)1Aerospace MJ threads Part 1:General requirements1 ScopeThis part of ISO 5855 specifies the general requirements for MJ threads used in aerospace construction.It de
15、termines the basic triangular profile for this type of thread and gives a system for designating the diameter andpitch combinations. For all diameters 1,6 mm to 300 mm, it offers in the form of tables the basic dimensions andtolerances for a selection of diameter and pitch combinations. It also prov
16、ides the method of calculation for thedimensions and tolerances for any diameter and pitch combination not given in the tables, including threads with adiameter in excess of 300 mm.For limit dimensions for bolts and nuts of nominal diameter 1,6 mm to 39 mm, see ISO 5855-2. For limit dimensions forfi
17、ttings for fluid systems, see ISO 5855-3.2 Normative referenceThe following normative document contains provisions which, through reference in this text, constitute provisions of thispart of ISO 5855. For dated references, subsequent amendments to, or revisions of, any of these publications do notap
18、ply. However, parties to agreements based on this part of ISO 5855 are encouraged to investigate the possibility ofapplying the most recent edition of the normative document indicated below. For undated references, the latest editionof the normative document referred to applies. Members of ISO and I
19、EC maintain registers of currently validInternational Standards.ISO 965-1:1998, ISO general-purpose metric screw threads Tolerances Part 1: Principles and basic data.3 Term and definitionFor the purpose of this part of ISO 5855, the following term and definition apply.3.1basic profiletheoretical pro
20、file, in an axial plane, corresponding to the basic dimensions (without tolerances) of the thread, i.e.major diameter, pitch diameter and minor diameterSee Figure 1.4 Basic profile4.1 SymbolsSee Figure 1.ISO 5855-1:1999(E) ISO24.2 DimensionsSee Figure 1 and Table 1.Basic deviations shall be applied
21、to the basic dimensions.whereD is the basic major diameter of internal threadD2is the basic pitch diameter of internal threadD1is the basic minor diameter of internal threadd is the basic major diameter of external threadd2is the basic pitch diameter of external threadd1is the basic minor diameter o
22、f external threadH is the height of fundamental triangleP is the pitchaAxis of threadFigure 1 Basic profile ISOISO 5855-1:1999(E)3Table 1 DimensionsISO 5855-1:1999(E) ISO45 Position and form of limit profiles5.1 External threadsThe actual thread profile is located between the limit profiles shown in
23、 Figures 2 and 3.Within these limits, any continuous, non-reversing curve is permitted, provided that it comprises radii no less than0,150 11P.aPitch D PbBasic and maximum profilescBasic profiledMinimum profileFigure 2 Limit profiles for external threads (clearance may be nil) ISOISO 5855-1:1999(E)5
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