ISO 3209-2016 Aerospace - Nuts anchor self-locking floating two lug with counterbore with MJ threads classifications 1 100 MPa (at ambient temperature ) 235 deg.pdf
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1、 ISO 2016 Aerospace Nuts, anchor, self-locking, floating, two lug, with counterbore, with MJ threads, classifications: 1 100 MPa (at ambient temperature)/ 235 C, 1 100 MPa (at ambient temperature)/315 C and 1 100 MPa (at ambient temperature)/ 425 C Dimensions Aronautique et espace crous river, frein
2、age interne, flottants, double patte, avec chambrage, filetage MJ, classifications: 1 100 MPa ( temprature ambiante)/235 C, 1 100 MPa ( temprature ambiante)/315 C et 1 100 MPa ( temprature ambiante)/425 C Dimensions INTERNATIONAL STANDARD ISO 3209 Third edition 2016-02-15 Reference number ISO 3209:2
3、016(E) ISO 3209:2016(E)ii ISO 2016 All rights reserved COPYRIGHT PROTECTED DOCUMENT ISO 2016, Published in Switzerland All rights reserved. Unless otherwise specified, no part of this publication may be reproduced or utilized otherwise in any form or by any means, electronic or mechanical, including
4、 photocopying, or posting on the internet or an intranet, without prior written permission. Permission can be requested from either ISO at the address below or ISOs member body in the country of the requester. ISO copyright office Ch. de Blandonnet 8 CP 401 CH-1214 Vernier, Geneva, Switzerland Tel.
5、+41 22 749 01 11 Fax +41 22 749 09 47 copyrightiso.org www.iso.org ISO 3209:2016(E)Foreword iv Introduction v 1 Scope . 1 2 Normative references 1 3 Configuration and dimensions . 1 ISO 2016 All rights reserved iii Contents Page ISO 3209:2016(E) Foreword ISO (the International Organization for Stand
6、ardization) 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
7、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. The procedures u
8、sed to develop this document and those intended for its further maintenance are described in the ISO/IEC Directives, Part 1. In particular the different approval criteria needed for the different types of ISO documents should be noted. This document was drafted in accordance with the editorial rules
9、 of the ISO/IEC Directives, Part 2 (see www.iso.org/directives). Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. ISO shall not be held responsible for identifying any or all such patent rights. Details of any patent rights identif
10、ied during the development of the document will be in the Introduction and/or on the ISO list of patent declarations received (see www.iso.org/patents). Any trade name used in this document is information given for the convenience of users and does not constitute an endorsement. For an explanation o
11、n the meaning of ISO specific terms and expressions related to conformity assessment, as well as information about ISOs adherence to the WTO principles in the Technical Barriers to Trade (TBT) see the following URL: Foreword - Supplementary information. The committee responsible for this document is
12、 ISO/TC 20, Aircraft and space vehicles, Subcommittee SC 4, Aerospace fastener systems. This third edition cancels and replaces the second edition (ISO 3209:1998), of which it constitutes a minor revision.iv ISO 2016 All rights reserved ISO 3209:2016(E) Introduction The dimensions specified in this
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