Aerospace — Omega clamps (saddle clamps) for fluid systems — Dimensions

ISO 8177:2015 specifies maximum and minimum dimensions for omega clamps (saddle clamps) installed by means of two bolts with nominal diameters of 5 mm. The specified dimensions define a dimensional envelope. This International Standard shall not be considered as an inter-changeability standard. The tolerances for each type of clamp are to be defined in the parts standards drawings.

Aéronautique et espace — Colliers en oméga pour systèmes de fluides — Dimensions

General Information

Status
Withdrawn
Publication Date
14-Jun-2015
Withdrawal Date
14-Jun-2015
Current Stage
9599 - Withdrawal of International Standard
Completion Date
08-Dec-2021
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ISO 8177:2015 - Aerospace -- Omega clamps (saddle clamps) for fluid systems -- Dimensions
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INTERNATIONAL ISO
STANDARD 8177
Third edition
2015-07-01
Aerospace — Omega clamps (saddle
clamps) for fluid systems — Dimensions
Aéronautique et espace — Colliers en oméga pour systèmes de
fluides — Dimensions
Reference number
ISO 8177:2015(E)
©
ISO 2015

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ISO 8177:2015(E)

COPYRIGHT PROTECTED DOCUMENT
© ISO 2015, 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 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 ISO’s member body in the country of
the requester.
ISO copyright office
Ch. de Blandonnet 8 • CP 401
CH-1214 Vernier, Geneva, Switzerland
Tel. +41 22 749 01 11
Fax +41 22 749 09 47
copyright@iso.org
www.iso.org
ii © ISO 2015 – All rights reserved

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ISO 8177:2015(E)

Contents Page
Foreword .iv
1 Scope . 1
2 Normative references . 1
3 Field of application . 1
4 Field of use . 1
5 Description . 1
6 Dimensions . 2
© ISO 2015 – All rights reserved iii

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ISO 8177:2015(E)

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.
The procedures used 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 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 identified 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 on the meaning of ISO specific terms and expressions related to conformity
assessment, as well as information about ISO’s 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 ISO/TC 20, Aircraft and space vehicles, SC 10, Aerospace
fluid systems and components.
This third edition cancels and replaces the s
...

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