SAE AIR 1418A-1996 Flexure Fatigue Strength of Tube Fitting Joints《管配件接头的弯曲疲劳强度》.pdf

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1、_SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising theref

2、rom, is the sole responsibility of the user.” SAE reviews each technical report at least every five years at which time it may be revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions.Copyright 2013 SAE International All rights reserved. No part of this pub

3、lication may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: +1 724-776-4970

4、(outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/AIR1418AAEROSPACEINFORMATIONREPORTAIR1418 REV. A Issued 1980-04 Revised 1996-08 Reaf

5、firmed 2013-01 Superseding AIR1418 Flexure Fatigue Strength of Tube Fitting Joints RATIONALEAIR1418A has been reaffirmed to comply with the SAE five-year review policy. SAE AIR1418A Page 2 of 15 SAE AIR1418A Page 3 of 15 SAE AIR1418A Page 4 of 15 SAE AIR1418A Page 5 of 15 SAE AIR1418A Page 6 of 15 SAE AIR1418A Page 7 of 15 SAE AIR1418A Page 8 of 15 SAE AIR1418A Page 9 of 15 SAE AIR1418A Page 10 of 15 SAE AIR1418A Page 11 of 15 SAE AIR1418A Page 12 of 15 SAE AIR1418A Page 13 of 15 SAE AIR1418A Page 14 of 15 SAE AIR1418A Page 15 of 15

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