SAE AMS 2809A-2007 Identification Titanium and Titanium Alloy Wrought Products《钛和钛合金锻造制品的鉴定》.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 ther
2、efrom, 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 2011 SAE International All rights reserved. No part of this
3、publication 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: +1 724-776-49
4、70 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org SAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/AMS2809A AEROSPACE MATERIAL SPECIFICATION AMS 2809 REV. A Issued 1986-01 Revised
5、 2007-08 Reaffirmed 2011-10 Superseding AMS 2809 Identification Titanium and Titanium Alloy Wrought Products RATIONALE AMS 2809A results from a Five Year Review and update of this specification. 1. SCOPE This specification covers procedures for identifying wrought products of titanium and titanium a
6、lloys. 2. APPLICABLE DOCUMENTS None. 3. TECHNICAL REQUIREMENTS 3.1 Bars and Wire Shall be identified as follows: 3.1.1 Each straight bar over 0.500 inch (12.50 mm) in nominal diameter or least width of flat surface shall be marked in a row of characters recurring at intervals not greater than 3 feet
7、 (900 mm) with the material specification number and its revision letter, if any, heat number, and manufacturers identification. The characters shall be of such size as to be legible, shall be applied using a suitable marking fluid whose residue shall contain not more than traces of halogen-bearing
8、compounds, and shall be removable in hot alkaline cleaning solution without rubbing. The markings shall have no deleterious effect on the product or its performance and shall be sufficiently stable to withstand normal handling. 3.1.2 Straight bars and wire 0.500 inch (12.50 mm) and under in nominal
9、diameter or least width of flat surface shall be securely bundled and identified by a durable tag marked with the purchase order number, the material specification number and its revision letter, if any, heat number, nominal size, and manufacturers identification and attached to each bundle or shall
10、 be boxed and the box marked with the same information. 3.1.3 Coiled bars and wire shall be securely bundled and identified by a durable tag marked with the purchase order number, the material specification number and its revision letter, if any, heat number, nominal size, and manufacturers identifi
11、cation and attached to each coil or shall be boxed and the box marked with the same information. SAE AMS 2809A Page 2 of 3 3.2 Sheet, Strip, and Plate Shall be identified as follows: 3.2.1 Each sheet, strip, and plate shall be marked on one face, in the respective location indicated below, with the
12、material specification number and its revision letter, if any, heat number, manufacturers identification, and nominal thickness. The characters shall be applied using a suitable marking fluid whose residue shall contain not more than traces of halogen-bearing compounds, and shall be removable in hot
13、 alkaline cleaning solution without rubbing. The markings shall have no deleterious effect on the product or its performance and shall be sufficiently stable to withstand normal handling. 3.2.1.1 Flat strip 6 inches (150 mm) and under in width shall be marked in one or more lengthwise rows of charac
14、ters recurring at intervals not greater than 3 feet (900 mm). 3.2.1.2 Flat sheet, flat strip over 6 inches (150 mm) in width and plate shall be marked in lengthwise rows of characters recurring at intervals not greater than 3 feet (900 mm), the rows being spaced not more than 6 inches (150 mm) apart
15、 and alternately staggered. 3.2.1.3 Coiled sheet and strip shall be marked near both the outside and inside ends of the coil; the markings shall be applied as in 3.2.1 or shall appear on a durable tag or label attached to the coil and marked with the information of 3.2.1. When the product is wound o
16、n cores, the tag or label may be attached to the core. 3.3 Aircraft Tubing Shall be identified as follows: 3.3.1 Aircraft Tubing Other Than Hydraulic 3.3.1.1 Straight tubes 0.029 inch (0.75 mm) and over in wall thickness and 0.500 inch (12.50 mm) and over in nominal OD, minor axis, or least width of
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