SAE AMS 4173F-2013 Aluminum Alloy Extrusions 1 0Mg - 0 60Si - 0 30Cu - 0 20Cr (6061-T6511 or T6510) Solution Heat Treated Stress Relieved by Stretching Straightened and Precipitati.pdf
《SAE AMS 4173F-2013 Aluminum Alloy Extrusions 1 0Mg - 0 60Si - 0 30Cu - 0 20Cr (6061-T6511 or T6510) Solution Heat Treated Stress Relieved by Stretching Straightened and Precipitati.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4173F-2013 Aluminum Alloy Extrusions 1 0Mg - 0 60Si - 0 30Cu - 0 20Cr (6061-T6511 or T6510) Solution Heat Treated Stress Relieved by Stretching Straightened and Precipitati.pdf(6页珍藏版)》请在麦多课文档分享上搜索。
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 there
2、from, is the sole responsibility of the user.” SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 2013 SAE International All rights reserved. No part of this publication m
3、ay 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 (outside U
4、SA) 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/AMS4173F AEROSPACE MATERIAL SPECIFICATION AMS4173 REV. F Issued 1969-11 Reaffirmed 2008-05 Re
5、vised 2013-04 Superseding AMS4173E Aluminum Alloy, Extrusions 1.0Mg - 0.60Si - 0.30Cu - 0.20Cr (6061-T6511 or T6510) Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Precipitation Heat Treated (Composition similar to A96061) RATIONALE AMS4173F was revised to add provisions for
6、 billet types for tubing (1.1.1), for T6510 temper material (3.2.2), and for press solution heat treatment (3.2.3), and revises Sampling and Testing (4.3.1) and Reports (4.4). 1. SCOPE 1.1 Form This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing
7、. 1.1.1 Tubing shall be additionally classified as follows: Type Description I - Seamless tubing extruded from hollow billets using die and mandrel II - Tubing extruded from solid billets using porthole or spider die or similar tooling When no Type is specified, Type I shall apply. 1.2 Application T
8、hese extrusions have been used typically for parts requiring moderate strength and where distortion during machining must be minimized, but usage is not limited to such applications. 2. APPLICABLE DOCUMENTS The issue of the following documents in effect on the date of the purchase order forms a part
9、 of this specification to the extent specified herein. The supplier may work to a subsequent revision of a document unless a specific document issue is specified. When the referenced document has been cancelled and no superseding document has been specified, the last published issue of that document
10、 shall apply. SAE AMS4173F Page 2 of 6 2.1 SAE Publications Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org. AMS2355 Quality Assurance. Sampling and Testing, Aluminum Alloys and
11、Magnesium Alloy, Wrought Products (Except Forging Stock), and Rolled, Forged, or Flash Welded Rings AMS2772 Heat Treatment of Aluminum Alloy Raw Materials AS1990 Aluminum Alloy Tempers 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, P
12、A 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM B 594 Ultrasonic Inspection of Aluminum-Alloy Wrought Products for Aerospace Applications ASTM B 660 Packaging/Packing of Aluminum and Magnesium Products ASTM B 666/B 666M Identification Marking of Aluminum and Magnesium Products ASTM B 807/B 807M
13、Extrusion Press Solution Heat Treatment for Aluminum Alloys 2.3 ANSI Publications Available from American National Standards Institute, 25 West 43rd Street, New York, NY 10036-8002, Tel: 212-642-4900, www.ansi.org. ANSI H35.2 Dimensional Tolerances for Aluminum Mill Products ANSI H35.2M Dimensional
14、Tolerances for Aluminum Mill Products (Metric) 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the percentages by weight shown in Table 1, determined in accordance with AMS2355. TABLE 1 - COMPOSITION Element min max Silicon 0.40 0.8 Iron - 0.7 Copper 0.15 0.40 Manganese - 0.15 Magnesium 0
15、.8 1.2 Chromium 0.04 0.35 Zinc - 0.25 Titanium - 0.15 Other Elements, each - 0.05 Other Elements, total - 0.15 Aluminum remainder SAE AMS4173F Page 3 of 6 3.2 Condition Material shall be produced in one of the following tempers. If no temper is specifed, Temper T6511 shall be supplied. 3.2.1 Temper
16、T6511 Solution heat treated, stress relieved by stretching to produce a nominal permanent set of 1.5%, but not less than 1% nor more than 3%, and precipitation heat treated to the T6511 temper (See AS1990). Extrusions may receive minor straightening, after stretching, of an amount necessary to meet
17、the requirements of 3.5. 3.2.1.1 Extrusions shall be supplied with an as-extruded surface finish; light polishing to remove minor surface imperfections is permissible provided such imperfections can be removed within specified dimensional tolerances. 3.2.2 Temper T6510 Solution heat treated, stress
18、relieved by stretching to produce a nominal permanent set of 1.5%, but not less than 1% nor more than 3%, and precipitation heat treated to the T6510 temper (See AS1990). Extrusions shall receive no additional straightening or stretching to meet requirements of 3.5. 3.2.3 Extrusions shall be supplie
19、d with the as-extruded surface finish; light polishing to remove minor surface imperfections is permissible provided such imperfections can be removed within specified dimensional tolerances. 3.2.4 Heat Treatment shall be classified as follows: Class Description 1 Furnace solution heat treated in ac
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