SAE AMS 4161H-2013 Aluminum Alloy Extrusions 1 0Mg - 0 60Si - 0 28Cu - 0 20Cr (6061-T4) Solution Heat Treated and Naturally Aged (UNS A96061)《溶解热处理和自然老化铝合金挤压制品1 0Mg 0 60Si 0 28Cu 0.pdf
《SAE AMS 4161H-2013 Aluminum Alloy Extrusions 1 0Mg - 0 60Si - 0 28Cu - 0 20Cr (6061-T4) Solution Heat Treated and Naturally Aged (UNS A96061)《溶解热处理和自然老化铝合金挤压制品1 0Mg 0 60Si 0 28Cu 0.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4161H-2013 Aluminum Alloy Extrusions 1 0Mg - 0 60Si - 0 28Cu - 0 20Cr (6061-T4) Solution Heat Treated and Naturally Aged (UNS A96061)《溶解热处理和自然老化铝合金挤压制品1 0Mg 0 60Si 0 28Cu 0.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/AMS4161H AEROSPACE MATERIAL SPECIFICATION AMS4161 REV. H Issued 1960-01 Reaffirmed 2010-05 Re
5、vised 2013-04 Superseding AMS4161G Aluminum Alloy, Extrusions 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061-T4) Solution Heat Treated and Naturally Aged (Composition similar to UNS A96061) RATIONALE AMS4161H adds provisions for billet types for tubing (1.1.1) and for press solution heat treatment (3.2.2),
6、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, shapes, profiles and tubing. 1.1.1 Tubing Tubing shall be additionally classified as follows: Type Description I - Seamless tubing extru
7、ded 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 These products have been used typically for parts requiring moderate strength, especially where such pa
8、rts require brazing or welding during fabrication, 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 of this specification to the extent specified herein. The supplier may work to a sub
9、sequent 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 shall apply. SAE AMS4161H Page 2 of 6 2.1 SAE Publications Available from SAE Intern
10、ational, 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 Magnesium Alloy, Wrought Products (Except Forging Stock), and Rolled, Forged, or Flas
11、h 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, PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM B 594 Ultrasonic Inspection of Al
12、uminum-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 Extrusion Press Solution Heat Treatment for Aluminum Alloys 2.3 ANSI Publications Ava
13、ilable 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 Tolerances for Aluminum Mill Products (Metric) 3. TECHNICAL REQUIREMENTS 3.1 Composit
14、ion 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 0.8 1.2 Chromium 0.04 0.35 Zinc - 0.25 Titanium - 0.15 Other Elements, each - 0.05 Oth
15、er Elements, total - 0.15 Aluminum remainder SAE AMS4161H Page 3 of 6 3.2 Condition Solution heat treated and naturally aged to the T4 temper (See AS1990). 3.2.1 Extrusions shall be supplied with the as-extruded surface finish; light polishing to remove minor surface imperfections is permissible pro
16、vided such imperfections can be removed within specified dimensional tolerances. 3.2.2 Heat Treatment shall be classified as follows: Class Description 1 Furnace solution heat treated in accordance with AMS2772 . 2 Extruded and press solution heat treated in accordance with ASTM B807/B807M. If no Cl
17、ass is specified, either Class may be provided. 3.3 Properties Extrusions shall conform to the following requirements, determined in accordance with AMS2355. 3.3.1 As Solution Heat Treated and Naturally Aged 3.3.1.1 Tensile Properties Shall be as shown in Table 2. TABLE 2 - MINIMUM TENSILE PROPERTIE
18、S Property Value Tensile Strength 26.0 ksi (179 MPa) Yield Strength at 0.2% Offset 16.0 ksi (110 MPa) Elongation in 2 inches (50.8 mm) or 4D 16% 3.3.2 Response to Heat Treatment Extrusions, precipitation heat treated in accordance with AMS2772 to the T62 temper (See AS1990), shall have the following
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