SAE AMS 4479-2015 Aluminum Alloy Extruded Profiles (2824-T3511) 4 0Cu - 1 35Mg - 0 7Mn Solution Heat Treated and Stress Relieved by Stretching (UNS A92824).pdf
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1、AEROSPACEMATERIAL SPECIFICATIONAMS4479Issued 2015-01Aluminum Alloy, Extruded Profiles (2824-T3511)4.0Cu - 1.35Mg - 0.7MnSolution Heat Treated and Stress Relieved by Stretching(Composition similar to UNS A92824)RATIONALEAMS4479 is a new specification for aluminum alloy 2824 extruded profiles, solutio
2、n heat treated and stress relieved by stretching.1. SCOPE1.1 FormThis specification covers an aluminum alloy in the form of extruded profiles with a maximum cross-sectional area of 25 in2(160.29 cm2) and nominal thicknesses from 0.250 to 2.500 inch, inclusive (6.3 to 63.50 mm, inclusive).1.2 Applica
3、tionThese extrusions have been used typically for machined parts requiring dimensional stability during machining processes, high strength and damage tolerance, but usage is not limited to such applications.1.2.1 Certain processing procedures may cause this product to become susceptible to stress-co
4、rrosion cracking; ARP823 recommends practices to minimize such conditions.2. APPLICABLE DOCUMENTSThe 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 subsequent revision of a doc
5、ument 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.2.1 SAE PublicationsAvailable from SAE International, 400 Commonwealth Drive, Warrendale, PA 1509
6、6-0001, 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 Flash Welded RingsAMS2772 Heat Treatment of Aluminum Alloy
7、 Raw Materials_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
8、arising therefrom, 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 2014 SAE InternationalAll rights reserved. No part
9、 of this 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
10、-776-4970 (outside USA)Fax: 724-776-0790Email: CustomerServicesae.orgSAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedbackon this Technical Report, please visithttp:/www.sae.org/technical/standards/AMS4479 SAE INTERNATIONAL AMS4479 Page 2 of 5AS1990 Aluminum Alloy TempersARP82
11、3 Minimizing Stress-Corrosion Cracking in Wrought Heat-Treatable Aluminum Alloy Products2.2 ANSI PublicationsAvailable from American National Standards Institute, 25 West 43rd Street, New York, NY 10036-8002, Tel: 212-642-4900, www.ansi.org.ANSI H 35.2 Dimensional Tolerances for Aluminum Mill Produc
12、tsANSI H 35.2M Dimensional Tolerances for Aluminum Mill Products (Metric)2.3 ASTM PublicationsAvailable 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 Aluminum Alloy Wrought Products
13、 for Aerospace Applications ASTM B 660 Packaging of Aluminum and Magnesium ProductsASTM B 666/B 666M Identification Marking of Aluminum and Magnesium Products3. TECHNICAL REQUIREMENTS3.1 CompositionShall conform to the percentages by weight shown in Table 1, determined in accordance with AMS2355.TAB
14、LE 1 - CompositionElement min maxSilicon - 0.08Iron - 0.11Copper 3.7 4.3Manganese 0.50 0.9Magnesium 1.1 1.6Chromium - 0.05Zinc - 0.25Titanium - 0.15Other Elements, each - 0.05Other Elements, total - 0.15Aluminum remainder3.2 ConditionExtruded, solution heat treated and stress relieved by stretching
15、to produce a nominal permanent set of 2%, but not less than 1% nor more than 3%, to the -T3511 temper (See AS1990). 3.2.1 Product shall be supplied with an as-extruded surface finish; light polishing to remove minor surface conditions is permissible provided such conditions can be removed within spe
16、cified dimensional tolerances.3.2.2 Product may receive minor straightening, after stretching, of an amount necessary to meet the requirements of 3.6.SAE INTERNATIONAL AMS4479 Page 3 of 53.3 Heat TreatmentSolution heat treatment shall be in accordance with AMS2772, with the solution heat treating te
17、mpature range between 910 and 930 F.3.4 PropertiesProduct shall conform to the following requirements, determined on the mill produced size in accordance with AMS2355:3.4.1 Longitudinal and long transverse tensile properties, when specified (See 8.5), of extrusions with a maximum cross-sectional are
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