SAE AMS 4078J-2011 Aluminum Alloy Sheet and Plate 5 6Zn C 2 5Mg-1 6Cu-0 23Cr 7075 (-T73 Sheet -T7351 Plate) Solution Heat Treated and Overaged (UNS A97075)《经溶液热处理的含有5 6Zn 2 5Mg 1 6.pdf
《SAE AMS 4078J-2011 Aluminum Alloy Sheet and Plate 5 6Zn C 2 5Mg-1 6Cu-0 23Cr 7075 (-T73 Sheet -T7351 Plate) Solution Heat Treated and Overaged (UNS A97075)《经溶液热处理的含有5 6Zn 2 5Mg 1 6.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4078J-2011 Aluminum Alloy Sheet and Plate 5 6Zn C 2 5Mg-1 6Cu-0 23Cr 7075 (-T73 Sheet -T7351 Plate) Solution Heat Treated and Overaged (UNS A97075)《经溶液热处理的含有5 6Zn 2 5Mg 1 6.pdf(5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 2011 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/AMS4078J AEROSPACE MATERIAL SPECIFICATION AMS4078 REV. J Issued 1967-04 Revised 2011-10Supers
5、eding AMS4078H Aluminum Alloy Sheet and Plate 5.6Zn 2.5Mg-1.6Cu-0.23Cr 7075: (-T73 Sheet, -T7351 Plate) Solution Heat Treated and Overaged (Composition similar to UNS A97075) RATIONALE AMS4078J adds tensile strength values for sheet to Table 2 and corrects the metric equivalent for conductivity in 3
6、.3.2.1. 1. SCOPE 1.1 Form This specification covers an aluminum alloy in the form of sheet and plate. 1.2 Application This product has been used typically for parts requiring high strength and resistance to stress-corrosion cracking, but usage is not limited to such applications. 2. APPLICABLE DOCUM
7、ENTS 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 subsequent revision of a document unless a specific document issue is specified. When the referenced document has been c
8、ancelled and no superseding document has been specified, the last published issue of that document shall apply. 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, www.sae.org. AMS2355 Qu
9、ality Assurance, Sampling and Testing, Aluminum Alloys and 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 SAE AMS4078J Page 2 of 5 2.2 ASTM Publications Available
10、 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 for Aerospace Applications ASTM B 660 Packaging/Packing of Aluminum and Magnesium Products ASTM B 666
11、/B 666M Identification Marking of Aluminum Products 2.3 ANSI Publications Available from American National Standards Institute, 25 West 43rd Street, New York, NY 10036, Tel: 212-642-4900, www.ansi.org. ANSI H35.2 Dimensional Tolerances for Aluminum Mill Products ANSI H35.2M Dimensional Tolerances fo
12、r 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 maxSilicon - 0.40Iron - 0.50Copper 1.2 2.0 Manganese - 0.30Magnesium 2.1 2.9 Chromium 0.18
13、 0.28Zinc 5.1 6.1 Titanium - 0.20Other Elements, each - 0.05Other Elements, total - 0.15Aluminum remainder 3.2 Condition 3.2.1 Sheet - Solution heat treated, and precipitation heat treated to T73 temper (See AS1990). Heat treatment shall be performed in accordance with AMS2772. 3.2.2 Plate - Solutio
14、n heat treated, stretched to produce a nominal permanent set of 2%, but not less than 1-1/2% nor more than 3%, and precipitation heat treated to T7351 temper (See AS1990). Heat treatment shall be performed in accordance with AMS2772. 3.2.2.1 Plate shall receive no straightening operations after stre
15、tching. SAE AMS4078J Page 3 of 5 3.3 Properties Sheet and plate shall conform to the following requirements, determined in accordance with AMS2355 on the mill produced size: 3.3.1 Tensile Properties Shall be as specified in Table 2. TABLE 2A - MINIMUM TENSILE PROPERTIES, INCH/POUND UNITS Nominal Thi
16、ckness Inches Tensile Strength ksi Yield Strength at 0.2% Offset ksi Elongation in 2 Inches or 4D % Over 0.039 to 0.249, incl 67.0 56.0 8 Over 0.250 to 1.000, incl 69.0 57.0 7 Over 1.000 to 2.000, incl 69.0 57.0 6 Over 2.000 to 2.500, incl 66.0 52.0 6 Over 2.500 to 3.000, incl 64.0 49.0 6 Over 3.000
17、 to 3.500, incl 63.0 49.0 6 Over 3.500 to 4.000, incl 61.0 48.0 6 TABLE 2B - MINIMUM TENSILE PROPERTIES, SI UNITS Nominal Thickness Millimeters Tensile Strength MPa Yield Strength at 0.2% Offset MPa Elongation in 50.8 mm or 4D % Over 0.991 to 6.32, incl 462 386 8 Over 6.35 to 25.40, incl 476 393 7 O
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