SAE AMS 4085D-2011 Aluminum Alloy Sheet 5 7Zn - 2 2Mg - 1 6Cu - 0 22Cr (7475-T761) Solution Heat Treated and Overaged (UNS A97475)《经固溶处理和过老化的5 7Zn 2 2Mg 1 6Cu 0 22Cr(7475- T761)铝合金.pdf
《SAE AMS 4085D-2011 Aluminum Alloy Sheet 5 7Zn - 2 2Mg - 1 6Cu - 0 22Cr (7475-T761) Solution Heat Treated and Overaged (UNS A97475)《经固溶处理和过老化的5 7Zn 2 2Mg 1 6Cu 0 22Cr(7475- T761)铝合金.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4085D-2011 Aluminum Alloy Sheet 5 7Zn - 2 2Mg - 1 6Cu - 0 22Cr (7475-T761) Solution Heat Treated and Overaged (UNS A97475)《经固溶处理和过老化的5 7Zn 2 2Mg 1 6Cu 0 22Cr(7475- T761)铝合金.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/AMS4085D AEROSPACE MATERIAL SPECIFICATION AMS4085 REV. D Issued 1976-07 Revised 2011-05 Super
5、seding AMS4085C Aluminum Alloy Sheet 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (7475-T761) Solution Heat Treated and Overaged (Composition similar to UNS A97475)RATIONALE AMS4085D deletes alternate testing for demonstration of fracture toughness (3.3.4, 3.3.4.1), revises acceptance and periodic test requiremen
6、ts (4.2.1, 4.2.2) as well as sampling for fracture toughness testing (4.3.1), and results from a Five Year Review and update of this specification. 1. SCOPE 1.1 Form This specification covers an aluminum alloy in the form of sheet. 1.2 Application This product has been used typically for structural
7、applications requiring sheet with high strength and resistance to exfoliation-corrosion, moderate fatigue strength, and high fracture-toughness, 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 for
8、ms 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 cancelled and no superseding document has been specified, the last published issue of that
9、 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 (outside USA), www.sae.org. AMS2355 Quality Assurance, Sampling and Testing, Aluminum Alloys and Magnesium Alloy
10、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 AMS4085D Page 2 of 5 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshoh
11、ocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM B 646 Fracture Toughness Testing of Aluminum Alloy ASTM B 660 Packing of Aluminum and Magnesium Products ASTM B 666/B 666M Identification Marking of Aluminum and Magnesium Products ASTM E 561 K-R Curve Determination ASTM G 34 Exfoliation Co
12、rrosion Susceptibility in 2XXX and 7XXX Series Aluminum Alloys (EXCO Test) 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 H 35.2 Dimensional Tolerances for Aluminum Mill Products ANSI H 3
13、5.2M Dimensional Tolerances for Aluminum Mill Products (Metric) 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the following percentages by weight, determined in accordance with AMS2355: TABLE 1 - COMPOSITION Element min max Silicon Iron Copper Manganese Magnesium Chromium Zinc Titanium
14、Other Elements, each Other Elements, total Aluminum - - 1.2 - 1.9 0.18 5.2 - - - remainder0.10 0.12 1.9 0.06 2.6 0.25 6.2 0.06 0.05 0.15 3.2 Condition Solution heat treated and precipitation heat treated to the T761 temper (See AS1990) in accordance with AMS2772. 3.3 Properties Sheet 0.040 inch (1.0
15、2 mm) and over in nominal thickness shall conform to the following requirements, determined in accordance with AMS2355, except fracture toughness (3.3.3) shall performed as indicated in the appropriate paragraph. Tests are to be performed on the mill produced size. SAE AMS4085D Page 3 of 5 3.3.1 Ten
16、sile Properties Shall be as shown in Table 2. TABLE 2A - MINIMUM TENSILE PROPERTIES, INCH/POUND UNITS Nominal Thickness Inches Specimen Orientation Tensile Strength ksi Yield Strength at 0.2% Offset ksi Elongation in 2 Inches % 0.040 to 0.249, incl Longitudinal 71.0 61.0 9 Long-Transverse 71.0 60.0
17、9 TABLE 2B - MINIMUM TENSILE PROPERTIES, SI UNITS Nominal Thickness Millimeters Specimen Orientation Tensile Strength MPa Yield Strength at 0.2% Offset MPa Elongation in 50.8 mm % 1.02 to 6.32, incl Longitudinal 490 421 9 Long-Transverse 490 414 9 3.3.2 Exfoliation Corrosion Resistance 3.3.2.1 Resis
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