SAE AMS 4100E-2010 Aluminum Alloy Alclad Sheet 5 7Zn - 2 2Mg - 1 6Cu - 0 22Cr (Alclad 7475-T761) Solution and Precipitation Heat Treated (UNS A87475)《溶解和沉积热处理5 7Zn 2 2Mg 1 6Cu 0 22.pdf
《SAE AMS 4100E-2010 Aluminum Alloy Alclad Sheet 5 7Zn - 2 2Mg - 1 6Cu - 0 22Cr (Alclad 7475-T761) Solution and Precipitation Heat Treated (UNS A87475)《溶解和沉积热处理5 7Zn 2 2Mg 1 6Cu 0 22.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4100E-2010 Aluminum Alloy Alclad Sheet 5 7Zn - 2 2Mg - 1 6Cu - 0 22Cr (Alclad 7475-T761) Solution and Precipitation Heat Treated (UNS A87475)《溶解和沉积热处理5 7Zn 2 2Mg 1 6Cu 0 22.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 2010 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/AMS4100EAEROSPACEMATERIALSPECIFICATIONAMS4100 REV. E Issued 1979-07 Revised 2010-04Supersedin
5、g AMS4100D Aluminum Alloy, Alclad, Sheet 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (Alclad 7475-T761) Solution and Precipitation Heat Treated (Composition similar to UNS A87475) RATIONALE AMS4100E corrects an error in the fracture toughness specimen size (3.3.2). 1. SCOPE 1.1 Form This specification covers an
6、aluminum alloy in the form of alclad sheet. 1.2 Application This sheet has been used typically for structural applications requiring material with high strength and resistance to exfoliation-corrosion, moderate fatigue strength, and high fracture toughness, but usage is not limited to such applicati
7、ons. 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 subsequent revision of a document unless a specific document issue is specified. When the refere
8、nced document has been cancelled 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
9、(outside USA), or 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 Rings AMS2772 Heat Treatment of Aluminum Alloy Raw Materials AS1990 Aluminum Alloy Tempers Copyright SAE Int
10、ernational Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AMS4100E Page 2 of 62.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-95
11、85, or www.astm.org.ASTM B 646 Fracture Toughness Testing of Aluminum Alloys ASTM B 660 Packaging/Packing of Aluminum and Magnesium Products ASTM B 666/B 666M Identification Marking of Aluminum and Magnesium Products ASTM E 338 Sharp-Notch Tension Testing of High-Strength Sheet Materials ASTM G 34 E
12、xfoliation Corrosion 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 H35.2 Dimensional Tolerances for Aluminum Mill Produc
13、ts ANSI H35.2M Dimensional 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 1A - COMPOSITION, CORE (7475) Element min max SiliconIronCopper Manganese Magn
14、esium Chromium ZincTitanium Other Elements, each Other Elements, total Aluminum -1.2- 1.90.18 5.2- - - remainder 0.100.121.90.062.60.256.20.060.050.15TABLE 1B - COMPOSITION, CLADDING (7072) Element min max Silicon + Iron Copper Manganese Magnesium ZincOther Elements, Each Other Elements, Total Alumi
15、num - - - - 0.8- - remainder 0.70.100.100.101.30.050.153.2 Condition Solution and precipitation heat treated in accordance with AMS2772 to the T761 temper (See AS1990). Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without lic
16、ense from IHS-,-,-SAE AMS4100E Page 3 of 63.3 Properties Sheet 0.040 inch (1.02 mm) and over in nominal thickness shall conform to the following requirements, determined in accordance with AMS2355 on the mill produced product. Tensile properties, and fracture toughness requirements for sheet under 0
17、.040 inch (1.02 mm) in nominal thickness shall be as agreed upon by purchaser and vendor. 3.3.1 Long Transverse Tensile Properties Shall be as shown in Table 2. TABLE 2A - MINIMUM TENSILE PROPERTIES, INCH/POUND UNITS Nominal Thickness Inch Tensile Strength ksi Yield Strengthat 0.2% Offsetksi Elongat
18、ion in 2 Inches or 4D0.040 to 0.062, incl Over 0.062 to 0.187, incl Over 0.187 to 0.249, incl 66.0 68.0 70.0 55.0 57.0 60.0 999TABLE 2B - MINIMUM TENSILE PROPERTIES, SI UNITS Nominal Thickness MillimetersTensile Strength MPaYield Strengthat 0.2% OffsetMPaElongation in 50.8 mm 1.02 to 1.57, incl Over
19、 1.57 to 4.75, incl Over 4.75 to 6.32, incl 455 469 483 379 393 414 9993.3.2 Fracture Toughness Plane-stress fracture toughness, KC, shall be as shown in Table 3 when tested according to ASTM B 646 using recommended 16-inch (40.6 mm) wide specimens. TABLE 3 - MINIMUM FRACTURE TOUGHNESS PROPERTIES No
20、minal Thickness Inch Nominal Thickness MillimetersSpecimen Orientation KCKC0.040 to 0.125, incl 0.040 to 0.125, incl Over 0.125 to 0.249, incl 1.02 to 3.18, incl 1.02 to 3.18, incl Over 3.18 to 6.32, incl T-L L-T T-L 87.0 100.0 80.0 95.6 110.0 87.9 3.3.3 Alternate Testing for Demonstration of Fractu
21、re Toughness When specified, the producer shall guarantee that sheet meets the fracture toughness requirements based on correlation of notch tensile strength/tensile yield strength (NTS/TYS) ratio, determined in accordance with 3.3.3.1 in lieu of fracture toughness testing (3.3.2). Sampling and test
22、 requirements, and lot acceptance criteria shall be as agreed upon. 3.3.3.1 Notch tensile strength in the long-transverse direction shall be determined in accordance with ASTM E 338 to obtain the NTS/TYS ratio. The values shall be divided by the long-transverse tensile yield strength to obtain the N
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