SAE AMS 4048N-2010 Aluminum Alloy Sheet and Plate Alclad 5 6Zn - 2 5Mg - 1 6Cu - 0 23Cr (Alclad 7075-O) Annealed or when specified “As Fabricated” (Alclad 7075-F) (UNS A97075)《铝衣合金.pdf
《SAE AMS 4048N-2010 Aluminum Alloy Sheet and Plate Alclad 5 6Zn - 2 5Mg - 1 6Cu - 0 23Cr (Alclad 7075-O) Annealed or when specified “As Fabricated” (Alclad 7075-F) (UNS A97075)《铝衣合金.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4048N-2010 Aluminum Alloy Sheet and Plate Alclad 5 6Zn - 2 5Mg - 1 6Cu - 0 23Cr (Alclad 7075-O) Annealed or when specified “As Fabricated” (Alclad 7075-F) (UNS A97075)《铝衣合金.pdf(7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/AMS4048NAEROSPACEMATERIALSPECIFICATIONAMS4048 REV. N Issued 1951-10 Revised 2010-08Supersedin
5、g AMS4048M Aluminum Alloy Sheet and Plate, Alclad 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (Alclad 7075-O) Annealedor when specified, “As Fabricated” (Alclad 7075-F) (Composition similar to UNS A97075) RATIONALE AMS4048N updates the F temper requirement (3.2.2), restricts tensile properties to 1 inch, max (Ta
6、ble 5), and introduces a UT inspection requirement (3.4.1) to facilitate cancellation of AMS-QQ-A-250/13. 1. SCOPE 1.1 Form This specification covers an aluminum alloy in the form of sheet and plate, clad on two sides supplied in the annealed (O) condition. When specified, product shall be supplied
7、in the “as fabricated” (F) temper. 1.2 Application These products have been used typically for formed structural parts which will be subsequently heat treated, but usage is not limited to such applications. 2. APPLICABLE DOCUMENTS The issue of the following documents in effect on the date of the pur
8、chase 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 issue is specified. When the referenced document has been cancelled and no superseding document has been specified, the last published issue o
9、f 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 Quality Assurance, Sampling and Testing, Aluminum Alloys and Magnesium Alloy, Wrought
10、Products (Except Forging Stock), and Rolled, Forged, or Flash Welded Rings AMS2772 Heat Treatment of Aluminum Alloy Raw Materials AS1990 Aluminum Alloy Tempers Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AMS4048N Page 2 of 72.2 ASTM Publicati
11、ons 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 Aluminum-Alloy Products for Aerospace Applications ASTM B 660 Packaging/Packing of Aluminum and Magnesium Products ASTM B
12、 666/B666M Identification of Aluminum and Magnesium Alloy Products 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 35.2M Dime
13、nsional Tolerances for Aluminum Mill Products (Metric) 3. TECHNICAL REQUIREMENTS 3.1 Components Shall conform to the percentages by weight, shown in Table 1 and Table 2, determined in accordance with AMS2355: TABLE 1 - COMPOSITION, CORE (7075) Element min max Silicon - 0.40 Iron - 0.50 Copper 1.2 2.
14、0 Manganese - 0.30Magnesium 2.1 2.9 Chromium 0.18 0.28 Zinc 5.1 6.1 Titanium - 0.20Other Elements, each - 0.05 Other Elements, total - 0.15 Aluminum remainder TABLE 2 - COMPOSITION CLADDING (7072) Element min max Silicon + Iron - 0.7 Copper - 0.10 Manganese - 0.10Magnesium 0.10Zinc 0.8 1.3 Other Ele
15、ments, each - 0.05 Other Elements, total - 0.15 Aluminum remainder Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AMS4048N Page 3 of 73.2 Condition 3.2.1 Annealed in accordance with AMS2772. 3.2.2 When specified, material may be provided in the
16、“as fabricated” (F) temper. Requirements of 3.3.1 do not apply to the F temper. 3.3 Properties The product shall conform to the following requirements, determined in accordance with AMS2355 on the mill produced size. 3.3.1 As Annealed 3.3.1.1 Tensile Properties Shall be as shown in Table 3. TABLE 3A
17、 - TENSILE PROPERTIES, INCH/POUND UNITS Nominal Thickness Inch Tensile Strength ksi, max Yield Strength at 0.2% Offset ksi, maximum Elongation in 2 in. or 4D %, minimum 0.008 to 0.014, incl 36.0 20.0 9 Over 0.014 to 0.062, incl 36.0 20.0 10 Over 0.062 to 0.187, incl 38.0 20.0 10 Over 0.187 to 0.499,
18、 incl 39.0 21.0 10 Over 0.499 to 1.000, incl 40.0 - 10 TABLE 3B - TENSILE PROPERTIES, SI UNITS Nominal Thickness MillimetersTensile Strength MPa, max Yield Strength at 0.2% Offset MPa, maximum Elongation in 50.8 mm or 4D %, minimum 0.20 to 0.36, incl 248 138 9 Over 0.36 to 1.57, incl 248 138 10 Over
19、 1.57 to 4.75, incl 262 138 10 Over 4.75 to 12.67, incl 269 145 10 Over 12.67 to 25.40, incl 276 - 10 3.3.1.2 Bending Product 0.008 to 0.499 inch (0.20 to 12.67 mm) in nominal thickness shall withstand, without cracking, bending at room temperature through an angle of 180 degrees around a diameter e
20、qual to the bend factor (shown in Table 4) times the nominal thickness of the product with axis of bend parallel to the direction of rolling. TABLE 4 - BENDING PARAMETERS Nominal Thickness Inch Nominal Thickness Millimeters Bend Factor 0.008 to 0.032, incl 0.20 to 0.81, incl 1 Over 0.032 to 0.062, i
21、ncl Over 0.81 to 1.57, incl 2 Over 0.062 to 0.125, incl Over 1.57 to 3.18, incl 3 Over 0.125 to 0.249, incl Over 3.18 to 6.32, incl 4 Over 0.249 to 0.499, incl Over 6.32 to 12.67, incl 6 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AMS4048N Pa
22、ge 4 of 73.3.2 Response to Heat Treatment The product, as received by purchaser, shall have the following properties after solution and precipitation heat treatment in accordance with AMS2772 to -T62 temper (See AS1990). 3.3.2.1 Tensile Properties Shall be as shown in Table 5. TABLE 5A - MINIMUM TEN
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