SAE AMS 4475B-2017 Aluminum Alloy Coiled Sheet Alclad 4 4Cu C 1 5Mg C 0 60Mn (Alclad 2024 -T4 Coiled Sheet) Solution Heat Treated (UNS A82024).pdf
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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 revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions. Copyright 2017 SAE International All rights reserved. No part of this p
3、ublication 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: +1 724-776-497
4、0 (outside USA) 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:/standards.sae.org/AMS4475B AEROSPACE MATERIAL SPECIFICATION AMS4475 REV. B Issued 2013-06 Revised 2017-11 Superse
5、ding AMS4475A Aluminum Alloy, Coiled Sheet, Alclad 4.4Cu 1.5Mg 0.60Mn (Alclad 2024; -T4 Coiled Sheet) Solution Heat Treated (Composition similar to UNS A82024) RATIONALE AMS4475B revises Condition (3.2), Properties (3.3, Tables 2, 3, 5 and 6), Classification of Tests (4.2), Reports (4.4), and Identi
6、fication (5.1.1), and is a Five-Year Review and update of this specification. 1. SCOPE 1.1 Form This specification covers an aluminum alloy in the form of alclad coiled sheet from 0.010 to 0.128 inches, incl (0.25 to 3.25 mm, incl) in thickness supplied in the T4 temper (see 8.5). 1.2 Application Th
7、ese products have been used typically for medium strength parts requiring formability and maximum corrosion resistance and whose fabrication does not involve welding, but usage is not limited to such applications. 2. APPLICABLE DOCUMENTS The issue of the following documents in effect on the date of
8、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 cancelled and no superseding document has been specified, the last p
9、ublished 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 +1 724-776-4970 (outside USA), www.sae.org. AMS2355 Quality Assurance, Sampling and Testing, Aluminum Al
10、loys and Magnesium Alloy, Wrought Products (Except Forging Stock), and Rolled, Forged, or Flash Welded Rings AMS2772 Heat Treatment of Aluminum Alloy Raw Materials AMS-QQ-A-250/5 Aluminum Alloy Alclad 2024, Plate and Sheet ARP1917 Clarification of Terms Used in Aerospace Metals Specifications SAE IN
11、TERNATIONAL AMS4475B Page 2 of 6 2.2 ASTM Publications 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 B660 Packaging/Packing of Aluminum and Magnesium Products ASTM B666/B666M Identification of Aluminum
12、 and Magnesium Alloy Products 2.3 ANSI Accredited Publications Copies of these documents are available online at http:/webstore.ansi.org/. ANSI H35.1/H35.1M Alloy and Temper Designation Systems for Aluminum ANSI H 35.2 Dimensional Tolerances for Aluminum Mill Products ANSI H 35.2M Dimensional Tolera
13、nces for Aluminum Mill Products (Metric) 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the percentages by weight as shown in Table 1 and 2, determined in accordance with AMS2355. Table 1 Composition, core (2024) Element Min Max Silicon - 0.50 Iron - 0.50 Copper 3.8 4.9 Manganese 0.30 0.
14、9 Magnesium 1.2 1.8 Chromium - 0.10 Zinc - 0.25 Titanium - 0.15 Other Elements, each - 0.05 Other Elements, total - 0.15 Aluminum remainder Table 2 Composition, cladding (1230) Element Min Max Iron + Silicon - 0.70 Copper - 0.10 Manganese - 0.05 Magnesium - 0.05 Zinc - 0.10 Titanium Vanadium - 0.03
15、0.05 Other Elements, each - 0.03 Aluminum 99.30 - SAE INTERNATIONAL AMS4475B Page 3 of 6 3.2 Condition The product shall be supplied in the following condition: 3.2.1 Coiled sheet Solution heat treated and naturally aged to the T4 temper in accordance with AMS2772. (see ANSI H35.1/H35.1M) 3.3 Proper
16、ties The product shall conform to the following requirements, determined in accordance with AMS2355 on the mill produced size. 3.3.1 Tensile Properties (T4 Temper) Shall be as shown in Table 3 (see 8.4). Table 3 Table 3A Minimum tensile properties, inch/pound units Temper Nominal Thickness, Inches T
17、ensile Strength, ksi Yield Strength at 0.2% Offset, ksi Elongation in 2 inches or 4D, % -T4 0.010 thru 0.020 0.021 thru 0.062 0.063 thru 0.128 58.0 58.0 61.0 36.0 36.0 38.0 12 15 15 Table 3B Minimum tensile properties, SI units Temper Nominal Thickness, Millimeters Tensile Strength, MPA Yield Streng
18、th at 0.2% Offset, MPA Elongation in 50.8 mm or 4D, % -T4 0.25 thru 0.51 0.53 thru 1.57 1.60 thru 3.25 400 400 421 248 248 262 12 15 15 3.4 Cladding Thickness 3.4.1 Thickness of Cladding Plates The aluminum alloy plates that are bonded to the two sides of the aluminum alloy (2024) ingot or slab, to
19、form a composite that is to be rolled, shall each have a thickness as specified in Table 4. Table 4 Cladding thickness Nominal Thickness, Inch Nominal Thickness, mm Nominal Cladding Thickness Per Side, % Of Thickness Average Cladding Thickness Per Side, % Of Thickness; Minimum 0.010 thru 0.062 0.25
20、thru 1.57 5 4 0.063 and above 1.60 and above 2.5 2 SAE INTERNATIONAL AMS4475B Page 4 of 6 3.5 Response to Temper Conversion (-T62) (see 8.4). When specified, product in the T4 temper after precipitation heat treatment to the T62 temper (see ANSI H35.1/H35.1M) in accordance with AMS2772, shall have t
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