SAE AMS 4096C-2010 Aluminum Alloy Sheet and Plate Alclad 6 3Cu - 0 30Mn - 0 18Zr - 0 10V - 0 06Ti (Alclad 2219-O) Annealed (UNS A92219)《退火的阿尔克莱德包铝(Alclad)铝合金薄板和板材6 3Cu-0 30Mn-0 18Z.pdf
《SAE AMS 4096C-2010 Aluminum Alloy Sheet and Plate Alclad 6 3Cu - 0 30Mn - 0 18Zr - 0 10V - 0 06Ti (Alclad 2219-O) Annealed (UNS A92219)《退火的阿尔克莱德包铝(Alclad)铝合金薄板和板材6 3Cu-0 30Mn-0 18Z.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4096C-2010 Aluminum Alloy Sheet and Plate Alclad 6 3Cu - 0 30Mn - 0 18Zr - 0 10V - 0 06Ti (Alclad 2219-O) Annealed (UNS A92219)《退火的阿尔克莱德包铝(Alclad)铝合金薄板和板材6 3Cu-0 30Mn-0 18Z.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/AMS4096CAEROSPACEMATERIALSPECIFICATIONAMS4096 REV. C Issued 1969-11 Revised 2010-10Supersedin
5、g AMS4096B Aluminum Alloy Sheet and Plate, Alclad 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (Alclad 2219-O) Annealed(Composition similar to UNS A92219) RATIONALE AMS4096C results from a Five Year Review and update of this specification. 1. SCOPE 1.1 Form This specification covers an aluminum alloy in
6、 the form of sheet and plate clad on two sides. 1.2 Application This specification has been used typically for parts requiring high strength up to 600 F (315 C). These products are also well suited for cryogenic applications and where welding and maximum corrosion resistance are required, but usage
7、is not limited to such applications. 1.2.1 Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking after heat treatment; ARP823 recommends practices to minimize such conditions. 2. APPLICABLE DOCUMENTS The issue of the following documents
8、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 cancelled and no superseding document has b
9、een specified, the last published issue of that document shall apply. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AMS4096C Page 2 of 72.1 SAE Publications Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Te
10、l: 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, Wrought Products (Except Forging Stock), and Rolled, Forged, or Flash Welded Rings AMS2772 Heat Treatment of Aluminum Alloy Raw Mat
11、erials ARP823 Minimizing Stress-Corrosion Cracking in Wrought Heat-Treatable Aluminum Alloy Products AS1990 Aluminum Alloy Tempers 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 B 6
12、60 Packaging/Packing of Aluminum and Magnesium Products ASTM B 666/B 666M Identification Marking of Aluminum and Magnesium 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 H35.2 Dim
13、ensional Tolerance for Aluminum Mill Products ANSI H35.2M Dimensional Tolerances for Aluminum Mill Products, Metric Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AMS4096C Page 3 of 73. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the
14、 following percentages by weight shown in Table 1 and Table 2, determined in accordance with AMS2355: TABLE 1 - COMPOSITION, CORE (2219) Elements min max SiliconIronCopper Manganese Magnesium ZincTitanium Vanadium Zirconium Other Elements, each Other Elements, total Aluminum - - 5.80.20 - - 0.02 0.0
15、5 0.10 - - remainder 0.20 0.30 6.80.40 0.02 0.10 0.10 0.15 0.25 0.05 0.15 TABLE 2 - COMPOSITION, CLADDING (7072) Elements min max Silicon + Iron Copper Manganese Magnesium ZincOther Elements, each Other Elements, total Aluminum - - - - 0.8- - remainder 0.70.10 0.10 0.10 1.30.05 0.15 3.2 Condition An
16、nealed to the -O condition (See AS1990) in accordance with AMS2772. 3.3 Properties The product shall conform to the following requirements, determined in accordance with AMS2355 on the mill product. 3.3.1 As Annealed 3.3.1.1 Tensile Properties Product 0.020 to 2.000 inch (0.50 to 50.00 mm), inclusiv
17、e, in nominal thickness shall meet the requirements of Table 3. TABLE 3 - TENSILE PROPERTIES Tensile Strength, max 32.0 ksi (220 MPa) Yield Strength at 0.2% Offset, max 16.0 ksi (110 MPa) Elongation in 2 in. (50 mm) or 4D, min 12% Provided by IHSNot for ResaleNo reproduction or networking permitted
18、without license from IHS-,-,-SAE AMS4096C Page 4 of 73.3.1.2 Bending Product 0.020 to 0.499 inch (0.50 to 12.50 mm) in nominal thickness shall withstand, without cracking, bending at room temperature through an angle of 180 deg around a diameter equal to the bend factor shown in Table 4 times the no
19、minal thickness of the product with axis of bend parallel to the direction of rolling. TABLE 4 - BEND FACTORS Nominal Thickness Inch Nominal Thickness MillimetersBend Factor 0.020 to 0.249, incl 0.50 to 6.25, incl 4 Over 0.249 to 0.499, incl Over 6.25 to 12.50, incl 6 3.3.2 After Solution and Precip
20、itation 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 specified in Table 5. TABLE 5A - MINIMUM TENSILE PROPERTIES
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