SAE AMS 4278B-2003 Aluminum Alloy Alclad Sheet 5 6Zn - 2 5Mg - 1 6Cu - 0 23Cr (Alclad 7075-0) Annealed Fine Grained (UNS A87075)《5 6Zn 2 5Mg 1 6Cu 0 23Cr(Alclad 7075-0)退火细粒铝合金涂覆的薄板.pdf
《SAE AMS 4278B-2003 Aluminum Alloy Alclad Sheet 5 6Zn - 2 5Mg - 1 6Cu - 0 23Cr (Alclad 7075-0) Annealed Fine Grained (UNS A87075)《5 6Zn 2 5Mg 1 6Cu 0 23Cr(Alclad 7075-0)退火细粒铝合金涂覆的薄板.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4278B-2003 Aluminum Alloy Alclad Sheet 5 6Zn - 2 5Mg - 1 6Cu - 0 23Cr (Alclad 7075-0) Annealed Fine Grained (UNS A87075)《5 6Zn 2 5Mg 1 6Cu 0 23Cr(Alclad 7075-0)退火细粒铝合金涂覆的薄板.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 revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions. Copyright 2013 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:/www.sae.org/technical/standards/AMS4278B AEROSPACE MATERIAL SPECIFICATION AMS4278 REV. B Issued 1997-12 Revised 2
5、003-08 Reissued 2003-09 Reaffirmed 2013-12 Superseding AMS4278A Aluminum Alloy, Alclad Sheet 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (Alclad 7075-0) Annealed, Fine Grained (Composition similar to UNS A87075) RATIONALE AMS4278B has been reaffirmed to comply with the SAE five-year review policy. 1. SCOPE:1.1 F
6、orm: This specification covers an aluminum alloy in the form of alclad sheet with a fine-grain core of ASTM No. 6 or finer.1.2 Application: This sheet has been used typically for severely formed structural parts which will be subsequently heat treated and painted or otherwise protected from corrosio
7、n, but usage is not limited to such applications.1.2.1 Certain design and processing procedures may cause this sheet 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 do
8、cuments in effect on the date of the purchase order forms a part of this specification to the extent supplied 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 documen
9、t has been specified, the last published issue of that document shall apply.SAE INTERNATIONAL AMS4278B Page 2 of 7 2.1 SAE Publications: Available from SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001 or www.sae.org.AMS 2355 Quality Assurance Sampling and Testing, Aluminum Alloys and Magnesium
10、 Alloys, Wrought Products, Except Forging Stock, and Rolled, Forged, or Flash Welded RingsAMS 2772 Heat Treatment of Aluminum Alloy Raw MaterialsARP823 Minimizing Stress-Corrosion Cracking in Wrought Heat-Treatable Aluminum Alloy ProductsAS1990 Aluminum Alloy Tempers2.2 ASTM Publications: Available
11、from ASTM, 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959 orwww.astm.org.ASTM B 660 Packaging/Packing of Aluminum and Magnesium ProductsASTM B 666/B 666M Identification Marking of Aluminum and Magnesium ProductsASTM E 112 Determining Average Grain Size2.3 ANSI Publications: Available from A
12、NSI, 25 West 43rd Street, New York, NY 10036 or www.ansi.org.ANSI H35.2 Dimensional Tolerances for Aluminum Mill ProductsANSI H35.2M Dimensional Tolerances for Aluminum Mill Products (Metric)3. TECHNICAL REQUIREMENTS: 3.1 Composition: Shall conform to the percentages by weight shown in Tables 1 and
13、2, determined in accordance with AMS 2355.SAE INTERNATIONAL AMS4278B Page 3 of 7 3.2 Condition: Annealed in accordance with AMS 2772.3.3 Properties: Sheet shall conform to the following requirements, determined in accordance with AMS 2355:3.3.1 As Annealed: 3.3.1.1 Average Grain Size of Core: Shall
14、be ASTM No. 6 or finer, determined in accordance with ASTM E 112 or by a technique agreed upon by purchaser and vendor.TABLE 1 - Composition, Core (7075)Element min maxSilicon - 0.40Iron - 0.50Copper 1.2 2.0Manganese - 0.30Magnesium 2.1 2.9Chromium 0.18 0.28Zinc 5.1 6.1Titanium - 0.20Other Elements,
15、 each - 0.05Other Elements, total - 0.15Aluminum remainderTABLE 2 - Composition, Cladding (7072)Element min maxSilicon + Iron - 0.7Copper - 0.10Manganese - 0.10Magnesium - 0.10Zinc 0.8 1.3Other Elements, each - 0.05Other Elements, total - 0.15Aluminum remainderSAE INTERNATIONAL AMS4278B Page 4 of 7
16、3.3.1.2 Tensile Properties: Shall be as shown in Table 3.3.3.1.3 Bending: Sheet shall withstand, without cracking, bending at room temperature through an angle of 180 degrees around a diameter equal to the bend factor shown in Table 4 times the nominal thickness of the sheet with axis of bend parall
17、el to the direction of rolling.3.3.2 Response to Heat Treatment: Sheet shall have the following properties after being solution and precipitation heat treated to the -T62 temper (See AS1990) in accordance with AMS 2772.3.3.2.1 Tensile Properties: Shall be as specified in Table 5.TABLE 3A - Tensile P
18、roperties, Inch/Pound UnitsNominal ThicknessInchTensileStrengthksi, maxYield Strengthat 0.2% Offsetksi, maximumElongation in2 Inches or 4D%, minimumOver 0.039 to 0.062, incl 36.0 20.0 10Over 0.062 to 0.126, incl 38.0 20.0 10TABLE 3B - Tensile Properties, SI UnitsNominal ThicknessMillimetersTensileSt
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