SAE AMS 4195C-2002 Aluminum Alloy Sheet and Plate Alclad 4 4Cu - 1 5Mg - 0 60Mn (Alclad 2024 and 1-1 2% Alclad 2024-T861 Flat Sheet 1-1 2% Alclad 2024-T861 Plate) Solution Heat Tre.pdf
《SAE AMS 4195C-2002 Aluminum Alloy Sheet and Plate Alclad 4 4Cu - 1 5Mg - 0 60Mn (Alclad 2024 and 1-1 2% Alclad 2024-T861 Flat Sheet 1-1 2% Alclad 2024-T861 Plate) Solution Heat Tre.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4195C-2002 Aluminum Alloy Sheet and Plate Alclad 4 4Cu - 1 5Mg - 0 60Mn (Alclad 2024 and 1-1 2% Alclad 2024-T861 Flat Sheet 1-1 2% Alclad 2024-T861 Plate) Solution Heat Tre.pdf(7页珍藏版)》请在麦多课文档分享上搜索。
1、AEROSPACE MATERIAL SPECIFICATIONAMS 4195CIssuedRevisedSuperseding AMS 4195BAluminum Alloy Sheet and Plate, Alclad4.4Cu - 1.5Mg - 0.60Mn (Alclad 2024 and 1-1/2% Alclad 2024-T861 Flat Sheet;1-1/2% Alclad 2024-T861 Plate)Solution Heat Treated, Cold Worked, and Precipitation Heat Treated1. SCOPE:1.1 For
2、m: This specification covers an aluminum alloy in the form of flat sheet and plate 0.500 inch (12.70 mm) and under in nominal thickness.1.2 Application: These products have been used typically for structural parts requiring a combination of good strength and maximum corrosion resistance. These produ
3、cts, when re-solution heat treated by the user, may not have the tensile properties shown. 1.2.1 Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking; ARP823 recommends practices to minimize such conditions.2. APPLICABLE DOCUMENTS: The
4、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 referenced document has been canceled a
5、nd no superseding document has been specified, the last published issue of that document shall apply.Reaffirmed RATIONALE This document has been reaffirmed to comply with the SAE 5-year Review policy. 1970-112002-012010-05SAE Technical Standards Board Rules provide that: “This report is published by
6、 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 therefrom, is the sole responsibility of the user.” SAE reviews each technical report
7、 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 may be reproduced, stored in a retrieval system or transmitted, in any form or by
8、 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 USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.s
9、ae.org SAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/AMS4195C Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AMS 4195C SAE A
10、MS 4195C- 2 -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 Alloys, Wrought Products, Except Forging Stock, and Rolled, Forged, or Flash Welded RingsMAM 2355 Qua
11、lity Assurance Sampling and Testing, Aluminum Alloys and Magnesium Alloys, Wrought Products, Except Forging Stock, and Rolled, Forged, or Flash Welded Rings, Metric (SI) UnitsAMS 2772 Heat Treatment of Aluminum Alloy Raw MaterialsARP823 Minimizing Stress-Corrosion Cracking in Wrought Heat Treatable
12、Aluminum Alloy Products2.2 ASTM Publications: Available from ASTM, 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959 or www.astm.org.ASTM E 29 Using Significant Digits in Test Data to Determine Conformance with SpecificationsASTM B 660 Packaging/Packing of Aluminum and Magnesium ProductsASTM B
13、 666/B 666M Identification of Aluminum and Magnesium Alloy Products2.3 ANSI Publications: Available from ANSI, 25 West 43rd Street, New York, NY 10036.ANSI H35.1 ANS Alloy and Temper Designation Systems for AluminumANSI H35.2 Dimensional Tolerances for Aluminum Mill ProductsANSI H35.2M Dimensional T
14、olerances for Aluminum Mill Products (Metric)3. TECHNICAL REQUIREMENTS: 3.1 Composition:Shall conform to the percentages by weight shown in Tables 1A and 1B, determined in accordance with AMS 2355 or MAM 2355.Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduc
15、tion or networking permitted without license from IHS-,-,-AMS 4195C SAE AMS 4195C- 3 -3.1.1 Limits for alloying elements and other elements are expressed in ANSI H35.1.3.1.2 Test results may be rounded by the “rounding off” method of ASTM E 29.3.2 Condition:Solution heat treated, cold reduced approx
16、imately 6% in thickness, and precipitation heat treated.Heat treatments shall be performed in accordance with AMS 2772.3.3 Properties:The product shall conform to the following requirements, determined in accordance with AMS 2355 or MAM 2355 on the mill product.TABLE 1A - Composition - Core (2024)El
17、ement (3.1.1) min maxSiliconIronCopperManganeseMagnesiumChromiumZincTitaniumOther Elements, eachOther Elements, totalAluminum-3.80.301.2-remainder0.500.504.90.91.80.100.250.150.050.15TABLE 1B - Composition - Cladding (1230)Element (3.1.1) min maxSilicon + IronCopperManganeseMagnesiumZincTitaniumVana
18、diumOther Elements, eachAluminum, by difference-99.300.700.100.050.050.100.030.050.03-Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AMS 4195C SAE AMS 4195C- 4 -3.3.1 Tensile Properties: Shall be as
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