SAE AMS 4194E-2018 Aluminum Alloy Sheet and Plate Alclad 4 4Cu - 1 5Mg - 0 60Mn (2024 -T361 Sheet Plate with 1 % Alclad) Solution Heat Treated 6% Cold Worked and Naturally Aged (UN.pdf
《SAE AMS 4194E-2018 Aluminum Alloy Sheet and Plate Alclad 4 4Cu - 1 5Mg - 0 60Mn (2024 -T361 Sheet Plate with 1 % Alclad) Solution Heat Treated 6% Cold Worked and Naturally Aged (UN.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4194E-2018 Aluminum Alloy Sheet and Plate Alclad 4 4Cu - 1 5Mg - 0 60Mn (2024 -T361 Sheet Plate with 1 % Alclad) Solution Heat Treated 6% Cold Worked and Naturally Aged (UN.pdf(6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 ther
2、efrom, 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 2018 SAE International All rights reserved. No part of this
3、publication 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: +1 724-776-49
4、70 (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/AMS4194E AEROSPACE MATERIAL SPECIFICATION AMS4194 REV. E Issued 1970-11 Noncurrent 1989-04 Rea
5、f. Nonc. 2012-03 Reaffirmed 2017-11 Revised 2018-01 Superseding AMS4194D Aluminum Alloy, Sheet and Plate, Alclad 4.4Cu - 1.5Mg - 0.60Mn (2024 -T361 Sheet/Plate with 1% Alclad) Solution Heat Treated, 6% Cold Worked and Naturally Aged (Composition similar to UNS A82024) RATIONALE AMS4194E revises Comp
6、osition (Table 1B), Condition (3.2), Properties (3.3.1.1), Reports (4.4.1) and Identification (5.1.1), and results from a Five-Year Review and update of this specification. 1. SCOPE 1.1 Form This specification covers an aluminum alloy in the form of sheet and plate, alclad both sides, supplied in th
7、e -T361 temper. 1.1.1 AMS4194 covers alclad material for sheet greater than 0.187 inch, and plate up to 0.500 inch (12.70 mm) in nominal thickness (see 8.5). The cladding thickness is minimized to provide a commensurate increase in tensile properties for this alclad reduction. Use of this product is
8、 not recommended without proper evaluation of corrosion resistance. 1.2 Supersession Notice Requirements for thin gage sheet (0.008 to 0.187 inch) in accordance with AMS4194 are hereby superseded by AMS4466. AMS-QQ-A-250/5 and AMS4466 have the same requirements for alclad thickness and tensile prope
9、rties for material less than 0.187 inch in thickness. 1.3 Application These products have been used typically for high strength parts requiring higher yield strength than is afforded by naturally aged tempers of this alloy and maximum corrosion resistance and whose fabrication does not involve weldi
10、ng, but usage is not limited to such applications. 2. APPLICABLE DOCUMENTS The 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 specifi
11、c document issue is specified. When the referenced document has been cancelled and no superseding document has been specified, the last published issue of that document shall apply. SAE INTERNATIONAL AMS4194E Page 2 of 6 2.1 SAE Publications Available from SAE International, 400 Commonwealth Drive,
12、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 Alloys and Magnesium Alloy Wrought Products (Except Forging Stock), and Rolled, Forged, or Flash Welded Rings AMS2772 Heat Trea
13、tment of Aluminum Alloy Raw Materials ARP1917 Clarification of Terms Used in Aerospace Metals Specifications 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 B594 Ultrasonic Inspecti
14、on of Aluminum-Alloy Wrought Products ASTM B660 Packaging/Packing of Aluminum and Magnesium Products ASTM B666/B 666M Identification Marking of Aluminum and Magnesium Products 2.3 ANSI Accredited Publications Copies of these documents are available online at http:/webstore.ansi.org/. ANSI H35.1/H35.
15、1M Standard Alloy and Temper Designation System For Aluminum ANSI H 35.2 Dimensional Tolerances for Aluminum Mill Products ANSI H 35.2M Dimensional Tolerances for Aluminum Mill Products (Metric) 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the percentages by weight as shown in Tables 1
16、, determined in accordance with AMS2355. Table 1 Table 1A - Composition, core (2024) Element Min Max Silicon - 0.50 Iron - 0.50 Copper 3.8 4.9 Manganese 0.30 0.9 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
17、SAE INTERNATIONAL AMS4194E Page 3 of 6 Table 1B - 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 0.05 Other Elements, each - 0.03 Aluminum 99.30 - 3.2 Condition The product shall be supplied in
18、 the following condition: 3.2.1 Sheet Solution heat treated, cold worked approximately 6% and naturally aged to the T361 temper in accordance with AMS2772 (see ANSI H35.1/H35.1M). 3.2.2 Plate Solution heat treated, cold worked approximately 6%, stretched to produce a nominal permanent set of 2%, but
19、 not less than 1-1/2% nor more than 3%, and naturally aged to the T361 temper in accordance with AMS2772 (see ANSI H35.1/H35.1M). 3.2.2.1 Plate shall receive no further straightening operations after stretching. 3.3 Properties The product shall conform to the following requirements, determined in ac
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