SAE AMS 4251A-2006 Aluminum Alloy Sheet 2 7Cu - 2 2Li - 0 12Zr (2090-T83) Solution Heat Treated Cold Worked and Precipitation Heat Treated (UNS A92090)《溶液和沉淀热处理的和冷处理的铝合金薄板2 7Cu 2 2.pdf
《SAE AMS 4251A-2006 Aluminum Alloy Sheet 2 7Cu - 2 2Li - 0 12Zr (2090-T83) Solution Heat Treated Cold Worked and Precipitation Heat Treated (UNS A92090)《溶液和沉淀热处理的和冷处理的铝合金薄板2 7Cu 2 2.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4251A-2006 Aluminum Alloy Sheet 2 7Cu - 2 2Li - 0 12Zr (2090-T83) Solution Heat Treated Cold Worked and Precipitation Heat Treated (UNS A92090)《溶液和沉淀热处理的和冷处理的铝合金薄板2 7Cu 2 2.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 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 2011 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/AMS4251A AEROSPACE MATERIAL SPECIFICATION AMS 4251 REV. A Issued 1989-04 Revised
5、2006-03 Reaffirmed 2011-11 Superseding AMS 4251 Aluminum Alloy Sheet 2.7Cu - 2.2Li - 0.12Zr (2090-T83) Solution Heat Treated, Cold Worked, and Precipitation Heat Treated (Composition similar to UNS A92090) RATIONALE This document has been reaffirmed to comply with the SAE five-year review policy. 1.
6、 SCOPE: 1.1 Form: This specification covers an aluminum alloy in the form of sheet. 1.2 Application: Primarily for applications requiring the strength of AMS 4045 and 7.8% lower nominal density. 2. APPLICABLE DOCUMENTS: The issue of the following documents in effect on the date of the purchase order
7、 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 published issue of
8、that document shall apply. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AMS 4251A Page 2 of 6 2.1 SAE Publications: Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada)
9、or 724-776-4970 (outside USA), www.sae.org. AMS 2355 Quality Assurance Sampling and Testing of Aluminum Alloys and Magnesium Alloys, Wrought Products (Except Forging Stock) and Flash Welded Rings AMS 2772 Heat Treatment of Aluminum Alloy Raw Materials AS1990 Aluminum Alloy Tempers 2.2 ASTM Publicati
10、ons: 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 660 Packaging/Packing of Aluminum and Magnesium Products ASTM B 666 Identification and Marking of Aluminum and Magnesium Products ASTM G 34 Exfoliat
11、ion Corrosion Susceptibility in 2XXX and 7XXX Series Aluminum Alloys (EXCO Test) ASTM G 85 Modified Salt Spray (Fog) Testing 2.3 ANSI Publications: Available from American National Standards Institute, 25 West 43rd Street, New York, NY 10036, Tel: 212-642-4900, www.ansi.org. ANSI H35.2 Dimensional T
12、olerances 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 AMS 4251A Page 3 of 6 3. TECHNICAL REQUIREMENTS: 3.1 Composition: Shall conform to the fol
13、lowing percentages by weight shown in Table 1, determined in accordance with AMS 2355. TABLE 1 Composition Element min max Silicon - 0.10 Iron - 0.12 Copper 2.4 3.0 Manganese - 0.05 Magnesium - 0.25 Chromium - 0.05 Zinc - 0.10 Titanium - 0.15 Lithium 1.9 2.6 Zirconium 0.08 0.15 Other Elements, each
14、- 0.05 Other Elements, total - 0.15 Aluminum remainder 3.2 Condition: Solution heat treated, cold worked, and precipitation heat treated to the T83 temper, see AS1990. 3.2.1 Heat treatment shall be in accordance with AMS 2772; times and temperatures shall be established by the producer (see 8.4). Pr
15、ovided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AMS 4251A Page 4 of 6 3.3 Properties: Shall conform to the following requirements, determined in accordance with AMS 2355 on the mill produced size: 3.3.1 Tensile Properties: Shall be as specified in
16、Table 2. TABLE 2A Nominal Thickness Inches Specimen Orientation Tensile Strength ksi, min Yield Strength at 0.2% Offset ksi, minimum Elongation in 2 Inches %, minimum 0.040 to 0.125, incl Longitudinal Long-Transverse 77.0 73.0 70.0 66.0 3 5 Over 0.125 to 0.249, incl Longitudinal Long-Transverse 75.0
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