SAE AMS 4600-2011 Aluminum Alloy Sheet and Plate 6 3Cu - 0 30Mn - 0 06Ti - 0 10V - 0 18Zr Solution Heat Treated Cold Worked (8%) and Naturally Aged (2219 -T37) (UNS A92219)《固溶热处理 冷.pdf
《SAE AMS 4600-2011 Aluminum Alloy Sheet and Plate 6 3Cu - 0 30Mn - 0 06Ti - 0 10V - 0 18Zr Solution Heat Treated Cold Worked (8%) and Naturally Aged (2219 -T37) (UNS A92219)《固溶热处理 冷.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4600-2011 Aluminum Alloy Sheet and Plate 6 3Cu - 0 30Mn - 0 06Ti - 0 10V - 0 18Zr Solution Heat Treated Cold Worked (8%) and Naturally Aged (2219 -T37) (UNS A92219)《固溶热处理 冷.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 reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 2011 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/AMS4600AEROSPACEMATERIALSPECIFICATIONAMS4600 Issued 2011-07 Aluminum Alloy, Sheet and Plate 6
5、.3Cu - 0.30Mn - 0.06Ti - 0.10V - 0.18Zr Solution Heat Treated, Cold Worked (8%) and Naturally Aged (2219 -T37) (Composition similar to UNS A92219) RATIONALE AMS4600 is a new specification for 2219-T37 sheet and plate to facilitate cancellation of AMS4295 and AMS-QQ-A-250/30. 1. SCOPE 1.1 Form This s
6、pecification covers an aluminum alloy in the form of sheet and plate. 1.2 Application This product form has been used typically for structural parts requiring high strength up to 500 F (260 C) after proper precipitation heat treatment and which may require forming or welding during fabrication, but
7、usage 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; ARP823 recommends practices to minimize such conditions. 2. APPLICABLE DOCUMENTS The issue of the following documents in effect on th
8、e 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 been specified,
9、the last published issue of that document shall apply. 2.1 SAE Publications Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org.AMS2355 Quality Assurance, Sampling and Testing, Alumi
10、num Alloys and Magnesium Alloy, Wrought Products (Except Forging Stock), and Rolled, Forged, or Flash Welded Rings AMS2770 Heat Treatment of Wrought Aluminum Alloy Parts AMS2772 Heat Treatment of Aluminum Alloy Raw Materials SAE AMS4600 Page 2 of 6 ARP823 Minimizing Stress-Corrosion Cracking in Wrou
11、ght 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 594 Ultrasonic Inspection of Aluminum-Alloy Wrought Product
12、s for Aerospace Applications ASTM B 666/B 666M Identification Marking of Aluminum 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 Dimensional Tolerances for Aluminum Mill Pro
13、ducts ANSI H35.2M Dimensional Tolerances for Aluminum Mill Products (Metric) 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the percentages by weight shown in Table 1, determined in accordance with AMS2355. TABLE 1 - COMPOSITION Element min max Silicon - 0.20 Iron - 0.30 Copper 5.8 6.8 M
14、anganese 0.20 0.40Magnesium - 0.02 Zinc - 0.10 Titanium 0.02 0.10Vanadium 0.05 0.15 Zirconium 0.10 0.25Other Elements, each - 0.05 Other Elements, total - 0.15 Aluminum remainder 3.2 Condition Product shall be supplied in one of the following conditions as specified by purchaser. 3.2.1 Sheet and Pla
15、te Solution heat treated, cold worked to produce a nominal permanent set of 8%, and naturally aged to temper T37 (See AS1990). 3.2.1.1 Plate shall receive no further straightening operations after stretching. SAE AMS4600 Page 3 of 6 3.3 Properties Product shall conform to the following requirements,
16、 determined on the mill produced size in accordance with AMS2355. In addition, test specimens in the T37 condition shall not be required to be tested within four days after completion of the heat treatment. If the manufacturer so elects, samples may be tested after less than four days aging, but if
17、they fail to show the specified properties, the test samples may be discarded and additional specimens may be tested after four days aging. These specimens shall be taken from the same locations in the production lot or sample from which the prior specimens were taken. 3.3.1 As Received 3.3.1.1 Tens
18、ile Properties Shall be as shown in Table 2 (See 8.2). All values are minimum, unless otherwise specified. TABLE 2A - TENSILE PROPERTIES, INCH/POUND UNITS Temper Nominal Thickness Inches Tensile Strength ksi Yield Strength at 0.2% Offset ksi Elongation in 2 inches or 4D %T37 0.020 to 0.039, inclOver
19、 0.039 to 2.500, inclOver 2.500 to 3.000, inclOver 3.000 to 4.000, inclOver 4.000 to 5.000, incl49.0 49.0 47.0 45.0 43.0 38.0 37.0 36.0 35.0 34.0 66654TABLE 2B - TENSILE PROPERTIES, SI UNITS Temper Nominal Thickness MillimetersTensile Strength MPaYield Strength at 0.2% Offset MPaElongation in 50.8 m
- 1.请仔细阅读文档,确保文档完整性,对于不预览、不比对内容而直接下载带来的问题本站不予受理。
- 2.下载的文档,不会出现我们的网址水印。
- 3、该文档所得收入(下载+内容+预览)归上传者、原创作者;如果您是本文档原作者,请点此认领!既往收益都归您。
下载文档到电脑,查找使用更方便
10000 积分 0人已下载
下载 | 加入VIP,交流精品资源 |
- 配套讲稿:
如PPT文件的首页显示word图标,表示该PPT已包含配套word讲稿。双击word图标可打开word文档。
- 特殊限制:
部分文档作品中含有的国旗、国徽等图片,仅作为作品整体效果示例展示,禁止商用。设计者仅对作品中独创性部分享有著作权。
- 关 键 词:
- SAEAMS46002011ALUMINUMALLOYSHEETANDPLATE63CU030MN006TI010V018ZRSOLUTIONHEATTREATEDCOLDWORKED8ANDNATURALLYAGED2219T37UNSA92219

链接地址:http://www.mydoc123.com/p-1021693.html