SAE AMS 4031J-2017 Aluminum Alloy Sheet and Plate 6 3Cu - 0 30Mn - 0 18Zr - 0 10V - 0 06Ti (2219-0) Annealed or when specified As Fabricated (2219-F) (UNS A92219).pdf
《SAE AMS 4031J-2017 Aluminum Alloy Sheet and Plate 6 3Cu - 0 30Mn - 0 18Zr - 0 10V - 0 06Ti (2219-0) Annealed or when specified As Fabricated (2219-F) (UNS A92219).pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4031J-2017 Aluminum Alloy Sheet and Plate 6 3Cu - 0 30Mn - 0 18Zr - 0 10V - 0 06Ti (2219-0) Annealed or when specified As Fabricated (2219-F) (UNS A92219).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 2017 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/AMS4031J AEROSPACE MATERIAL SPECIFICATION AMS4031 REV. J Issued 1962-06 Revised 2017-07 Supers
5、eding AMS4031H Aluminum Alloy, Sheet and Plate 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-O) Annealed or when specified, “As Fabricated” (2219-F) (Composition similar to UNS A92219) RATIONALE AMS4031J revises the Title to correct a temper designation, ANSI Accredited Publications (2.3), Response
6、 to Heat Treatment (3.3.2), Properties (3.3.3), Reports (4.4.1) and Identification (5.1.1), and is 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 0.020 to 2.000 inches (0.51 to 50.80 mm), inclusive, in
7、 nominal thickness, supplied in the annealed (O) condition (see 8.4). When specified, product shall be supplied in the “as fabricated” (F) temper. 1.2 Application These products have been used typically for parts requiring high strength up to 500F (260C) after heat treatment, but usage is not limite
8、d to such applications. May be welded and formed in the specified condition but properties are improved by heat treatment. 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 s
9、upplier 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 that document shall apply. 2.1 SAE Publications Available from SAE Intern
10、ational, 400 Commonwealth Drive, 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 F
11、lash Welded Rings AMS2772 Heat Treatment of Aluminum Alloy Raw Materials ARP1917 Clarification of Terms Used in Aerospace Metals Specifications SAE INTERNATIONAL AMS4031J Page 2 of 6 AS1990 Aluminum Alloy Tempers 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Bo
12、x C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM B594 Ultrasonic Inspection of Aluminum-Alloy Products for Aerospace Applications ASTM B660 Packaging/Packing of Aluminum and Magnesium Products ASTM B666/B666M Identification Marking of Aluminum and Magnesium-Products 2.
13、3 ANSI Accredited Publications Copies of these documents are available online at http:/webstore.ansi.org/ ANSI H35.1/H35.1M Alloy and Temper Designation Systems for Aluminum ANSI 35.2 Dimensional Tolerances for Aluminum Mill Products ANSI 35.2M Dimensional Tolerances for Aluminum Mill Products (Metr
14、ic) 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 Iron Copper Manganese Magnesium Zinc Titanium Vanadium Zirconium Other Elements, each Other Elements, total
15、Aluminum - - 5.8 0.20 - - 0.02 0.05 0.10 - - remainder 0.20 0.30 6.8 0.40 0.02 0.10 0.10 0.15 0.25 0.05 0.15 3.2 Condition 3.2.1 Annealed in accordance with AMS2772. 3.2.2 When specified, material may be provided in the “as fabricated” (F) temper. Requirements of 3.3.1 do not apply to the F temper.
16、SAE INTERNATIONAL AMS4031J Page 3 of 6 3.3 Properties The product shall conform to the following requirements, determined in accordance with AMS2355 on the mill produced size. 3.3.1 As Annealed 3.3.1.1 Tensile Properties Shall be as specified in Table 2 for product 0.020 to 2.000 inches (0.51 to 50.
17、80 mm), inclusive, in nominal thickness. Table 2 - Tensile properties Property Value Tensile Strength, max 32.0 ksi (221 MPa) Yield Strength at 0.2% Offset, max 16.0 ksi (110 MPa) Elongation in 2 Inches (50.8 mm) or 4D, min 12% 3.3.1.2 Bending Product shall withstand, without cracking, bending at ro
18、om temperature through an angle of 180 degrees around a diameter equal to the bend factor shown in Table 3 times the nominal thickness of the product with axis of bend parallel to the direction of rolling. Table 3 - Bending parameters Nominal Thickness Inch Nominal Thickness Millimeters Bend Factor
19、0.020 to 0.250, incl 0.51 to 6.35, incl 4 Over 0.250 to 0.750, incl Over 6.35 to 19.05, incl 6 Over 0.750 to 1.000, incl Over 19.05 to 25.40, incl 8 3.3.2 Response to Heat Treatment (-T62) The product, as received by purchaser, shall have the following properties after solution and precipitation hea
20、t treatment to the -T62 condition (see ANSI H35.1/H35.1M) in accordance with AMS2772: 3.3.2.1 Tensile Properties Shall be as specified in Table 4. Table 4 Table 4A - Minimum tensile properties, inch/pound units Nominal Thickness Inches Tensile Strength ksi Yield Strength at 0.2% Offset ksi Elongatio
- 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:
- SAEAMS4031J2017ALUMINUMALLOYSHEETANDPLATE63CU030MN018ZR010V006TI22190ANNEALEDORWHENSPECIFIEDASFABRICATED2219FUNSA92219PDF

链接地址:http://www.mydoc123.com/p-1021322.html