SAE AMS 4134F-2012 Aluminum Alloy Die Forgings 4 4Cu - 0 85Si - 0 80Mn - 0 50Mg (2014-T4) Solution Heat Treated (UNS A92014)《4 4Cu 0 85Si 0 80Mn 0 50Mg 2014-T4型溶液热处理的铝合金冲摸锻件》.pdf
《SAE AMS 4134F-2012 Aluminum Alloy Die Forgings 4 4Cu - 0 85Si - 0 80Mn - 0 50Mg (2014-T4) Solution Heat Treated (UNS A92014)《4 4Cu 0 85Si 0 80Mn 0 50Mg 2014-T4型溶液热处理的铝合金冲摸锻件》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4134F-2012 Aluminum Alloy Die Forgings 4 4Cu - 0 85Si - 0 80Mn - 0 50Mg (2014-T4) Solution Heat Treated (UNS A92014)《4 4Cu 0 85Si 0 80Mn 0 50Mg 2014-T4型溶液热处理的铝合金冲摸锻件》.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 theref
2、rom, 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 2012 SAE International All rights reserved. No part of this publication ma
3、y 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 US
4、A) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/AMS4134FAEROSPACEMATERIALSPECIFICATIONAMS4134 REV. F Issued 1945-10 Revised 2012-01 Superseding
5、 AMS4134E Aluminum Alloy, Die Forgings 4.4Cu - 0.85Si - 0.80Mn - 0.50Mg (2014-T4) Solution Heat Treated (Composition similar to UNS A92014)RATIONALEAMS4134F revises the temper designation for forgings (3.2.1), and is a Five Year Review and update of this specification.1. SCOPE 1.1 Form This specific
6、ation covers an aluminum alloy in the form of die forgings and forging stock. 1.2 Application These forgings have been used typically for parts, requiring strength similar to that of parts machined from AMS4118 bars, but usage is not limited to such applications. Higher strength can be obtained by p
7、recipitation hardening to the T6 temper.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 specific document
8、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 International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (insi
9、de USA and Canada) or 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 Treatment of Aluminum Alloy Raw Materials AMS2808 Identi
10、fication, Forgings AMS4118 Aluminum Alloy, Rolled or Cold Finished Bars, Rods, and Wire, 4.0Cu - 0.70Mn - 0.60Mg - 0.50Si (2017, -T4, -T451), Solution Heat Treated AS1990 Aluminum Alloy Tempers SAE AMS4134F Page 2 of 6 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P
11、.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org.ASTM B 594 Ultrasonic Inspection of Aluminum-Alloy Wrought Products for Aerospace Applications ASTM B 660 Packaging/Packing of Aluminum and Magnesium Products ASTM E 1417 Liquid Penetrant Testing 2.3 ANSI Publications Av
12、ailable 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 Products ANSI H35.2M Dimensional Tolerances for Aluminum Mill Products (Metric) 3. TECHNICAL REQUIREMENTS 3.1 Composit
13、ion Shall conform to the percentages by weight shown in Table 1, determined in accordance with AMS2355 TABLE 1 - COMPOSITION Element min max Silicon 0.50 1.2 Iron - 0.7 Copper 3.9 5.0 Manganese 0.40 1.2 Magnesium 0.20 0.8 Chromium - 0.10Zinc - 0.25Titanium - 0.15Other Elements, each - 0.05Other Elem
14、ents, total - 0.15Aluminum remainder 3.2 Condition Shall be as follows: 3.2.1 Forgings Solution heat treated to the T4 temper (See AS1990) in accordance with AMS2772. 3.2.2 Forging Stock Composition shall be in accordance with Table 1 and shall be free of discontinuities that are unacceptable in the
15、 final forged product (See 3.4). SAE AMS4134F Page 3 of 6 3.3 Properties The product shall conform to the following requirements, determined in accordance with AMS2355 on the mill product. 3.3.1 Forgings 3.3.1.1 Tensile Properties Shall be as follows: 3.3.1.1.1 Test Specimens Specimens, machined fro
16、m separately-forged coupons or from forging stock representing the forgings and, in either case, heat treated with the forgings or machined from prolongations on heat treated forgings, shall have the properties shown in Table 2. TABLE 2 - MINIMUM TENSILE PROPERTIES Property Value Tensile Strength 55
17、.0 ksi (379 MPa) Yield Strength at 0.2% Offset 30.0 ksi (207 MPa) Elongation in 2 inches (50.8 mm) or 4D 16% 3.3.1.1.2 Forgings, With Grain Flow Specimens, machined from forgings 4 inches (102 mm) and under in nominal thickness, with axis of the specimen in area of gage length varying not more than
18、15 degrees from parallel to forging flow lines, shall have properties shown in Table 2 except that elongation may be as low as 11%. 3.3.1.2 Response to Heat Treatment Forgings, after precipitation heat treatment to the T62 temper in accordance with the time and temperature parameters of AMS2772, sha
19、ll meet the following requirements: 3.3.1.2.1 Test Specimens Specimens, machined from separately-forged coupons or from forging stock representing the forgings and, in either case, heat treated with the forgings or machined from prolongations on heat treated forgings, shall have the properties shown
20、 in Table 3. TABLE 3 - MINIMUM TENSILE PROPERTIES Property Value Tensile Strength 65.0 ksi (448 MPa) Yield Strength at 0.2% Offset 55.0 ksi (379 MPa) Elongation in 2 inches (50.8 mm) or 4D 10% 3.3.1.2.2 Forgings, With Grain Flow Specimens machined from forgings with axis of the specimen in area of g
21、age length varying not more than 15 degrees from parallel to the forging flow lines, shall have properties shown in Table 3 except that elongation may be as low as 7%. 3.3.1.2.3 Forgings, Across Grain Flow Specimens, machined from forgings with axis of the specimen in area of gage length varying not
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