SAE AMS 4223E-2015 Aluminum Alloy Castings 4 5Cu - 0 70Ag - 0 30Mn - 0 25Mg - 0 25Ti (A201 0-T4) Solution Heat Treated and Naturally Aged (UNS A12010).pdf
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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 2015 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/AMS4223E AEROSPACE MATERIAL SPECIFICATION AMS4223 REV. E Issued 1974-12 Reaffirme
5、d 2007-04 Revised 2015-08 Superseding AMS4223D Aluminum Alloy, Castings 4.5Cu - 0.70Ag - 0.30Mn - 0.25Mg - 0.25Ti (A201.0-T4) Solution Heat Treated and Naturally Aged (Composition similar to UNS A12010) RATIONALE AMS4223E revises heat treatment requirements (Section 3.5) as a result of Limited Scope
6、 Ballot. 1. SCOPE 1.1 Form This specification covers an aluminum alloy in the form of castings. 1.2 Application These castings have been used typically for components requiring moderate strength combined with good ductility and impact strength, but usage is not limited to such applications. Certain
7、design and processing procedures (see 8.2) may cause these castings to become susceptible to stress-corrosion cracking. 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 supp
8、lier 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 Internati
9、onal, 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. AMS2360 Room Temperature Tensile Properties of Castings AMS2694 In-Process Welding of Castings AMS2771 Heat Treatment of Aluminum Alloy Castings SAE INTER
10、NATIONAL AMS4223E Page 2 of 8 AMS2804 Identification Castings AMS2175 Casting, Classification and Inspection of 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.o
11、rg. ASTM B557 Tension Testing Wrought and Cast Aluminum- and Magnesium-Alloy Products ASTM B557M Tension Testing Wrought and Cast Aluminum- and Magnesium-Alloy Products (Metric) ASTM B660 Packaging/Packing of Aluminum and Magnesium Products ASTM E10 Brinell Hardness of Metallic Materials ASTM E29 Us
12、ing Significant Digits in Test Data to Determine Conformance with Specifications ASTM E34 Chemical Analysis of Aluminum and Aluminum-Base Alloys ASTM E101 Spectrographic Analysis of Aluminum and Aluminum Alloys by the Point-to-Plane Technique ASTM E227 Optical Emission Spectrometric Analysis of Alum
13、inum and Aluminum Alloys by the Point-to-Plane Technique ASTM E607 Atomic Emission Spectrometric Analysis of Aluminum and Aluminum Alloys by the Point-to-Plane Technique, Nitrogen Atmosphere ASTM E716 Sampling of Aluminum and Its Alloys for Spectrochemical Analysis ASTM E1251 Optical Emission Spectr
14、ometric Analysis of Aluminum and Aluminum Alloys by Argon Atmosphere, Point-to-Plane, Unipolar Self-Initiating Capacitor Discharge ASTM E1417/E1417M Liquid Penetrant Testing ASTM E742/E1742M Radiographic Examination ASTM G44 Exposure of Metals and Alloys by Alternate Immersion in Neutral 3.5% Sodium
15、 Chloride Solution 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the percentages by weight shown in Table 1, determined by wet chemical methods in accordance with ASTM E34, by spectrochemical methods in accordance with ASTM E101, ASTM E227, ASTM E607, or ASTM E1251, or by other analytic
16、al methods acceptable to purchaser (see 3.4.1). SAE INTERNATIONAL AMS4223E Page 3 of 8 Table 1 Composition Element min max Silicon Iron Copper Manganese Magnesium Titanium Silver Other Elements, each Other Elements, total Aluminum - - 4.0 0.20 0.15 0.15 0.40 - - remainder 0.05 0.10 5.00 0.40 0.35 0.
17、35 1.0 0.03 0.10 3.1.1 Test results may be rounded in accordance with the “rounding off” method of ASTM E29. 3.2 Condition Solution heat treated and naturally aged to the T4 temper (see AS1990). 3.3 Casting Castings shall be produced from metal conforming to 3.1, determined by analysis of a specimen
18、 (3.4.1) cast after the last melt addition. 3.4 Test Specimens Chemical analysis specimens, and tensile specimens shall be cast as follows: 3.4.1 Chemical Analysis Specimens Shall be cast from each melt after the last melt addition and shall be tested to qualify the melt lot as in 3.1. Spectrochemic
19、al sample shall be prepared in accordance with ASTM E716. 3.4.2 Tensile Specimens Shall be produced as follows: 3.4.2.1 Specimens Cut from Castings Shall be removed after heat treatment and machined to conform to ASTM B557 or ASTM B557M, and shall be either 0.500 inch (12.70 mm) diameter at the redu
20、ced parallel gage section, subsize specimens proportional to the standard, or standard sheet-type specimens, as required by 3.6.1.1. 3.4.2.2 Separately-Cast Specimens Shall conform to ASTM B557 or ASTM B557M and shall be cast from each melt, after the last melt addition. Specimens shall be cast in m
21、olds representing the mold formulation used for castings. Chills are not permitted on test specimen cavity except on the end face of the specimen when approved in accordance with 4.4.2. 3.5 Heat Treatment 3.5.1 Castings and representative tensile specimens shall be solution heat treated and naturall
22、y aged in accordance with AMS2771, except as required by 3.5.2 and 3.5.2.1, to produce the properties specified in 3.6.1 and 3.6.2 (see 8.5 and 8.6). For specific castings, in lieu of the changes introduced by AMS4223E, it is permissible to continue using heat treating process parameters which were
23、previously approved as in 4.4. When separately-cast or integral specimens are permitted, at least one set of tensile specimens shall, during each stage of heat treatment, be put into a batch-type furnace with each load of castings represented or put into a continuous furnace at intervals of not long
24、er than 3 hours. SAE INTERNATIONAL AMS4223E Page 4 of 8 3.5.2 Solution Heat Treatment Unless otherwise specified in 3.5.2.1, soak at 910 F 10 F (488 C 6 C) for 2 hours 0.25 hour, raise temperature to 950 F 10 F (510 C 6 C) and soak for 2 hours 0.25 hour, raise temperature to 985 F 10 F (529 C 6 C) a
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