SAE AMS 4214J-2008 Castings Aluminum Alloy Sand 5 0Si - 1 2Cu - 0 50Mg (355 0-T71) Solution Heat Treated and Overaged (UNS A03550)《5 0Si 1 2Cu 0 50Mg溶解热处理和稳定的铝合金沙铸件》.pdf
《SAE AMS 4214J-2008 Castings Aluminum Alloy Sand 5 0Si - 1 2Cu - 0 50Mg (355 0-T71) Solution Heat Treated and Overaged (UNS A03550)《5 0Si 1 2Cu 0 50Mg溶解热处理和稳定的铝合金沙铸件》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4214J-2008 Castings Aluminum Alloy Sand 5 0Si - 1 2Cu - 0 50Mg (355 0-T71) Solution Heat Treated and Overaged (UNS A03550)《5 0Si 1 2Cu 0 50Mg溶解热处理和稳定的铝合金沙铸件》.pdf(7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 2013 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/AMS4214J AEROSPACE MATERIAL SPECIFICATION AMS4214 REV. J Issued 1941-09 Revised 2
5、008-06 Reaffirmed 2013-12 Superseding AMS4214H Castings, Aluminum Alloy Sand 5.0Si - 1.2Cu - 0.50Mg (355.0-T71) Solution Heat Treated and Overaged (Composition similar to UNS A03550) RATIONALE AMS4214J has been reaffirmed to comply with the SAE five-year review policy. 1. SCOPE 1.1 Form This specifi
6、cation covers an aluminum alloy in the form of sand castings. 1.2 Application These castings have been used typically for components requiring strength up to 450 F (232 C), but usage is not limited to such applications. 2. APPLICABLE DOCUMENTS The issue of the following documents in effect on the da
7、te 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, the
8、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. AMS2175 Casting, Classification and Inspection of AMS2360
9、 Room Temperature Tensile Properties of Castings AMS2694 Repair Welding of Aerospace Castings AMS2771 Heat Treatment of Aluminum Alloy Castings AMS2804 Identification, Castings SAE INTERNATIONAL AMS4214J Page 2 of 7 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O.
10、 Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM B 557 Tension Testing Wrought and Cast Aluminum- and Magnesium-Alloy Products ASTM B 557M Tension Testing Wrought and Cast Aluminum- and Magnesium-Alloy Products (Metric) ASTM B 660 Packaging/Packing of Aluminum and M
11、agnesium Products ASTM E 29 Using Significant Digits in Test Data to Determine Conformance with Specifications ASTM E 34 Chemical Analysis of Aluminum and Aluminum-Base Alloys ASTM E 227 Optical Emission Spectrometric Analysis of Aluminum and Aluminum Alloys by the Point-to-Plane Technique ASTM E 60
12、7 Optical Emission Spectrometric Analysis of Aluminum and Aluminum Alloys by the Point-to-Plane Technique, Nitrogen Atmosphere ASTM E 716 Sampling Aluminum and Aluminum Alloys for Spectrochemical Analysis ASTM E 1251 Optical Emission Spectrometric Analysis of Aluminum and Aluminum Alloys by the Argo
13、n Atmosphere, Point-to-Plane, Unipolar Self-Initiating Capacitor Discharge ASTM E 1417 Liquid Penetrant Examination ASTM E 1742 Radiographic Examination 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the percentages by weight shown in Table 1, determined by wet chemical methods in accord
14、ance with ASTM E 34, by spectrochemical methods in accordance with ASTM E 227, ASTM E 607, or ASTM E 1251, or by other analytical methods acceptable to purchaser (See 3.4.1). TABLE 1 - COMPOSITION Element min maxSilicon 4.5 5.5 Iron (3.1.1) - 0.6 Copper 1.0 1.5 Manganese (3.1.1) - 0.50Magnesium 0.40
15、 0.6 Chromium - 0.25Zinc - 0.35Titanium - 0.25Other Elements, each - 0.05Other Elements, total - 0.15Aluminum remainder 3.1.1 If iron content exceeds 0.45%, manganese content shall be not less than one-half the iron content. 3.1.2 Test results may be rounded in accordance with the “rounding off“ met
16、hod of ASTM E 29. 3.2 Condition Solution heat treated and overaged. 3.3 Casting Castings shall be produced from metal conforming to 3.1, determined by analysis of a specimen (3.4.1) cast after the last melt addition. SAE INTERNATIONAL AMS4214J Page 3 of 7 3.4 Cast Test Specimens Chemical analysis sp
17、ecimens 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. Spectrochemical sample shall be prepared in accordance with ASTM E 716. 3.4.2 Tensile Specimens U
18、nless specimens cut from castings are specified by purchaser, separately-cast specimens, conforming to ASTM B 557 or ASTM B 557M, shall be cast from each melt after the last melt addition. Specimens shall be cast in molds representing the mold formulation used for castings. Chills are not permitted
19、on test specimen cavity except on the end face of the specimen when approved in accordance with 4.4.2. A tensile specimen shall be processed with each heat treat lot and tested for conformance to 3.6.1.1. 3.4.2.1 When purchaser specifies specimens cut from castings, such specimens shall be machined
20、to conform to ASTM B 557 or ASTM B 557M, and shall be either 0.500 inch (12.70 mm) diameter at the reduced parallel gage section, subsize specimens proportional to the standard, or standard sheet-type specimens as required by 3.6.1.2. 3.5 Heat Treatment Castings and representative tensile specimens
21、(3.4.2) shall be solution heat treated and overaged in accordance with AMS2771 except that set temperature and soak time shall be 465 to 485 F (240 to 252 C) for 4 to 6 hours. Test specimens shall be put into a batch furnace with each load of castings or into a continuous furnace at intervals of not
22、 longer than three hours. 3.6 Properties Castings and representative tensile specimens produced in accordance with 3.4.2 shall conform to the following requirements: 3.6.1 Tensile Properties Shall be as follows, determined in accordance with ASTM B 557 or ASTM B 557M; conformance to the requirements
23、 of 3.6.1.1 shall be used as basis for acceptance of castings except when purchaser specifies that the requirements of 3.6.1.2 apply: 3.6.1.1 Separately-Cast Specimens Shall have the properties shown in Table 2. TABLE 2 - MINIMUM TENSILE PROPERTIES Property Value Tensile Strength 30.0 ksi (207 MPa)Y
24、ield Strength at 0.2% Offset 22.0 ksi (152 MPa)Elongation in 4D 1.0% SAE INTERNATIONAL AMS4214J Page 4 of 7 3.6.1.2 Specimens Cut from Castings When specified by purchaser, specimens cut from castings (See 4.3.4.1) shall have the properties shown in Table 3. TABLE 3 - MINIMUM TENSILE PROPERTIES Prop
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