SAE AMS 4280J-2008 Aluminum Alloy Castings Permanent Mold 5 0Si - 1 2Cu - 0 5Mg (355 0-T71) Solution Heat Treated and Overaged (UNS A03550)《5 0Si 1 2Cu 0 5Mg(355 0-T71)溶解热处理和老化的永久铸.pdf
《SAE AMS 4280J-2008 Aluminum Alloy Castings Permanent Mold 5 0Si - 1 2Cu - 0 5Mg (355 0-T71) Solution Heat Treated and Overaged (UNS A03550)《5 0Si 1 2Cu 0 5Mg(355 0-T71)溶解热处理和老化的永久铸.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 4280J-2008 Aluminum Alloy Castings Permanent Mold 5 0Si - 1 2Cu - 0 5Mg (355 0-T71) Solution Heat Treated and Overaged (UNS A03550)《5 0Si 1 2Cu 0 5Mg(355 0-T71)溶解热处理和老化的永久铸.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 2014 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/AMS4280J AEROSPACE MATERIAL SPECIFICATION AMS4280 REV. J Issued 1942-06 Revised 2
5、008-06 Reaffirmed 2014-05 Superseding AMS4280J Aluminum Alloy Castings, Permanent Mold 5.0Si - 1.2Cu - 0.5Mg (355.0-T71) Solution Heat Treated and Overaged (Composition similar to UNS A03550) RATIONALE This document has been reaffirmed to comply with the SAE five-year review policy. 1. SCOPE 1.1 For
6、m This specification covers an aluminum alloy in the form of permanent mold castings. 1.2 Application These castings have been used typically for components requiring moderate strength and dimensional stability up to 300 F (149 C), but usage is not limited to such applications. 2. APPLICABLE DOCUMEN
7、TS 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 issue is specified. When the referenced document has been can
8、celled 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 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org
9、. AMS 2175 Casting, Classification and Inspection of AMS 2360 Room Temperature Tensile Properties of Castings AMS 2694 Repair Welding of Aerospace Castings AMS 2771 Heat Treatment of Aluminum Alloy Castings AMS 2804 Identification, Castings SAE INTERNATIONAL AMS4280J Page 2 of 7 2.2 ASTM Publication
10、s 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 557 Tension Testing Wrought and Cast Aluminum- and Magnesium-Alloy Products ASTM B 557M Tension Testing Wrought and Cast Aluminum- and Magnesium-Alloy
11、Products (Metric) ASTM B 660 Packaging/Packing of Aluminum and Magnesium 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 Alumi
12、num and Aluminum Alloys by the Point-to-Plane Technique ASTM E 607 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 S
13、pectrometric Analysis of Aluminum and Aluminum Alloys by the Argon 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 weig
14、ht shown in Table 1, determined by wet chemical methods in accordance with ASTM E 34, by spectrochemical methods in accordance with ASTM E 1251, ASTM E 227, or ASTM E 607, or ASTM 1251, or by other analytical methods acceptable to purchaser (See 3.4.1). TABLE 1 - COMPOSITION Element (3.1.1) min maxS
15、ilicon 4.5 5.5 Iron (3.1.2) - 0.6 Copper 1.0 1.5 Manganese (3.1.2) - 0.5 Magnesium 0.4 0.6 Chromium - 0.25Zinc - 0.35Titanium - 0.25Other Elements, each - 0.05Other Elements, total - 0.15Aluminum remainder 3.1.1 Test results may be rounded by the “rounding off“ method of ASTM E 29. 3.1.2 If iron con
16、tent exceeds 0.45, manganese content shall be not less than one-half the iron content. 3.2 Condition Solution heat treated and overaged. 3.3 Castings 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 INTERNATI
17、ONAL AMS4280J Page 3 of 7 3.4 Cast 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. Spectrochemical sample shal
18、l be prepared in accordance with ASTM E 716. 3.4.2 Tensile Specimens 3.4.2.1 Unless specimens cut from a casting 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 permane
19、nt molds. Chills are not permitted on test specimen cavity except on the end face of the specimen when approved in accordance with 4.4.2. Tensile specimens shall be processed with each heat treat lot and tested for conformance to 3.6.1. 3.5 Heat Treatment Castings and separately-cast tensile specime
20、ns shall be solution heat treated and overaged to the T71 condition in accordance with AMS 2771. Unless specimens cut from a casting are specified, one or more sets of separately-cast specimens shall, during each stage of heat treatment, be put into a batch-type furnace with each load of castings or
21、 into a continuous furnace at intervals of not longer than three hours. 3.6 Properties Castings and separately-cast tensile specimens 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
22、 requirements of 3.6.1.1 shall be used as the basis for acceptance of castings except when purchaser specifies that 3.6.1.2 applies: 3.6.1.1 Separately-Cast Specimens Specimens as in 4.3.2 shall have the properties shown in Table 2. TABLE 2 - MINIMUM TENSILE PROPERTIES FOR SEPARATELY-CAST SPECIMENS
23、Property Value Tensile Strength 34.0 ksi (234 MPa)Yield Strength at 0.2% Offset 27.0 ksi (186 MPa)Elongation in 4D 1% 3.6.1.2 Specimens Cut from Castings Specimens as in 4.3.4 shall have the properties shown in Table 3. TABLE 3 - MINIMUM TENSILE PROPERTIES FOR SPECIMENS CUT FROM CASTINGS Property Va
24、lue Tensile Strength 25.50 ksi (176 MPa) Yield Strength at 0.2% Offset 20.00 ksi (138 MPa) SAE INTERNATIONAL AMS4280J Page 4 of 7 3.6.1.2.1 When properties other than those of 3.6.1.2 are required, tensile specimens taken from locations indicated on the drawing, from a casting or castings chosen at
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