SAE AMS 4212L-2016 Aluminum Alloy Castings 5 0Si - 1 2Cu - 0 50Mg (355 0-T6) Solution and Precipitation Heat Treated (UNS A03550).pdf
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1、_ 6$(7HFKQLFDO6WDQGDUGV%RDUG5XOHVSURYLGHWKDW7KLVUHSRUWLVSX EOLVKHGE6$(WRDGYDQFHWKHVWDWHRIWHFKQLFDODQGHQJL neering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefrom, is thHVROHUHVSR
2、QVLELOLWRIWKHXVHU 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 2016 SAE International All rights reserved. No part of this publication may be reproduced,
3、 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 USA) Fax: 724-776-
4、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/AMS4212L AEROSPACE MATERIAL SPECIFICATION AMS4212 REV. L Issued 1940-10 Revised 2016-11 Superseding AMS4212K Aluminum Alloy
5、Castings 5.0Si - 1.2Cu - 0.50Mg (355.0-T6) Solution and Precipitation Heat Treated (Composition similar to UNS A03550) RATIONALE AMS4212L revises Condition (3.2) 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 c
6、astings. 1.2 Application These castings have been used typically for components requiring high strength at room and elevated temperatures, but usage is not limited to such applications. 2. APPLICABLE DOCUMENTS The issue of the following documents in effect on the date of the purchase order forms a p
7、art 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 last published issue of that docum
8、ent 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 +1 724-776-4970 (outside USA), www.sae.org. AMS2175 Castings, Classification and Inspection of AMS2360 Room Temperature Tensile Prop
9、erties of Castings AMS2694 In-Process Welding of Castings AMS2771 Heat Treatment of Aluminum Alloy Castings SAE INTERNATIONAL AMS4212L Page 2 of 8 AMS2804 Identification Castings ARP1917 Clarification of Terms Used in Aerospace Metals Specifications 2.2 ASTM Publications Available from ASTM Internat
10、ional, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org. 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 Pack
11、aging/Packing of Aluminum and Magnesium Products ASTM E10 Brinell Hardness of Metallic Materials ASTM E18 Rockwell Hardness of Metallic Materials ASTM E29 Using Significant Digits in Test Data to Determine Conformance with Specifications ASTM E34 Chemical Analysis of Aluminum and Aluminum-Base Alloy
12、s ASTM E607 Atomic Emission Spectrometric Analysis of Aluminum and Aluminum Alloys by the Point-to-Plane Technique, Nitrogen Atmosphere ASTM E716 Sampling and Sample Preparation of Aluminum and Aluminum Alloys for Determination of Chemical Composition by Spectrochemical Analysis ASTM E1251 Analysis
13、of Aluminum and Aluminum Alloys by Spark Emission Spectrometry ASTM E1417/E1417M Liquid Penetrant Testing ASTM E1742/E1742M Radiographic Examination 2.3 ANSI Accredited Publications Copies of these documents are available online at http:/webstore.ansi.org/. ANSI H35.1/H35.1M Standard Alloy and Tempe
14、r Designation Systems for Aluminum SAE INTERNATIONAL AMS4212L Page 3 of 8 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 E607, AS
15、TM E1251, or by other analytical methods acceptable to purchaser (see 3.3.1.1). Table 1 - Composition Element Min. Max. Silicon Iron (3.1.1) Copper Manganese (3.1.1) Magnesium Chromium Zinc Titanium Other Elements, each Other Elements, total Aluminum 4.5 - 1.0 - 0.40 - - - - - remainder 5.5 0.6 1.5
16、0.50 0.6 0.25 0.35 0.25 0.05 0.15 3.1.1 If iron content exceeds 0.45%, manganese content shall be not less than one-half of the iron content. 3.1.2 7HVWUHVXOWVPDEHURXQGHGLQDFFRUGDQFHZLWKWKHURXQGLQJRIIPHWKRGRI$670 E29. 3.2 Condition Solution and precipitation heat treated to the T6 temper (see ANSI H
17、35.1/H35.1M). 3.3 Cast Test Specimens 3.3.1 Chemical analysis specimens and tensile specimens shall be cast as follows: 3.3.1.1 Chemical Analysis Specimen 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
18、prepared in accordance with ASTM E716. 3.3.2 Tensile Specimens Shall be produced as follows: 3.3.2.1 Specimens Cut from a Casting and Specimens from Integrally Cast Coupons Shall be removed after heat treatment, shall conform to ASTM B557 or ASTM B557M and shall be either 0.500 inch (12.70 mm) diame
19、ter at the reduced parallel gage section, standard sheet type specimens, or subsize specimens proportional to the standard. 3.3.2.2 Separately Cast Specimens Shall conform to ASTM B557 or ASTM B557M and shall be cast from each melt after the last melt additions. Specimens shall be cast in molds repr
20、esenting 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. Tensile specimens shall be processed with each heat treat lot and tested for conformance to 3.5.1. SAE INTERNATIONAL AMS42
21、12L Page 4 of 8 3.4 Heat Treatment Castings and representative tensile specimens (3.3.2) shall be solution and precipitation heat treated in accordance with AMS2771 except that set temperature and soak time shall be 300 to 320 qF (149 to 160 qC) for 1 to 6 hours. Unless specimens cut from a casting
22、or integrally-cast coupons are specified, separately-cast tensile specimens shall be put into a batch-type furnace with each load of castings or into a continuous furnace at intervals not longer than 3 hours. 3.5 Properties Castings, integrally-cast coupons, and separately cast tensile specimens sha
23、ll conform to the following requirements: 3.5.1 Tensile Properties Shall be as follows, determined in accordance with ASTM B557 or ASTM B557M; conformance to the requirements of 3.5.1.1 shall be used as basis for acceptance of castings except when purchaser specifies that requirements of 3.5.1.2 or
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