SAE AMS 5085J-2017 Steel Sheet Strip and Plate 0 48 - 0 55C (SAE 1050) (UNS G10500).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 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 revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions.Copyright 2017 SAE InternationalAll rights reserved. No part of this publi
3、cation 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: +1 724-776-4970 (out
4、side USA)Fax: 724-776-0790Email: CustomerServicesae.orgSAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedback on thisTechnical Report, please visithttp:/standards.sae.org/AMS5085JAEROSPACEMATERIAL SPECIFICATIONAMS5085 REV. JIssued 1954-05Revised 2017-03Superseding AMS5085HSteel
5、 Sheet, Strip, and Plate0.48 - 0.55C (SAE 1050)(Composition similar to UNS G10500)RATIONALEAMS5085J results from a Five-Year Review and update of this specification that revises grain size testing requirements (3.1.1 and 3.3.3), allows additional heat treatments (3.2), prohibits cutting bar from pla
6、te (3.2.2), and revises decarburization testing (3.3.2) and reporting (4.4).1. SCOPE1.1 FormThis specification covers a carbon steel in the form of sheet, strip, and plate.1.2 ApplicationThese products have been used typically for stamped or formed parts that may subsequently be heat treated, but us
7、age is not limited to such applications.2. APPLICABLE DOCUMENTSThe 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 i
8、ssue 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 PublicationsAvailable from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside
9、USA and Canada) or +1 724-776-4970 (outside USA), www.sae.org.AMS2232 Tolerances Carbon Steel, Sheet, Strip, and PlateAMS2259 Chemical Check Analysis Limits Wrought Low-Alloy and Carbon SteelsAMS2370 Quality Assurance Sampling and Testing Carbon and Low-Alloy Steel Wrought Products and Forging Stock
10、SAE INTERNATIONAL AMS5085J Page 2 of 5AMS2807 Identification Carbon and Low-Alloy Steels, Corrosion and Heat-Resistant Steels and Alloys Sheet, Strip, Plate, and Aircraft TubingARP1917 Clarification of Terms Used in Aerospace Metals Specifications2.2 ASTM PublicationsAvailable from ASTM Internationa
11、l, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org.ASTM A370 Mechanical Testing of Steel ProductsASTM E112 Determining Average Grain SizeASTM E140 Hardness Conversion Tables for Metals Relationship Among Brinell Hardness, Vickers Hardness, Supe
12、rficial Hardness, Knoop Hardness, Scleroscope Hardness, and Leeb Hardness Rockwell HardnessASTM E350 Chemical Analysis of Carbon Steel, Low-Alloy Steel, Silicon Electrical Steel, Ingot Iron, and Wrought IronASTM E384 Microindentation Hardness of Materials3. TECHNICAL REQUIREMENTS3.1 CompositionShall
13、 conform to the percentages by weight shown in Table 1, determined by wet chemical methods in accordance with ASTM E350, by spectrochemical methods, or by other analytical methods acceptable to purchaser.Table 1 - CompositionElement Min MaxCarbon 0.48 0.55Manganese 0.60 0.90Silicon 0.15 0.30Phosphor
14、us - 0.030Sulfur - 0.0353.1.1 Aluminum is an optional grain refining element and need not be determined or reported unless used to satisfy the average grain size requirements of 3.3.3.3.1.2 Check AnalysisComposition variations shall meet the applicable requirements of AMS2259.3.2 ConditionThe produc
15、t shall be supplied in the following condition; hardness shall be not higher than 85 HRB, or equivalent (see 8.2), determined in accordance with ASTM A370:3.2.1 Sheet and StripCold rolled and bright annealed; or hot rolled, annealed, sub-critically annealed or normalized, if necessary, and descaled.
16、3.2.2 PlateHot rolled, annealed, sub-critically annealed or normalized if necessary, and descaled. Bar shall not be cut from plate (also see 4.4.1).SAE INTERNATIONAL AMS5085J Page 3 of 53.2.2.1 If allowed by the purchaser, cold rolled, annealed, sub-critically annealed or normalized if necessary, an
17、d descaled as necessary, having hardness not higher than 85 HRB, or equivalent (see 8.2).3.3 PropertiesThe product shall conform to the following requirements; hardness and bend tests shall be performed in accordance with ASTM A370:3.3.1 BendingThe product shall withstand, without cracking, bending
18、at room temperature through an angle of 180 around a diameter equal to twice the nominal thickness of the product with axis of bend parallel to the direction of rolling.3.3.2 DecarburizationDecarburization shall be evaluated by one of the methods of 3.3.2.1 or 3.3.2.2.3.3.2.1 Metallographic MethodA
19、cross section taken perpendicular to the surface shall be prepared, etched, and visually examined metallographically at a magnification not to exceed 100X. The product shall not show a layer of complete (ferrite) or partial decarburization exceeding the limits of Table 2.3.3.2.2 Hardness Traverse Me
20、thodThe total depth of decarburization shall be determined by a traverse method using microindentation hardness testing in accordance with ASTM E384, at a magnification not exceeding 100X, conducted on a hardened but untempered specimen protected during heat treatment to prevent changes in surface c
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