SAE AMS 6412N-2015 Steel Bars and Forgings 0 80Cr - 1 8Ni - 0 25Mo (0 35 - 0 40C) (4337) (UNS G43370).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 2015 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 feedbackon this Technical Report, please visithttp:/www.sae.org/technical/standards/AMS6412NAEROSPACEMATERIAL SPECIFICATIONAMS6412 REV. NIssued 1940-01Reaffirmed 2006-02Revised
5、2015-12Superseding AMS6412MSteel, Bars and Forgings0.80Cr - 1.8Ni - 0.25Mo (0.35 - 0.40C) (4337)(Composition similar to UNS G43370)RATIONALEAMS6412N results from a Five Year Review and update of this document that revises macrostructure, grain size, decarburization testing methods and reporting.1. S
6、COPE1.1 FormThis specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.1.2 ApplicationThese products have been used typically for parts, 0.875 inch (22.22 mm) and under in nominal section thickness at time of heat treatment, requiring a through-ha
7、rdening steel capable of developing hardness as high as 50 HRC and for parts of greater thickness but requiring proportionately lower hardness, but usage is not limited to such applications.2. APPLICABLE DOCUMENTSThe issue of the following documents in effect on the date of the purchase order forms
8、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 last published issue of that do
9、cument shall apply.2.1 SAE PublicationsAvailable 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.AMS2251 Tolerances, Low-Alloy Steel BarsAMS2259 Chemical Check Analysis Limits, Wrought
10、Low-Alloy and Carbon SteelsAMS2301 Steel Cleanliness, Aircraft Quality, Magnetic Particle Inspection ProcedureSAE INTERNATIONAL AMS6412N Page 2 of 7AMS2370 Quality Assurance Sampling and Testing, Carbon and Low-Alloy Steel, Wrought Products and Forging StockAMS2372 Quality Assurance Sampling and Tes
11、ting, Carbon and Low-Alloy Steel ForgingsAMS2806 Identification Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and Alloy Steels and Corrosion and Heat Resistant Steels and AlloysAMS2808 Identification ForgingsAS1182 Standard Stock Removal Allowance, Aircraft-Quality and Premium Aircraft-Quali
12、ty Steel Bars and Mechanical Tubing2.2 ASTM PublicationsAvailable from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org.ASTM A255 Determining Hardenability of SteelASTM A370 Mechanical Testing of Steel ProductsASTM E112 Deter
13、mining Average Grain SizeASTM E350 Chemical Analysis of Carbon Steel, Low-Alloy Steel, Silicon Electrical Steel, Ingot Iron, and Wrought IronASTM E381 Macroetch Testing Steel Bars, Billets, Blooms, and ForgingsASTM E384 Knoop and Vickers Hardness of Materials3. TECHNICAL REQUIREMENTS3.1 CompositionS
14、hall 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 0.35 0.40Manganese 0.65 0.85Silicon 0.15 0.35Phos
15、phorus - 0.025Sulfur - 0.025Chromium 0.70 0.90Nickel 1.65 2.00Molybdenum 0.20 0.30Copper - 0.353.1.1 Aluminum, vanadium and columbium are optional grain refining elements and need not be determined or reported unless used to satisfy average grain size requirements of 3.3.2. 3.1.2 Check AnalysisCompo
16、sition variations shall meet the applicable requirements of AMS2259.SAE INTERNATIONAL AMS6412N Page 3 of 73.2 ConditionThe product shall be supplied in the following condition; hardness and tensile strength shall be determined in accordance with ASTM A370.3.2.1 BarsBar shall not be cut from plate.3.
17、2.1.1 Bars 0.500 Inch (12.70 mm) and Under in Nominal Diameter or Least Distance Between Parallel SidesCold finished having tensile strength not higher than 130 ksi (896 MPa) or equivalent hardness (see 8.2).3.2.1.2 Bars Over 0.500 Inch (12.70 mm) in Nominal Diameter or Least Distance Between Parall
18、el SidesHot finished and annealed, unless otherwise ordered, having hardness not higher than 229 HB, or equivalent (see 8.3). Bars ordered cold finished may have hardness as high as 248 HB, or equivalent (see 8.3).3.2.2 ForgingsAs ordered.3.2.3 Forging StockAs ordered by the forging manufacturer.3.3
19、 PropertiesThe product shall conform to the following requirements; hardness testing shall be performed in accordance with ASTM A370:3.3.1 MacrostructureVisual examination of transverse full cross-sections from bars, billets, and forging stock, etched in hot hydrochloric acid in accordance with ASTM
20、 E381, shall show no pipe or cracks. Porosity, segregation, inclusions, and other imperfections shall be no worse than the macrographs of ASTM E381 shown in Table 2.Table 2 - Macrostructure limitsCross-Sectional Area Square InchesCross-Sectional AreaSquare Centimeters MacrographsUp to 36, incl Up to
21、 232, incl S2 - R1 - C2Over 36 to 100, incl Over 232 to 645, incl S2 - R2 - C3Over 133 Over 858 Note 1Note 1: Limits for larger sizes shall be agreed upon by purchaser and producer. The purchaser shall have written approval of the agreement from the cognizant engineering organization.3.3.2 Average G
22、rain Size of Bars and ForgingsAverage grain size shall be determined by either 3.3.2.1 or 3.3.2.2.3.3.2.1 Shall be ASTM No. 5 or finer, determined in accordance with ASTM E112 3.3.2.2 The product of a heat shall be considered to have an ASTM No. 5 or finer austenitic grain size if one or more of the
23、 following are determined by heat analysis (see 8.6).3.3.2.2.1 A total aluminum content of 0.020% to 0.050%.SAE INTERNATIONAL AMS6412N Page 4 of 73.3.2.2.2 An acid soluble aluminum content of 0.015% to 0.050%. 3.3.2.2.3 A vanadium content of 0.02 to 0.08%.3.3.2.2.4 A columbium content of 0.02 to 0.0
24、5%.3.3.3 Hardenability of each heatShall be J10/16 inch (15.9 mm) = 50 HRC minimum and J18/16 inch (28.6 mm) = 44 HRC minimum, determined on the standard end-quench test specimen in accordance with ASTM A255 except that the steel shall be normalized at 1700 F 25 F (927 C 14 C) and the test specimen
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