SAE AMS 6413M-2016 Steel Mechanical Tubing 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 2016 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/AMS6413MAEROSPACEMATERIAL SPECIFICATIONAMS6413 REV. MIssued 1942-12Revised 2016-01Superseding
5、 AMS6413LSteel, Mechanical Tubing0.80Cr - 1.8Ni - 0.25Mo (0.35 - 0.40C) (4337)(Composition similar to UNS G43370)RATIONALEAMS6413M is a Five Year Review and update of this specification that revises macrostructure, grain size, decarburizationtesting methods and reporting.1. SCOPE1.1 Form This specif
6、ication covers an aircraft-quality, low-alloy steel in the form of mechanical tubing.1.2 Application This product has been used typically for parts, 0.875 inch (22.22 mm) and under in section thickness at time of heat treatment, requiring a through-hardening steel capable of developing hardness as h
7、igh as 50 HRC, and also 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 a part of this specification to the extent spec
8、ified 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 document shall apply.2.1 SAE Publications Availab
9、le 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.AMS2253 Tolerances, Carbon and Alloy Steel TubingAMS2259 Chemical Check Analysis Limits, Wrought Low-Alloy and Carbon SteelsAMS2301 St
10、eel Cleanliness, Aircraft Quality Magnetic Particle Inspection ProcedureAMS2370 Quality Assurance Sampling and Testing, Carbon and Low-Alloy Steel Wrought Products and Forging StockSAE INTERNATIONAL AMS6413M Page 2 of 6AMS2806 Identification Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and
11、Alloy Steels and Corrosion and Heat-Resistant Steels and AlloysAS1182 Standard Stock Removal Allowance Aircraft-Quality and Premium Aircraft-Quality Steel Bars and Mechanical Tubing2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19
12、428-2959, Tel: 610-832-9585, www.astm.org.ASTM A255 Determining Hardenability of SteelASTM A370 Mechanical Testing of Steel ProductsASTM E112 Determining Average Grain SizeASTM E350 Chemical Analysis of Carbon Steel, Low-Alloy Steel, Silicon Electrical Steel, Ingot Iron, and Wrought IronASTM E381 Ma
13、croetch Testing Steel Bars, Billets, Blooms, and ForgingsASTM E384 Knoop and Vickers Hardness of Materials3. 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 E350, by spectrochemical methods
14、, or by other analytical methods acceptable to purchaser.Table 1 - CompositionElement min maxCarbon 0.35 0.40Manganese 0.65 0.85Silicon 0.15 0.35Phosphorus - 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 grai
15、n refining elements and need not be determined or reported unless used to satisfy the average grain size requirements of 3.3.2.2.3.1.2 Check AnalysisComposition variations shall meet the applicable requirements of AMS2259.3.2 Condition Cold finished, unless otherwise ordered, having hardness not hig
16、her than 25 HRC, or equivalent (see 8.2). Tubing ordered hot finished and annealed shall have hardness not higher than 99 HRB, or equivalent (see 8.2). Hardness shall be determined in accordance with ASTM A370.SAE INTERNATIONAL AMS6413M Page 3 of 63.3 Properties Tubing shall conform to the following
17、 requirements; hardness testing shall be performed in accordance with ASTM A370:3.3.1 MacrostructureVisual examination of transverse full cross-sections from billets or tube rounds, etched in hot hydrochloric acid in accordance with ASTM E381, shall show no pipe or cracks. Porosity, segregation, inc
18、lusions, and other imperfections shall be no worse than the macrographs of ASTM E381 shown in Table 2.Table 2 - Macrostructure limitsSection SizeSquare InchesSection SizeSquare Centimeters MacrographsUp to 36, incl Up to 232, incl S2 - R1 - C2Over 36 to 133, incl Over 232 to 858, incl S2 - R2 - C3Ov
19、er 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 Grain SizeAverage grain size shall be determined by either 3.3.2.1 or 3.3.2.2.3.3
20、.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 following are determined by heat analysis (see 8.5):3.3.2.2.1 A total aluminum content of 0.020 to 0
21、.050%.3.3.2.2.2 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 0.05%.3.3.3 HardenabilityShall be J 10/16 inch (15.9 mm) = 50 HRC minimum and J 18/16 inch (28.6 mm) = 18 HRC minimum, determined on the standard
22、 end-quench test specimen in accordance with ASTM A255 except that the steel shall be normalized at 1,700 F 10 F (927 C 6 C) and the test specimen austenitized at 1,500 F 10 F (816 C 6 C).3.3.4 Decarburization 3.3.4.1 Tubing ordered ground, turned, or polished shall be free from decarburization on t
23、he ground, turned, or polished surfaces. Decarburization on tubing ID shall not exceed the maximum depth specified in Table 3.3.3.4.2 Allowable decarburization of pierced billets, of tube rounds and tubing for redrawing or forging, or of tubing ordered to specified microstructural requirements shall
24、 be as agreed upon by purchaser and producer.3.3.4.3 Decarburization of tubing that 3.3.4.1 or 3.3.4.2 is not applicable shall be not greater than shown in Table 3.SAE INTERNATIONAL AMS6413M Page 4 of 6Table 3A - Maximum total depth of decarburization, inch/pound unitsNominal Wall ThicknessInchesTot
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