SAE AMS 6493A-2013 Steel Bars Forgings and Tubing 1 0Cr - 3 25Ni - 0 40Mo (0 17 - 0 22C) Electroslag Remelted or Consumable Electrode Vacuum Remelted Premium Aircraft-Quality (UNS .pdf
《SAE AMS 6493A-2013 Steel Bars Forgings and Tubing 1 0Cr - 3 25Ni - 0 40Mo (0 17 - 0 22C) Electroslag Remelted or Consumable Electrode Vacuum Remelted Premium Aircraft-Quality (UNS .pdf》由会员分享,可在线阅读,更多相关《SAE AMS 6493A-2013 Steel Bars Forgings and Tubing 1 0Cr - 3 25Ni - 0 40Mo (0 17 - 0 22C) Electroslag Remelted or Consumable Electrode Vacuum Remelted Premium Aircraft-Quality (UNS .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 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 2013 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/AMS6493AAEROSPACE MATERIAL SPECIFICATIONAMS6493 REV. AIssued 2009-09Revised 2013-11Supersedin
5、g AMS6493Steel Bars, Forgings, and Tubing1.0Cr - 3.25Ni - 0.40Mo (0.17 - 0.22C)Electroslag Remelted or Consumable Electrode Vacuum RemeltedPremium Aircraft-Quality(Composition similar to UNS K41910)RATIONALEAMS6493A results from a Five Year Review and update of this specification.1. SCOPE1.1 FormThi
6、s specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.1.2 ApplicationThese products have been used typically for carburized parts requiring high minimum core hardness with a narrow range, reduced distortion and subject
7、to stringent magnetic particle inspection standards, but usage is not limited to such applications.1.3 ClassificationSteel covered by this specification is classified by melting practice as follows:Type 1 Electroslag remelted (ESR)Type 2 Consumable electrode vacuum remelted (VAR)1.3.1 Unless a speci
8、fic type is ordered, either type may be supplied.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 d
9、ocument 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.SAE INTERNATIONAL AMS6493A Page 2 of 72.1 SAE PublicationsAvailable from SAE International, 400 Commonwealth Drive, Warren
10、dale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org.AMS2251 Tolerances, Low-Alloy Steel BarsAMS2253 Tolerances, Carbon and Alloy Steel TubingAMS2259 Chemical Check Analysis Limits, Wrought Low-Alloy and Carbon SteelsAMS2300 Steel Cleanliness, Pre
11、mium Aircraft-Quality, Magnetic Particle Inspection ProcedureAMS2370 Quality Assurance Sampling and Testing, Carbon and Low-Alloy Steel Wrought Products and Forging StockAMS2372 Quality Assurance Sampling and Testing, Carbon and Low-Alloy Steel, Forgings AMS2806 Identification, Bars, Wire, Mechanica
12、l 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-Quality Steel Bars and Mechanical Tubing2.2 ASTM PublicationsAvailable from ASTM Internat
13、ional, 100 Barr Harbor Drive, P. O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org.ASTM A 255 Determining Hardenability of SteelASTM A 370 Mechanical Testing of Steel ProductsASTM A 604 Macroetch Testing of Consumable Electrode Remelted Steel Bars and BilletsASTM E 112 D
14、etermining Average Grain SizeASTM E 350 Chemical Analysis of Carbon Steel, Low-Alloy Steel, Silicon Electrical Steel,Ingot Iron, and Wrought IronASTM E 384 Knoop and Vickers Hardness of Materials3. TECHNICAL REQUIREMENTS3.1 CompositionShall conform to the following percentages by weight shown in Tab
15、le 1, determined by wet chemical methods in accordance with ASTM E 350, by spectrochemical methods, or by other analytical methods acceptable to purchaser.SAE INTERNATIONAL AMS6493A Page 3 of 7TABLE 1 COMPOSITIONElement min maxCarbon 0.17 0.22Manganese 0.30 0.60Silicon - 0.40Phosphorus - 0.020Sulfur
16、 - 0.015Chromium 0.80 1.20Nickel 3.00 3.50Molybdenum 0.30 0.603.1.1 Check AnalysisComposition variations shall meet the applicable requirements of AMS2259.3.2 Melting Practice Steel shall be multiple melted using either electroslag remelt practice (ESR) or vacuum arc consumable electrode practice (V
17、AR) in the remelt cycle (See 1.3).3.3 ConditionThe product shall be supplied in the following condition; hardness and tensile strength shall be determined in accordance with ASTM A 370:3.3.1 Bars3.3.1.1 Bars 0.500 inch (12.70 mm) and Under in Nominal Diameter or Least Distance Between Parallel Sides
18、 Cold finished having tensile strength not higher than 138 ksi (950 MPa) or hardness not higher than 285 HB or equivalent (See 8.2).3.3.1.2 Bars over 0.500 inch (12.70 mm) in Nominal Diameter or Least Distance Between Parallel Sides Hot finished and annealed, unless otherwise ordered, having hardnes
19、s not higher than 285 HB or equivalent (See 8.2). Bars ordered cold finished may have hardness as high as 310 HB or equivalent (See 8.2).3.3.1.3 Bars shall not be cut from plate.3.3.2 ForgingsAs ordered.3.3.3 Mechanical TubingCold finished, unless otherwise ordered, having hardness not higher than 2
20、85 HB, or equivalent (See 8.2). Tubing ordered hot finished and annealed or tempered shall have hardness not higher than 285 HB or equivalent (See 8.2).3.3.4 Forging Stock As ordered by the forging manufacturer.3.4 PropertiesThe product shall conform to the following requirements; hardness, tensile,
21、 and impact testing shall be performed in accordance with ASTM A 370:SAE INTERNATIONAL AMS6493A Page 4 of 73.4.1 MacrostructureVisual examination of transverse full cross-sections from bars, billets, tube rounds, and forging stock, etched in hot hydrochloric acid in accordance with ASTM A 604, shall
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