SAE AMS 6496A-2013 Steel Bars Forgings and Tubing Nitriding 1 4Cr C 1 2Mo C 0 3V (0 29 C 0 36C) Aircraft-Quality for Bearing Applications (UNS K23280)《航空器质量轴承应用件用渗氮法 4Cr - 1 2Mo - .pdf
《SAE AMS 6496A-2013 Steel Bars Forgings and Tubing Nitriding 1 4Cr C 1 2Mo C 0 3V (0 29 C 0 36C) Aircraft-Quality for Bearing Applications (UNS K23280)《航空器质量轴承应用件用渗氮法 4Cr - 1 2Mo - .pdf》由会员分享,可在线阅读,更多相关《SAE AMS 6496A-2013 Steel Bars Forgings and Tubing Nitriding 1 4Cr C 1 2Mo C 0 3V (0 29 C 0 36C) Aircraft-Quality for Bearing Applications (UNS K23280)《航空器质量轴承应用件用渗氮法 4Cr - 1 2Mo - .pdf(8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/AMS6496AAEROSPACE MATERIAL SPECIFICATIONAMS6496 REV. AIssued 2009-09Revised 2013-11Steel Bars
5、, Forgings, and Tubing, Nitriding1.4Cr - 1.2Mo - 0.3V (0.29 - 0.36C)Aircraft-Quality for Bearing Applications(Composition similar to UNS K23280)RATIONALEAMS6496A results from a Five Year Review and update of this specification.1. SCOPE1.1 FormThis specification covers a nitriding grade of aircraft-q
6、uality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. AMS6497 and AMS6498 cover UNS K23280 having other quality levels.1.2 ApplicationThese products have been used typically for nitrided parts such as bearings, operating under heavy loads and high speeds at mod
7、erate temperatures, and subject to rigid inspection standards, and requiring highest surface hardness, high core toughness, and less distortion than parts made from steel requiring quenching to case harden, but usage is not limited to such applications.2. APPLICABLE DOCUMENTSThe issue of the followi
8、ng 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 issue is specified. When the referenced document has been cancelled and no superseding d
9、ocument 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 USA and Canada) or 724-776-4970 (outside USA), www.sae.org.AMS2251 Tolerances, Low-Allo
10、y Steel BarsAMS2253 Tolerances, Carbon and Alloy Steel TubingAMS2259 Chemical Check Analysis Limits, Wrought Low-Alloy and Carbon SteelsAMS2301 Steel Cleanliness, Aircraft-Quality, Magnetic Particle Inspection ProcedureSAE INTERNATIONAL AMS6496A Page 2 of 8AMS2370 Quality Assurance Sampling and Test
11、ing, 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, Mechanical Tubing, and Extrusions, Carbon and Alloy Steels and Corrosion and Heat-Resistant Steels and AlloysAMS2
12、808 Identification, ForgingsAS1182 Standard Stock Removal Allowance, Aircraft-Quality and Premium Aircraft-Quality 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.a
13、stm.org.ASTM A 255 Determining Hardenability of SteelASTM A 370 Mechanical Testing of Steel ProductsASTM E 381 Macroetch Testing Steel Bars, Billets, Blooms and ForgingsASTM E 112 Determining Average Grain SizeASTM E 350 Chemical Analysis of Carbon Steel, Low-Alloy Steel, Silicon Electrical Steel,In
14、got 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 Table 1, determined by wet chemical methods in accordance with ASTM E 350, by spectrochemical methods, or by other analyti
15、cal methods acceptable to purchaser.TABLE 1 COMPOSITIONElement min maxCarbon 0.29 0.36Manganese 0.70 1.20Silicon - 0.30Phosphorus - 0.015Sulfur - 0.005Chromium 1.10 1.60Nickel 0.50 1.00Molybdenum 0.90 1.40Vanadium 0.20 0.40Aluminum 0.10 0.303.1.1 Check AnalysisComposition variations shall meet the a
16、pplicable requirements of AMS2259.3.2 ConditionThe product shall be supplied in the following condition; hardness and tensile strength shall be determined in accordance with ASTM A 370:SAE INTERNATIONAL AMS6496A Page 3 of 83.2.1 Bars3.2.1.1 Bars 0.500 inch (12.70 mm) and Under in Nominal Diameter or
17、 Least Distance Between Parallel SidesCold finished having tensile strength not higher than 138 ksi (950 MPa) or hardness not higher than 285 HB or equivalent (See 8.2).3.2.1.2 Bars over 0.500 inch (12.70 mm) in Nominal Diameter or Least Distance Between Parallel SidesHot finished and annealed, unle
18、ss otherwise ordered, having hardness 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).3.2.1.3 Bars shall not be cut from plate.3.2.2 ForgingsAs ordered.3.2.3 Mechanical TubingCold finished, unless otherwise ordere
19、d, having hardness not higher than 285 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).3.2.4 Forging StockAs ordered by the forging manufacturer.3.3 PropertiesThe product shall conform to the followi
20、ng requirements; hardness, tensile, and impact testing shall be performed in accordance with ASTM A 370:3.3.1 MacrostructureVisual examination of transverse full cross-sections from bars, billets, tube rounds, and forging stock, etched in hot hydrochloric acid in accordance with ASTM E 381, shall sh
21、ow no pipe or cracks. Porosity, segregation, inclusions, and other imperfections shall be no worse than the macrographs of ASTM E 381 shown in Table 2.TABLE 2 - MACROSTRUCTURE LIMITSCross-Section AreaSquare InchesCross-Section AreaSquare Centimeters MacrographsUp to 36, incl Up to 232, incl S2 -R1 -
22、C2Over 36 to 133, incl Over 232 to 858, incl S2 -R2 -C3Over 133 Over 858 Note 1Note 1 Limits for larger sizes shall be agreed upon by purchaser and vendor. The purchaser shall have written approval of the agreement from the cognizant engineering organization.3.3.1.1 If tubes are produced directly fr
23、om ingots or large blooms, transverse sections may be taken from the tubes rather than tube rounds. Macroetch standards for such tubes shall be agreed upon by purchaser and vendor.3.3.2 Average Grain SizeShall be ASTM No. 6 or finer determined in accordance with ASTM E 112.SAE INTERNATIONAL AMS6496A
24、 Page 4 of 83.3.3 Response to Heat Treatment3.3.3.1 Bars, Forgings and Mechanical TubingSpecimens from product shall have the properties shown in Table 4 after being austenitized by heating to 1720 F 25 (938 C 14), holding at heat for a time commensurate with section thickness, heating equipment, an
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