SAE AMS 6278D-2011 Steel Bars Forgings and Tubing 4 1Cr - 3 4Ni - 4 2Mo - 1 2V (0 11 - 0 15C) Premium Aircraft-Quality for Bearing Applications Double Vacuum Melted (UNS K91231)《经过.pdf
《SAE AMS 6278D-2011 Steel Bars Forgings and Tubing 4 1Cr - 3 4Ni - 4 2Mo - 1 2V (0 11 - 0 15C) Premium Aircraft-Quality for Bearing Applications Double Vacuum Melted (UNS K91231)《经过.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 6278D-2011 Steel Bars Forgings and Tubing 4 1Cr - 3 4Ni - 4 2Mo - 1 2V (0 11 - 0 15C) Premium Aircraft-Quality for Bearing Applications Double Vacuum Melted (UNS K91231)《经过.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 there
2、from, is the sole responsibility of the user.” SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 2011 SAE International All rights reserved. No part of this publication m
3、ay 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 (outside U
4、SA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org SAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/AMS6278DAEROSPACEMATERIALSPECIFICATIONAMS6278 REV. D Issued 1985-10 Revised 2011-06Supersedin
5、g AMS6278C Steel, Bars, Forgings, and Tubing 4.1Cr - 3.4Ni - 4.2Mo - 1.2V (0.11 - 0.15C) Premium Aircraft-Quality for Bearing Applications Double Vacuum Melted (Composition similar to UNS K91231) RATIONALE AMS6278D results from a Five-Year Review and update of this specification. 1. SCOPE 1.1 Form T
6、his specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. 1.2 Application These products have been used typically for critical carburized parts, such as bearings, operating under heavy loads and high speeds at moderate t
7、emperatures, and subject to very rigid inspection standards, but usage is not limited to such applications. 2. APPLICABLE DOCUMENTS The 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 wor
8、k 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 Available from SAE International, 400 Co
9、mmonwealth 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-Alloy Steel Bars AMS2253 Tolerances, Carbon and Alloy Steel Tubing AMS2259 Chemical Check Analysis Limits, Wrought Low-Alloy and Carbon Steels AMS
10、2300 Steel Cleanliness, Premium Aircraft-Quality Magnetic Particle Inspection Procedure Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AMS6278D Page 2 of 8 AMS2370 Quality Assurance Sampling and
11、 Testing, Carbon and Low-Alloy Steel Wrought Products and Forging Stock AMS2372 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 Alloy
12、s AMS2808 Identification, Forgings AS1182 Standard Stock Removal Allowance, Aircraft-Quality and Premium Aircraft-Quality Steel Bars and Mechanical Tubing 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-958
13、5, www.astm.org.ASTM A 370 Mechanical Testing of Steel Products ASTM A 604 Macroetch Testing of Consumable Electrode Remelted Steel Bars and Billets ASTM E 45 Determining the Inclusion Content of Steel ASTM E 112 Determining Average Grain Size ASTM E 350 Chemical Analysis of Carbon Steel, Low-Alloy
14、Steel, Silicon Electrical Steel, Ingot Iron, and Wrought Iron ASTM E 384 Microindentation Hardness of Materials 3. 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 E 350, by spectrochemical
15、methods, or by other analytical methods acceptable to purchaser. TABLE 1 - Composition Element min max Carbon 0.11 0.15 Manganese 0.15 0.35Silicon 0.10 0.25 Phosphorus - 0.015Sulfur - 0.010Chromium 4.00 4.25 Nickel 3.20 3.60Molybdenum 4.00 4.50Vanadium 1.13 1.33 Cobalt - 0.25Tungsten - 0.15Copper -
16、0.10Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AMS6278D Page 3 of 8 3.1.1 Check Analysis Composition variations shall meet the applicable requirements of AMS2259. 3.2 Melting Practice Steel
17、shall be double vacuum melted, using vacuum induction melting followed by vacuum consumable electrode remelting.3.3 Condition The product shall be supplied in the following condition; hardness and tensile strength shall be determined in accordance with ASTM A 370: 3.3.1 Bars Bar shall not be cut fro
18、m plate. 3.3.1.1 Bars 0.500 Inch (12.70 mm) and Under in Nominal Diameter or Least Distance Between Parallel Sides Cold finished, having tensile strength not higher than 125 ksi (862 MPa) or hardness not higher than 27 HRC, or equivalent (See 8.2). 3.3.1.2 Bars Over 0.500 Inch (12.70 mm) in Nominal
19、Diameter or Least Distance Between Parallel Sides Hot finished and annealed, unless otherwise ordered, having hardness not higher than 255 HB, or equivalent (See 8.2). Bars ordered cold finished may have hardness as high as 269 HB, or equivalent (See 8.2). 3.3.2 Forgings As ordered. 3.3.3 Mechanical
20、 Tubing Cold finished, unless otherwise ordered, having hardness not higher than 272 HB, or equivalent (See 8.2). Tubing ordered hot finished and annealed shall have hardness not higher than 248 HB, or equivalent (See 8.2). 3.3.4 Forging Stock As ordered by the forging manufacturer. 3.4 Properties T
21、he product shall conform to the following requirements; hardness testing shall be performed in accordance with ASTM A 370: 3.4.1 Macrostructure Visual examination of transverse full cross-sections from bars, billets, tube rounds or forging stock, etched in hot hydrochloric acid in accordance with AS
22、TM A 604, shall show no pipe or cracks. Porosity, segregation, inclusions, and other imperfections shall be no worse than the macrographs of ASTM A 604 shown in Table 2. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without li
23、cense from IHS-,-,-SAE AMS6278D Page 4 of 8 TABLE 2 - Macrostructure Limits Class Condition Severity 1 Freckles A 2 White Spots A 3 Radial Segregation B 4 Ring Pattern B 3.4.1.1 If tubes are produced directly from ingots or large blooms, transverse sections may be taken from tubes rather than tube r
24、ounds. Macrostructure standards for such tubes shall be as agreed upon by purchaser and vendor. 3.4.2 Micro-Inclusion Rating of Each Heat No specimen shall exceed the limits shown in Table 3, determined in accordance with ASTM E 45, Method D. TABLE 3 - Micro-Inclusion Rating Limits AThin AHeavy BThi
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