SAE AMS 6495A-2011 Steel Bars Forgings and Tubing 1 0Cr - 2 50Ni - 2 0Mo - 1 10Si (0 10 - 0 20C) Premium Aircraft-Quality Electroslag Remelted or Consumable Electrode Vacuum Remelt.pdf
《SAE AMS 6495A-2011 Steel Bars Forgings and Tubing 1 0Cr - 2 50Ni - 2 0Mo - 1 10Si (0 10 - 0 20C) Premium Aircraft-Quality Electroslag Remelted or Consumable Electrode Vacuum Remelt.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 6495A-2011 Steel Bars Forgings and Tubing 1 0Cr - 2 50Ni - 2 0Mo - 1 10Si (0 10 - 0 20C) Premium Aircraft-Quality Electroslag Remelted or Consumable Electrode Vacuum Remelt.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 reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 2011 SAE International All rights reserved. No part of this publication ma
3、y 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 US
4、A) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/AMS6495AAEROSPACEMATERIALSPECIFICATIONAMS6495 REV. A Issued 2009-10Revised 2011-07 Superseding
5、AMS6495 Steel Bars, Forgings, and Tubing 1.0Cr 2.50Ni 2.0Mo 1.10Si (0.10 0.20C) Premium Aircraft-Quality Electroslag Remelted or Consumable Electrode Vacuum Remelted(Composition similar to UNS K51570) RATIONALEAMS6495A results from a correction of the temperature used for the response to heat treatm
6、ent in 3.4.3. 1. SCOPE 1.1 Form This 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 carburized parts requiring high minimum core hardness with a narrow r
7、ange, reduced distortion and subject to stringent magnetic particle inspection standards, but usage is not limited to such applications.1.3 Classification Steel covered by this specification is classified by melting practice as follows: Type 1 Electroslag remelted (ESR) Type 2 Consumable electrode v
8、acuum remelted (VAR) 1.3.1 Unless a specific type is ordered, either type may be supplied. 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 work to a subsequent
9、 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. Copyright SAE International Provided by IHS under license with SAENot for Resa
10、leNo reproduction or networking permitted without license from IHS-,-,-SAE AMS6495A Page 2 of 7 2.1 SAE Publications Available 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 Toler
11、ances, Low-Alloy Steel Bars AMS2253 Tolerances, Carbon and Alloy Steel Tubing AMS2259 Chemical Check Analysis Limits, Wrought Low-Alloy and Carbon Steels AMS2300 Steel Cleanliness, Premium Aircraft-Quality, Magnetic Particle Inspection Procedure AMS2370 Quality Assurance Sampling and Testing, Carbon
12、 and Low-Alloy Steel Wrought Products and Forging Stock AMS2372 Quality Assurance Sampling and Testing, Carbon and Low-Alloy Steel ForgingsAMS2806 Identification, Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and Alloy Steels and Corrosion and Heat-Resistant Steels and Alloys AMS2808 Identif
13、ication, 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: 610-832-9585, www.astm.org.
14、ASTM A 255 Determining Hardenability of Steel ASTM A 370 Mechanical Testing of Steel Products ASTM A 604 Macroetch Testing of Consumable Electrode Remelted Steel Bars and Billets ASTM E 112 Determining Average Grain Size ASTM E 350 Chemical Analysis of Carbon Steel, Low-Alloy Steel, Silicon Electric
15、al Steel, Ingot Iron, and Wrought Iron ASTM E 384 Knoop and Vickers Hardness of Materials 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall 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
16、by other analytical methods acceptable to purchaser. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AMS6495A Page 3 of 7 TABLE 1 - COMPOSITION Element min max Carbon 0.10 0.20 Manganese - 1.00 S
17、ilicon 0.90 1.30 Phosphorus - 0.020 Sulfur - 0.015 Chromium 0.80 1.20 Nickel 2.30 2.70 Molybdenum 1.70 2.20 Vanadium - 0.50 3.1.1 Check Analysis Composition variations shall meet the applicable requirements of AMS2259. 3.2 Melting Practice Steel shall be multiple melted using either electroslag reme
18、lt practice (ESR) or vacuum arc consumable electrode practice (VAR) in the remelt cycle (See 1.3). 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 3.3.1.1 Bars 0.500 inch (12.70 mm) an
19、d Under in Nominal Diameter or 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). 3.3.1.2 Bars over 0.500 inch (12.70 mm) in Nominal Diameter or Least Distance Between Parallel Sides
20、Hot finished and annealed, unless 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). 3.3.2 Forgings As ordered. 3.3.3 Mechanical Tubing Cold finished, unless otherwise ordered, hav
21、ing 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). 3.3.4 Forging StockAs ordered by the forging manufacturer. Copyright SAE International Provided by IHS under license
22、with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AMS6495A Page 4 of 7 3.4 PropertiesThe product shall conform to the following requirements; hardness, tensile, and impact testing shall be performed in accordance with ASTM A 370: 3.4.1 Macrostructure Visu
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