SAE AMS 6560-2013 Steel Bars Wire and Forgings 10 Co - 7 Mo - 6 V - 6 W - 4 Cr (2 2 - 2 4C) Premium Aircraft-Quality for Bearing Applications Inert Gas Atomized and Hot Isostatical.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 reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions.Copyright 2012 SAE InternationalAll rights reserved. No part of this publication may b
3、e 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 USA)Fax
4、: 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/AMS6560AEROSPACEMATERIALSPECIFICATIONAMS6560Issued 2013-02Steel Bars, Wire and Forgings10 Co - 7 Mo - 6 V
5、 - 6 W - 4 Cr (2.2 - 2.4C)Premium Aircraft-Quality for Bearing ApplicationsInert Gas Atomized and Hot Isostatically Pressed Consolidated(Composition similar to UNS T61301)RATIONALEAMS6560 is a new specification to cover UNS T61301 a high speed steel in the form of gas-atomized and HIP-consolidated s
6、olid bar products, forgings and forging stock.1. SCOPE1.1 FormThis specification covers a premium aircraft-quality, high-alloy steel in the form of bars, wire, forgings, and forging stock.1.2 ApplicationThese products have been used typically for critical parts, such as bearings operating under heav
7、y loads and high speeds at moderate temperatures and subject to very rigid inspection standards, 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 PublicationsAvailabl
9、e 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.AMS2248 Chemical Check Analysis Limits Corrosion and Heat-Resistant Steels and Alloys, Maraging and Other Highly-Alloyed Steels, and Iron
10、AlloysAMS2370 Quality Assurance Sampling and Testing, Carbon and Low-Alloy Steel Wrought Products and Forging Stock AMS2372 Quality Assurance Sampling and Testing, Carbon and Low-Alloy Steel Forgings SAE AMS6560 Page 2 of 7AMS2806 Identification, Bars, Wire, Mechanical Tubing, and Extrusions, Carbon
11、 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 International, 100 Barr Harbor Drive, P.
12、O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org.ASTM E 45 Determining the Inclusion Content of Steel ASTM A 370 Mechanical Testing of Steel ProductsASTM E 350 Chemical Analysis of Carbon Steel, Low-Alloy Steel, Silicon Electrical Steel, Ingot Iron, and Wrought IronASTM
13、 E 384 Knoop and Vickers Hardness of Materials2.3 European Committee for StandardizationAvailable from British Standards Institution Group, 389 Chiswick High Road, London, W4 4AL, United Kingdom,Tel: +44 (0)20 8996 9001, Or: Nationial Standards Authority of Ireland, 1 Swift Square, Northwood, Santry
14、, Dublin 9, Ireland, Tel: +353 1 807 3800, www.nsai.ieEN 10228 Steel Cleanliness Non-destructive testing of Steel Forgings Part 3: Ultrasonic Testing of Ferritic or Martensitic Steel3. TECHNICAL REQUIREMENTS3.1 CompositionShall conform to the percentages by weight shown in Table 1, determined by wet
15、 chemical methods in accordance with ASTM E 350, by spectrochemical methods, or by other analytical methods acceptable to purchaser.TABLE 1 - COMPOSITIONElement min maxCarbon 2.25 2.35Manganese 0.1 0.5Silicon 0.4 0.8Phosphorus - 0.03Sulfur - 0.03Chromium 3.75 4.5Molybdenum 6.5 7.5Vanadium 6.25 6.75N
16、ickel - 0.5Cobalt 10.0 11.0Tungsten 6.0 7.0SAE AMS6560 Page 3 of 73.1.1 Check AnalysisComposition variations shall meet the requirements of AMS2248, except that carbon shall be plus or minus 0.04% and vanadium plus or minus 0.10%.3.2 Melting PracticeSteel shall be produced by inert gas atomization o
17、f pre-alloyed melts, with resulting powder consolidated via hot isostatic pressing (HIP). Sintering or the use of binders or fillers to consolidate powder is not permitted. Blending of elemental powders to achieve the required chemical composition is not permitted.3.3 ConditionThe product shall be s
18、upplied in the following condition; hardness shall be determined in accordance with ASTM A 370.3.3.1 Bars3.3.1.1 Annealed material shall have hardness not higher than 360 BHN, or equivalent hardness (See 8.2).3.3.1.2 Hot drawn material shall have hardness not higher than 360 BHN or equivalent hardne
19、ss (See 8.2).3.3.2 Wire Hot finished having tensile strength not higher than 177 ksi (1220 MPa) or equivalent hardness (See 8.3).3.3.3 ForgingsAs ordered.3.3.4 Forging StockAs ordered by the forging manufacturer.3.4 Properties3.4.1 Response to Heat Treatment of Each Lot of Bars, Forgings, Wire and F
20、orging StockSpecimen or samples cut from larger products with section thickness not exceeding 0.375 inch (9.52 mm) shall have hardness not lower than 67 HRC, or equivalent (See 8.2), after being heat treated in accordance with the following heat treatment: Preheat to 1472 F (800 C), hold for one min
21、ute, austenitize at 2102 F (1150 C), quench down to 100 to 120 F (38 to 49 C) or lower in air, temper three times at 1040 F (560 C) at least 1 hour at temperature each time, air cool to room temperature 77 F (25 C) between tempers. 3.4.2 Micro-Inclusion Rating of Each Heat No specimen shall exceed t
22、he limits of Table 2, determined in accordance with ASTM E 45, Method A.TABLE 2 - MICRO-INCLUSION RATINGType A B C DThin 1.5 1.5 1.5 1.5Heavy 1.0 1.0 1.0 1.03.4.3 Decarburization 3.4.3.1 Bars and wire ordered ground, turned, or polished shall be free from decarburization on the ground, turned, or po
23、lished surfaces.SAE AMS6560 Page 4 of 73.4.3.2 Allowable decarburization of bars, wire, and billets ordered for forging or to specified microstructural requirements shall be as agreed upon by purchaser and vendor.3.4.3.3 Decarburization of bars and wire to which 3.4.3.1 or 3.4.3.2 is not applicable
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