SAE AMS 5833D-2014 Cobalt Alloy Corrosion and Heat-Resistant Round Wire 20Cr - 15Ni - 40Co - 7 0Mo - 16Fe Solution Heat Treated and Cold Drawn (UNS R30003)《溶解热处理和冷拉20Cr - 15Ni - 40.pdf
《SAE AMS 5833D-2014 Cobalt Alloy Corrosion and Heat-Resistant Round Wire 20Cr - 15Ni - 40Co - 7 0Mo - 16Fe Solution Heat Treated and Cold Drawn (UNS R30003)《溶解热处理和冷拉20Cr - 15Ni - 40.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 5833D-2014 Cobalt Alloy Corrosion and Heat-Resistant Round Wire 20Cr - 15Ni - 40Co - 7 0Mo - 16Fe Solution Heat Treated and Cold Drawn (UNS R30003)《溶解热处理和冷拉20Cr - 15Ni - 40.pdf(6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/AMS5833DAEROSPACE MATERIAL SPECIFICATIONAMS5833 REV. DIssued 1984-10Reaffirmed 2008-05Revised
5、 2014-02Superseding AMS5833CCobalt Alloy, Corrosion and Heat-Resistant, Round Wire20Cr - 15Ni - 40Co - 7.0Mo - 16FeSolution Heat Treated and Cold Drawn(Composition similar to UNS R30003)RATIONALEAMS5833D results from a Five Year Review and update that revises Properties (3.5.3) and Reports (4.4).1.
6、SCOPE1.1 FormThis specification covers a corrosion and heat-resistant cobalt alloy in the form of round wire 0.140 inch (3.56 mm) and under in nominal diameter supplied in straight lengths. (See 8.4.)1.2 ApplicationThis wire has been used typically for springs and torsion bars requiring a combinatio
7、n of high strength up to 800 F (427 C) after aging, excellent corrosion resistance, and good fatigue properties, but usage is not limited to such applications. The alloy is nonmagnetic.2. APPLICABLE DOCUMENTSThe issue of the following documents in effect on the date of the purchase order forms a par
8、t of this specification to the extent supplied 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
9、 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.AMS2269 Chemical Check Analysis Limits, Nickel, Nickel Alloys and Cobalt AlloysAMS2371 Quality As
10、surance Sampling and Testing, Corrosion and Heat Resistant Steels and Alloys, Wrought Products and Forging StockAMS2750 PyrometrySAE INTERNATIONAL AMS5833D Page 2 of 6AMS2806 Identification, Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and Alloy Steels and Corrosion and Heat-Resistant Steel
11、s and Alloys2.2 ASTM PublicationsAvailable from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959Tel: 610-832-9585, www.astm.org.ASTM E 8/E 8M Tensile Testing of Metallic MaterialsASTM E 18 Rockwell Hardness of Metallic MaterialsASTM E 354 Chemical Analysis o
12、f High-Temperature, Electrical, Magnetic, and Other Similar Iron, Nickel and Cobalt Alloys3. TECHNICAL REQUIREMENTS3.1 CompositionShall conform to the percentages by weight shown in Table 1, determined by wet chemical methods in accordance with ASTM E 354, by spectrochemical methods, or by other ana
13、lytical methods acceptable to purchaser.TABLE 1 COMPOSITIONElement Min maxCarbon - 0.15Manganese 1.5 2.5Silicon - 1.20Phosphorus - 0.015Sulfur - 0.015Chromium 19.0 21.0Nickel 14.0 16.0Cobalt 39.0 41.0Molybdenum 6.0 8.0Beryllium - 0.10Other Elements, total - 1.00Iron remainder3.1.1 Check AnalysisComp
14、osition variations shall meet the applicable requirements of AMS2269.3.2 Melting PracticeThe alloy shall be produced by multiple melting using vacuum induction followed by vacuum consumable electrode or electroslag remelting practices.3.3 ConditionSolution heat treated and cold drawn.3.4 Solution He
15、at TreatmentWire shall be solution heat treated by heating to 2150 F 25 (1177 C 14), holding at heat for a time commensurate with section thickness, and cooling as required. Pyrometry shall be in accordance with AMS2750.3.5 PropertiesWire shall conform to the following requirements:SAE INTERNATIONAL
16、 AMS5833D Page 3 of 63.5.1 As Solution Heat Treated and Cold Drawn:3.5.1.1 Tensile PropertiesShall be as shown in Table 2, determined in accordance with ASTM E 8/E 8M.TABLE 2A - MINIMUM TENSILE STRENGTH, INCH/POUND UNITSSpecified DiameterInchTensile Strengthksi0.001 to 0.005, incl 260Over 0.005 to 0
17、.040, incl 240Over 0.040 to 0.060, incl 235Over 0.060 to 0.100, incl 225Over 0.100 to 0.140, incl 220TABLE 2B - MINIMUM TENSILE STRENGTH, SI UNITSSpecified DiameterMillimetersTensile StrengthMPa0.03 to 0.13, incl 1793Over 0.13 to 1.02, incl 1655Over 1.02 to 1.52, incl 1620Over 1.52 to 2.54, incl 155
18、1Over 2.54 to 3.56, incl 15173.5.2 After AgingWire shall meet the requirements of 3.5.2.1 and 3.5.2.2 after being aged by heating to a temperature within the range 900 to 1000 F (482 to 538 C), holding at the selected temperature within 25 F (14 C) for 5 to 5-1/2 hours, and cooling to room temperatu
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