SAE AMS 6544D-2005 Maraging Steel Plate 2 0Cr - 10Ni - 8 0Co - 1 0Mo (0 10 - 0 14C) Double Vacuum Melted Solution Heat Treated (UNS K91971).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 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/AMS6544DAEROSPACE MATERIAL SPECIFICATIONAMS6544 REV. DIssued 1975-09Revised 2013-12Supersedin
5、g AMS6544CMaraging Steel, Plate2.0Cr - 10Ni - 8.0Co - 1.0Mo (0.10 - 0.14C)Double Vacuum Melted, Solution Heat Treated(Composition similar to UNS K91971)RATIONALEAMS6544D results from a Five Year Review and update of this specification.1. SCOPE1.1 FormThis specification covers a maraging steel in the
6、 form of rolled or forged plate 0.375 through 8.00 inches (9.5 through 203.2 mm).1.2 ApplicationThis product has been used typically for heat treated parts requiring a combination of high strength, toughness, and weldability, but usage is not limited to such applications.2. APPLICABLE DOCUMENTSThe i
7、ssue 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 revision of a document unless a specific document issue is specified. When the referenced document has been cancelled a
8、nd no superseding document 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.AMS2242 T
9、olerances, Corrosion hardness, tensile, and impact testing shall be performed in accordance with ASTM A 370:3.5.1 As Solution Heat Treated3.5.1.1 HardnessShall be not lower than 42 HRC, or equivalent (See 8.3).3.5.1.2 MacrostructureVisual examination of transverse full cross sections from slabs, bil
10、lets, or suitable rerolled product, etched in hot hydrochloric acid in accordance with ASTM 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. TABLE 2 MACROSTRUCTURE LIMITSClass Condit
11、ion Severity1Freckles B2 White Spots C3 Radial Segregation C4 Ring Pattern D3.5.2 After AgingSpecimens from plate shall meet the requirements of 3.5.2.1, 3.5.2.2, and 3.5.2.3 after being aged by heating to 950 F 10 (510 C 6), holding at heat for not less than 5 hours for sections 2.0 inches (51 mm)
12、and under in nominal thickness and for 10 hours + 0.5, -0, for thicker sections, and cooling at a rate equivalent to air cooling.3.5.2.1 Tensile PropertiesShall be as shown in Table 3.SAE INTERNATIONAL AMS6544D Page 4 of 6TABLE 3A - MINIMUM TENSILE PROPERTIES, INCH/POUND UNITSNominal ThicknessInches
13、TensileStrengthksiYield Strengthat 0.2% OffsetksiElongationin 4D%Reductionof Area%0.375 to 2.000, incl 190 180 14 62Over 2.000 to 4.000, incl 190 175 15 60Over 4.000 to 8.000, incl 190 170 15 50TABLE 3B - MINIMUM TENSILE PROPERTIES, SI UNITSNominal ThicknessMillimetersTensileStrengthMPaYield Strengt
14、hat 0.2% OffsetMPaElongationin 4D%Reductionof Area%9.52 to 50.80, incl 1310 1241 14 62Over 50.80 to 101.60, incl 1310 1207 15 60Over 101.60 to 203.20, incl 1310 1172 15 503.5.2.1.1 Mechanical property requirements for product outside the size range covered by Table 3 shall be agreed between purchase
15、r and producer.3.5.2.2 Impact StrengthShall be as shown in Table 4 when tested in the longitudinal direction. Product meeting the requirements of Table 4 when tested in the transverse direction need not be tested in the longitudinal direction.TABLE 4A - IMPACT STRENGTH, INCH/POUND UNITSNominal Thick
16、nessInchesCharpy V-Notchat 0 FFoot Pounds0.500 to 2.000, incl 65Over 2.000 to 4.000, incl 45Over 4.000 to 8.000, incl 40TABLE 4B - IMPACT STRENGTH, SI UNITSNominal ThicknessMillimetersCharpy V-Notchat -18 CJ12.70 to 50.80, incl 81Over 50.80 to 101.60, incl 61Over 101.60 to 203.20, incl 543.5.2.3 Fra
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