SAE AMS 6543E-2011 Steel Bars and Forgings 2 0Cr - 10Ni - 8 0Co - 1 0Mo (0 10 - 0 14C) (HY-180) Double Vacuum Melted Solution Heat Treated Marage Hardenable (UNS K91970)《经过双重真空熔化 热.pdf
《SAE AMS 6543E-2011 Steel Bars and Forgings 2 0Cr - 10Ni - 8 0Co - 1 0Mo (0 10 - 0 14C) (HY-180) Double Vacuum Melted Solution Heat Treated Marage Hardenable (UNS K91970)《经过双重真空熔化 热.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 6543E-2011 Steel Bars and Forgings 2 0Cr - 10Ni - 8 0Co - 1 0Mo (0 10 - 0 14C) (HY-180) Double Vacuum Melted Solution Heat Treated Marage Hardenable (UNS K91970)《经过双重真空熔化 热.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/AMS6543EAEROSPACEMATERIALSPECIFICATIONAMS6543 REV. E Issued 1975-09 Revised 2011-06Supersedin
5、g AMS6543D Steel, Bars and Forgings 2.0Cr - 10Ni - 8.0Co - 1.0Mo (0.10 - 0.14C) (HY-180) Double Vacuum Melted Solution Heat Treated, Marage Hardenable (Composition similar to UNS K91970)RATIONALE AMS6543E results from a Five Year Review and update of this specification. 1. SCOPE 1.1 Form This specif
6、ication covers a premium aircraft-quality maraging steel in the form of bars 0.50 inch (12.7 mm) and over in nominal diameter or least distance between parallel sides, forgings, and forging stock. 1.2 Application These products have been used typically for heat treated parts requiring a combination
7、of high strength, toughness, and weldability, 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 work to a subseque
8、nt 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 Commonwealth Driv
9、e, 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 Alloys AMS2251 Tolerances, Low-Alloy Steel Bar
10、s AMS2370 Quality Assurance Sampling and Testing, Carbon and Low-Alloy Steel Wrought Products and Forging Stock Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AMS6543E Page 2 of 8 AMS2372 Qualit
11、y Assurance Sampling and Testing, Carbon and Low-Alloy Steel Forgings AMS2630 Inspection, Ultrasonic, Product Over 0.5 Inch (12.7 mm) Thick AMS2750 Pyrometry AMS2806 Identification, Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and Alloy Steels and Corrosion and Heat-Resistant Steels and All
12、oys 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: 610-832-9
13、585, 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 353 Chemical Analysis of Stainless, Heat-Resisting, Maraging, and Other Similar Chromium-Nickel-Iron Alloys 3. TECHNICAL REQUIREMENTS 3.1 Comp
14、osition Shall conform to the percentages by weight shown in Table 1, determined by wet chemical methods in accordance with ASTM E 353, by spectrochemical methods, or by other analytical methods acceptable to purchaser. TABLE 1 - COMPOSITION Element min max Carbon 0.10 0.14 Manganese 0.05 0.25Silicon
15、 - 0.10 Phosphorus - 0.010 Sulfur - 0.006 Chromium 1.80 2.20 Nickel 9.50 10.50Cobalt 7.50 8.50 Molybdenum 0.90 1.10Titanium - 0.015 Aluminum - 0.025Oxygen - 0.0025 (25 ppm)Nitrogen - 0.0075 (75 ppm)Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or net
16、working permitted without license from IHS-,-,-SAE AMS6543E Page 3 of 8 3.1.1 Check Analysis Composition variations shall meet the applicable requirements of AMS2248. No variation is permitted for oxygen and nitrogen. 3.2 Melting Practice Shall be multiple melted using vacuum induction melting follo
17、wed by vacuum consumable electrode remelting. 3.3 Condition The product shall be supplied in the following condition; hardness shall be determined in accordance with ASTM A 370: 3.3.1 Bars Bar shall not be cut from plate. Hot finished, solution heat treated, and descaled, having hardness not lower t
18、han 42 HRC, or equivalent (See 8.2). 3.3.2 Forgings Hot finished, solution heat treated, and descaled, having hardness not lower than 42 HRC, or equivalent (See 8.2). 3.3.3 Forging Stock As ordered by the forging manufacturer. 3.4 Heat Treatment Bars and forgings shall be solution heat treated as in
19、 3.4.1 or 3.4.2, as applicable, holding at heat for sufficient time to ensure complete transformation, and quenching in agitated water sufficiently cool (See 8.3) to develop the mechanical properties specified herein. Pyrometry shall be in accordance with AMS2750. 3.4.1 Product 2.0 Inches (51 mm) an
20、d Under in Nominal Section Thickness Shall be solution heat treated by heating in air to 1525 F 25 (829 C 14) and quenching. 3.4.2 Product Over 2.0 Inches (51 mm) in Nominal Section Thickness Shall be solution heat treated by heating in air to 1650 F 25 (899 C 14), quenching, reheating to 1525 F 25
21、(829 C 14), and quenching. 3.5 Properties The product shall conform to the following requirements; tensile and impact testing shall be performed in accordance with ASTM A 370: 3.5.1 Bars and Forgings 3.5.1.1 As Solution Heat Treated Copyright SAE International Provided by IHS under license with SAEN
22、ot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AMS6543E Page 4 of 8 3.5.1.1.1 Macrostructure Visual examination of transverse full cross-sections from bars, forgings, and forging stock, etched in hot hydrochloric acid in accordance with ASTM A 604, shall show n
23、o 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 LIMITS Class Condition Severity 1 Freckles A 2 White Spots A 3 Radial Segregation B 4 Ring Pattern B 3.5.1.2 Response to Heat T
24、reatment (Maraging) for Bars and Forgings Bars and forgings shall meet the requirements of 3.5.1.2.1, 3.5.1.2.2, and 3.5.1.2.3 after being maraged by heating within the range 900 to 950 F (482 to 510 C), holding at the selected temperature within 10 F (6 C) for not less than 5 hours, and cooling in
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