SAE AMS 6543F-2016 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).pdf
《SAE AMS 6543F-2016 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).pdf》由会员分享,可在线阅读,更多相关《SAE AMS 6543F-2016 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).pdf(7页珍藏版)》请在麦多课文档分享上搜索。
1、_ 6$(7HFKQLFDO6WDQGDUGV%RDUG5XOHVSURYLGHWKDW7KLVUHSRUWLVSX EOLVKHGE6$(WRDGYDQFHWKHVWDWHRIWHFKQLFDODQGHQJL neering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefrom, LVWKHVROHUHVSRQ
2、VLELOLWRIWKHXVHU 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 2016 SAE International All rights reserved. No part of this publication may be reproduced,
3、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: 724-776-0
4、790 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/AMS6543F AEROSPACE MATERIAL SPECIFICATION AMS6543 REV. F Issued 1975-09 Revised 2016-02 Superseding AMS6543E St
5、eel, 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 AMS6543F results from a Five Year Review and update of this specification that revises reporting. 1. SCOPE 1.1 Form
6、This specification 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 c
7、ombination 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
8、 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 Publications Available from SAE International, 400 Common
9、wealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or +1 724-776-4970 (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-
10、Alloy Steel Bars AMS2370 Quality Assurance Sampling and Testing, Carbon and Low-Alloy Steel Wrought Products and Forging Stock SAE INTERNATIONAL $06 F Page 2 of 7 AMS2372 Quality Assurance Sampling and Testing Carbon and Low-Alloy Steel Forgings AMS2630 Inspection, Ultrasonic, Product Over 0.5 Inch
11、(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 Alloys AMS2808 Identification Forgings AS1182 Standard Stock Removal Allowance, Aircraft-Quality and Premium Aircraft-Quality St
12、eel 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. ASTM A370 Mechanical Testing of Steel Products ASTM A604 Macroetch Testing of Consumable Electrode Remelted
13、 Steel Bars and Billets ASTM E353 Chemical Analysis of Stainless, Heat-Resisting, Maraging, and Other Similar Chromium-Nickel-Iron Alloys 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the percentages by weight shown in Table 1, determined by wet chemical methods in accordance with ASTM
14、E353, 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 0.25 Silicon - 0.10 Phosphorus - 0.010 Sulfur - 0.006 Chromium 1.80 2.20 Nickel 9.50 10.50 Cobalt 7.50 8.50 Molybdenum 0.90 1.10 Titanium -
15、0.015 Aluminum - 0.025 Oxygen - 0.0025 (25 ppm) Nitrogen - 0.0075 (75 ppm) 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 fo
16、llowed by vacuum consumable electrode remelting. SAE INTERNATIONAL $06 F Page 3 of 7 3.3 Condition The product shall be supplied in the following condition; hardness shall be determined in accordance with ASTM A370: 3.3.1 Bars Bar shall not be cut from plate (also see 4.4.2). Hot finished, solution
17、heat treated, and descaled, having hardness not lower than 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
18、 Bars and forgings shall be solution heat treated as in 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 accor
19、dance with AMS2750. 3.4.1 Product 2.0 Inches (51 mm) and Under in Nominal Section Thickness Shall be solution heat treated by heating in air to 1525 F 25 F (829 C 14 C) 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
20、to 1650 F 25 F (899 C 14 C), quenching, reheating to 1525 F 25 F (829 C 14 C), and quenching. 3.5 Properties The product shall conform to the following requirements; tensile and impact testing shall be performed in accordance with ASTM A370: 3.5.1 Bars and Forgings 3.5.1.1 As Solution Heat Treated 3
21、.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 A604, shall show no pipe or cracks. Porosity, segregation, inclusions, and other imperfections shall be no worse than the macro
22、graphs of ASTM A604 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 SAE INTERNATIONAL $06 F Page 4 of 7 3.5.1.2 Response to Heat Treatment (Maraging) for Bars and Forgings Bars and forgings shall meet the
23、 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 air. 3.5.1.2.1 Tensile Properties Shall be as shown in Table 3. Table 3A -
24、 Minimum tensile properties, inch/pound units Nominal Diameter or Least Distance Between Parallel Sides Inches Tensile Strength ksi Yield Strength at 0.2% Offset ksi Elongation in 4D % Reduction of Area % 0.500 to 2.000, incl 190 180 12 60 Over 2.000 to 4.000, incl 190 175 12 60 Over 4.000 to 8.000,
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