SAE AMS 5930A-2005 Steel Corrosion-Resistant Bars and Forgings 13 0Cr - 2 5Ni - 5 5Co - 2 0Mo - 0 60V (0 05 - 0 09C) Vacuum Induction Plus Vacuum Consumable Electrode Melted《真空感应加真.pdf
《SAE AMS 5930A-2005 Steel Corrosion-Resistant Bars and Forgings 13 0Cr - 2 5Ni - 5 5Co - 2 0Mo - 0 60V (0 05 - 0 09C) Vacuum Induction Plus Vacuum Consumable Electrode Melted《真空感应加真.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 5930A-2005 Steel Corrosion-Resistant Bars and Forgings 13 0Cr - 2 5Ni - 5 5Co - 2 0Mo - 0 60V (0 05 - 0 09C) Vacuum Induction Plus Vacuum Consumable Electrode Melted《真空感应加真.pdf(8页珍藏版)》请在麦多课文档分享上搜索。
1、 AEROSPACE MATERIAL SPECIFICATION Steel, Corrosion-Resistant, Bars and Forgings 13.0Cr - 2.5Ni - 5.5Co - 2.0Mo - 0.60V (0.05 - 0.09C) Vacuum Induction Plus Vacuum Consumable Electrode Melted (Composition similar to UNS S42670) AMS 5930ASuperseding AMS 5930 1. SCOPE: 1.1 Form: This specification cove
2、rs a premium aircraft-quality, alloy steel in the form of bars, forgings, and forging stock. 1.2 Application: These products have been used typically for carburized parts requiring high minimum case hardness and corrosion resistance equivalent to AISI Type 440C, but usage is not limited to such appl
3、ications. These products are suitable for service up to 675 F (357 C). 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 subsequent revision of a docu
4、ment 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, 400 Commonwealth Drive, Warrendale, PA, 15096-0001 or w
5、ww.sae.org. AMS 2241 Tolerances, Corrosion and Heat-Resistant Steel, Iron Alloy, Titanium, and Titanium Alloy Bars and Wire AMS 2248 Chemical Check Analysis Limits, Corrosion and Heat-Resistant Steels and Alloys, Maraging and Other Highly-Alloyed Steels, and Iron Alloys AMS 2300 Steel Cleanliness, P
6、remium Aircraft-Quality, Magnetic Particle Inspection Procedure Issued 1990-10 Revised 2005-08Reaffirmed 2010-10 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
7、, and its applicability and suitability for any particular use, including any patent infringement arising therefrom, 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 writte
8、n comments and suggestions. Copyright 2010 SAE International All rights reserved. No part of this publication 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 permissi
9、on of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: +1 724-776-4970 (outside USA) Fax: 724-776-0790 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/te
10、chnical/standards/AMS5930A Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE- 2 - AMS 5930A AMS 5930A2.1 (Continued): AMS 2371 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant S
11、teels and Alloys, Wrought Products and Forging Stock AMS 2374 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steel and Alloy Forgings AMS 2806 Identification, Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and Alloy Steels and Corrosion and Heat-Resistant Steels and Allo
12、ys AMS 2808 Identification, Forgings AS1182 Standard Machining Allowance, Aircraft-Quality and Premium Aircraft-Quality Steel Bars and Mechanical Tubing 2.2 ASTM Publications: Available from ASTM, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959 or www.astm.org. ASTM A 370 Mech
13、anical Testing of Steel Products ASTM A 604 Macroetch Testing of Consumable Electrode Remelted Steel Bars and BilletsASTM E 45 Determining the Inclusion Content of Steel ASTM E 112 Determining Average Grain Size ASTM E 353 Chemical Analysis of Stainless, Heat-Resisting, Maraging, and Other Similar C
14、hromium-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 E 353, by spectrochemical methods, or by other analytical methods acceptable to purchaser. TABLE 1 - Composit
15、ion Element min max CarbonManganeseSiliconPhosphorusSulfurChromiumNickelCobaltMolybdenumVanadium0.050.500.10-12.002.004.001.500.400.091.000.700.0150.01014.003.007.002.500.80Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without
16、 license from IHS-,-,-SAE- 3 - AMS 5930A AMS 5930A3.1.1 Check Analysis: Composition variations shall meet the applicable requirements of AMS 2248. 3.2 Melting Practice: Steel shall be multiple melted using vacuum induction melting practice followed by vacuum consumable electrode remelting. 3.3 Condi
17、tion: The product shall be supplied in the following condition; hardness and tensile strength shall be determined in accordance with ASTM A 370: 3.3.1 Bars: 3.3.1.1 Bars 0.500-Inch (12.70-mm) and Under in Nominal Diameter or Least Distance Between Parallel Sides: Annealed and cold-finished having te
18、nsile strength not higher than 150 ksi(1034 MPa) or equivalent hardness (See 8.2). 3.3.1.2 Bars Over 0.500-Inch (12.70-mm) in Nominal Diameter or Least Distance Between Parallel Sides: Hot finished and annealed, unless otherwise ordered, having hardness not higher than 302 HB, or equivalent (See 8.3
19、). Bars ordered annealed and cold finished may have hardness as high as 311 HB, or equivalent (See 8.3). 3.3.2 Forgings: Annealed. 3.3.3 Forging Stock: As ordered by the forging manufacturer. 3.4 Properties: The product shall conform to the following requirements:3.4.1 Macrostructure: Visual examina
20、tion of transverse full cross-sections from bars, billets, and forging stock, etched in hot hydrochloric acid in accordance with ASTM A 604, shall show no pipe or cracks. Porosity, segregation, inclusions, and other imperfections for product 36 square inches (232 cm2) and under in nominal cross-sect
21、ional area shall be no worse than the macrographs of ASTM A 604 shown in Table 2. TABLE 2 - Macrostructure Limits Class Condition Severity 1234FrecklesWhite Spots Radial Segregation Ring Pattern AABBCopyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or ne
22、tworking permitted without license from IHS-,-,-SAE- 4 - AMS 5930A AMS 5930A3.4.2 Micro-Inclusion Rating: No specimen shall exceed the limits of Table 3, determined in accordance with ASTM E 45, Method D. TABLE 3 - Micro-Inclusion Rating Limits A ThinAHeavyBThinBHeavyCThinCHeavyDThinDHeavyWorst Fiel
23、d Severity Worst Field Frequency maximum Total Rateable Fields, Frequency, maximum2.0ab1.0111.5ab1.0111.5ab1.0111.55c1.011a Combined A+B+C, not more than three fields of No. 2.0 A Type or No. 1.5 B and C Types b Combined A+B+C, not more than eight fields c Any number of lower rateable fields is perm
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