SAE AMS 5769F-2003 Alloy Corrosion and Heat-Resistant Bars Forgings and Rings 21Cr - 20Ni - 20Co - 3 0Mo - 2 5W - 1 0(Cb+Ta) - 0 15N - 32Fe Solution Heat Treated (UNS R30155)《固溶热处理.pdf
《SAE AMS 5769F-2003 Alloy Corrosion and Heat-Resistant Bars Forgings and Rings 21Cr - 20Ni - 20Co - 3 0Mo - 2 5W - 1 0(Cb+Ta) - 0 15N - 32Fe Solution Heat Treated (UNS R30155)《固溶热处理.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 5769F-2003 Alloy Corrosion and Heat-Resistant Bars Forgings and Rings 21Cr - 20Ni - 20Co - 3 0Mo - 2 5W - 1 0(Cb+Ta) - 0 15N - 32Fe Solution Heat Treated (UNS R30155)《固溶热处理.pdf(6页珍藏版)》请在麦多课文档分享上搜索。
1、AEROSPACE MATERIAL SPECIFICATION AMS5769 REV. F Issued 1960-06 Revised 2003-10 Reaffirmed 2014-10 Superseding AMS5769E Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings,21Cr - 20Ni - 20Co - 3.0Mo - 2.5W - 1.0(Cb+Ta) - 0.15N - 32Fe Solution Heat Treated (Composition similar to UNS R30155
2、) RATIONALE AMS5769F has been reaffirmed to comply with the SAE five year review policy. _ 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 applicabilit
3、y 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 revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments
4、 and suggestions. Copyright 2014 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 permission of SAE.
5、 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/technical/st
6、andards/AMS5769F 1. SCOPE: 1.1 Form: This specification covers a corrosion and heat-resistant alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings, or heading. 1.2 Application: These products have been used typically for parts, such as turbine rotors, sh
7、afts, blades, and bolts, requiring high strength up to 1350 F (732 C) and oxidation resistance up to 1800 F (982 C), 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 specifica
8、tion 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 shall apply. 2.1 S
9、AE Publications: Available from SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001 or www.sae.org. AMS 2248 Chemical Check Analysis Limits, Corrosion and Heat-Resistant Steels and Alloys, Maraging and Other Highly-Alloyed Steels, and Iron Alloys AMS 2261 Tolerances, Nickel, Nickel Alloy, and Cob
10、alt Alloy Bars, Rods, and Wire AMS 2371 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steels and Alloys, Wrought Products and Forging Stock AMS 2374 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steel and Alloy Forgings SAE INTERNATIONAL AMS5769F Page 2
11、of 6 2.1 (Continued): AMS 2806 Identification, Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and Alloy Steels and Corrosion and Heat-Resistant Steels and Alloys AMS 2808 Identification, Forgings AMS 7490 Rings, Flash Welded, Corrosion and Heat-Resistant Austenitic Steels, Austenitic- Type Al
12、loys, Nickel or Cobalt Alloys, or Precipitation-Hardenable Alloys 2.2 ASTM Publications: Available from ASTM, 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959 or www.astm.org. ASTM E 10 Brinell Hardness of Metallic Materials ASTM E 139 Conducting Creep, Creep-Rupture, and Stress-Rupture Tests
13、 of Metallic Materials ASTM E 353 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 AST
14、M E 353, by spectrochemical methods, or by other analytical methods acceptable to purchaser. TABLE 1 - Composition Element min max Carbon 0.08 0.16 Manganese 1.00 2.00 Silicon - 1.00 Phosphorus - 0.040 Sulfur - 0.030 Chromium 20.00 22.50 Nickel 19.00 21.00 Cobalt 18.50 21.00 Molybdenum 2.50 3.50 Tun
15、gsten 2.00 3.00 Columbium 0.75 1.25 Nitrogen 0.10 0.20 Iron remainder SAE INTERNATIONAL AMS5769F Page 3 of 6 3.1.1 Check Analysis: Composition variations shall meet the applicable requirements of AMS 2248. 3.2 Condition: The product shall be supplied in the following condition: 3.2.1 Bars, Forgings,
16、 and Flash Welded Rings: Solution heat treated. Forgings shall be descaled. 3.2.1.1 Flash welded rings shall not be supplied unless specified or permitted on purchasers part drawing. When supplied, rings shall be manufactured in accordance with AMS 7490. 3.2.2 Stock for Forging, Flash Welded Rings,
17、or Heading: As ordered by the forging, flash welded ring, or heading manufacturer. 3.3 Heat Treatment: Bars, forgings, and flash welded rings shall be solution heat treated by heating to 2150 F 25 (1177 C 14), holding at heat for not less than 1 hour, and quenching in water. 3.4 Properties: The prod
18、uct shall conform to the following requirements: 3.4.1 Bars, Forgings, and Flash Welded Rings: 3.4.1.1 Hardness: Shall be as follows, determined in accordance with ASTM E 10: 3.4.1.1.1 Bars and Forgings: 156 to 217 HB, or equivalent (See 8.2). 3.4.1.1.2 Flash Welded Rings: 156 to 241 HB, or equivale
19、nt (See 8.2). 3.4.1.2 Stress-Rupture Properties at 1350 F (732 C): A tensile specimen, maintained at 1350 F 3 (732 C 2) while a load sufficient to produce an initial axial stress of 32.0 ksi (221 MPa) or higher is applied continuously, shall not rupture in less than 23 hours. The test shall be conti
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