SAE AMS 5772D-2004 Cobalt Alloy Corrosion and Heat-Resistant Bars Forgings and Rings 40Co - 22Cr - 22Ni - 14 5W - 0 07La Solution Heat Treated (UNS R30188)《40Co 22Cr 22Ni 14 5W 0 0.pdf
《SAE AMS 5772D-2004 Cobalt Alloy Corrosion and Heat-Resistant Bars Forgings and Rings 40Co - 22Cr - 22Ni - 14 5W - 0 07La Solution Heat Treated (UNS R30188)《40Co 22Cr 22Ni 14 5W 0 0.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 5772D-2004 Cobalt Alloy Corrosion and Heat-Resistant Bars Forgings and Rings 40Co - 22Cr - 22Ni - 14 5W - 0 07La Solution Heat Treated (UNS R30188)《40Co 22Cr 22Ni 14 5W 0 0.pdf(8页珍藏版)》请在麦多课文档分享上搜索。
1、Cobalt Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings40Co - 22Cr - 22Ni - 14.5W - 0.07LaSolution Heat Treated(Composition similar to UNS R30188)1. SCOPE:1.1 Form: This specification covers a corrosion and heat-resistant cobalt alloy in the form of bars, forgings, flash welded rings,
2、and stock for forging or flash welded rings.1.2 Application: These products have been used typically for parts requiring high strength up to 1800 F (982 C) and oxidation resistance up to 2000 F (1093 C), but usage is not limited to such applications.2. APPLICABLE DOCUMENTS: The issue of the followin
3、g 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 and no superseding do
4、cument 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 www.sae.org.AMS 2261 Tolerances, Nickel, Nickel Alloy, and Cobalt Alloy Bars, Rods, and WireAMS 2269 Chemical Check Analysis
5、 Limits, Nickel, Nickel Alloys, and Cobalt AlloysAMS 2371 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steels and Alloys, Wrought Products and Forging StockAMS 2374 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steel and Alloy ForgingsAEROSPACE MATERIAL
6、 SPECIFICATIONAMS 5772DIssued 1971-05Revised 2004-01Superseding AMS 5772CReaffirmed 2009-06SAE 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
7、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 reaffirmed, revised, or cancelled. SAE invites your written comments and suggest
8、ions. Copyright 2009 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. TO PLACE A
9、DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: 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 feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AMS5772D
10、 Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AMS 5772D SAE AMS 5772D- 2 -2.1 (Continued):AMS 2750 PyrometryAMS 2806 Identification, Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and Alloy
11、 Steels and Corrosion and Heat-Resistant Steels and AlloysAMS 2808 Identification, ForgingsAMS 7490 Rings, Flash Welded, Corrosion and Heat-Resistant Austenitic Steels and Austenitic-Type Alloys, or Precipitation-Hardenable Alloys2.2 ASTM Publications: Available from ASTM, 100 Barr Harbor Drive, Wes
12、t Conshohocken, PA 19428-2959 or www.astm.org.ASTM E 8 Tension Testing of Metallic MaterialsASTM E 8M Tension Testing of Metallic Materials (Metric)ASTM E 10 Brinell Hardness of Metallic MaterialsASTM E 139 Creep, Creep-Rupture, and Stress-Rupture Tests of Metallic MaterialsASTM E 354 Chemical Analy
13、sis of High-Temperature, Electrical, Magnetic, and Other Similar Iron, Nickel, and Cobalt Alloys3. 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 354, by spectrochemical methods, or by
14、 other analytical methods acceptable to purchaser.3.1.1 Check Analysis: Composition variations shall meet the applicable requirements of AMS 2269.TABLE 1 - CompositionElement min maxCarbon 0.05 0.15Manganese - 1.25Silicon 0.20 0.50Phosphorus - 0.020Sulfur - 0.015Chromium 20.00 24.00Nickel 20.00 24.0
15、0Tungsten 13.00 16.00Lanthanum 0.02 0.12Boron - 0.015Iron - 3.00Cobalt remainderCopyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AMS 5772D SAE AMS 5772D- 3 -3.2 Condition: The product shall be supplie
16、d in the following condition:3.2.1 Bars: Hot finished and solution heat treated; round bars shall be ground or turned.3.2.2 Forgings and Flash Welded Rings: Solution heat treated. Surface finish shall be as agreed upon by purchaser and the forging or flash welded ring manufacturer.3.2.2.1 Flash weld
17、ed rings shall not be supplied unless specified or permitted on purchasers part drawing. When supplied, rings shall be manufactured in accordance with AMS 7490.3.2.3 Stock for Forging or Flash Welded Rings: As ordered by the forging or flash welded ring manufacturer.3.3 Solution Heat Treatment: Bars
18、, forgings, and flash welded rings shall be solution heat treated by heating to 2150 F 25 (1177 C 14), holding at heat for a time commensurate with cross-sectional thickness, and cooling at a rate which will produce product meeting the requirements of 3.4.1.1, 3.4.1.2, and 3.4.1.3. Pyrometry shall b
19、e in accordance with AMS 2750.3.3.1 Any thermal treatment following solution heat treatment as in 3.3 shall not involve use of temperatures higher than 2050 F 25 (1121 C 14).3.4 Properties: The product shall conform to the following requirements:3.4.1 Bars, Forgings, and Flash Welded Rings: 3.4.1.1
20、Tensile Properties: Specimens, taken in the longitudinal direction from bars, in the circumferential direction from parent metal of flash welded rings, and from forgings in locations agreed upon by purchaser and vendor, shall have the properties shown in Table 2, determined in accordance with ASTM E
21、 8 or ASTM E 8M.3.4.1.2 Hardness: Shall be as follows, determined in accordance with ASTM E 10:3.4.1.2.1 Bars: Not higher than 302 HB, or equivalent (See 8.2), determined approximately midway between center and surface.TABLE 2 - Minimum Tensile PropertiesProperty ValueTensile Strength 125 ksi (862 M
22、Pa) Yield Strength at 0.2% Offset 55 ksi (379 MPa)Elongation in 4D 45%Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AMS 5772D SAE AMS 5772D- 4 -3.4.1.2.2 Forgings and Flash Welded Rings: Not higher
23、 than 293 HB, or equivalent (See 8.2).3.4.1.3 Stress-Rupture Properties at 1700 F (927 C): A tensile specimen, maintained at 1700 F 3 (927 C 2) while a load sufficient to produce an initial axial stress of 13.0 ksi (90 MPa) or higher is applied continuously to specimens from bars and flash welded ri
24、ngs and of 12.0 ksi (83 MPa) or higher is similarly applied to specimens from forgings, shall not rupture in less than 23 hours. The test shall be continued to rupture without change of load. Elongation after rupture, measured at room temperature, shall be not less than 15% in 4D. Test shall be cond
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