SAE AMS 5759M-2015 Cobalt Alloy Corrosion and Heat-Resistant Bars Forging Stock Forgings and Rings 52Co C 20Cr C 10Ni C 15W (UNS R30605).pdf
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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 revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions. Copyright 2015 SAE International All rights reserved. No part of this p
3、ublication 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 DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: +1 724-776-497
4、0 (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/standards/AMS5759M AEROSPACE MATERIAL SPECIFICATION AMS5759 REV. M Issued 1986-02 Revised 2
5、015-12 Superseding AMS5759L Cobalt Alloy, Corrosion and Heat-Resistant, Bars, Forging Stock, Forgings, and Rings 52Co 20Cr 10Ni 15W (Similar to UNS R30605) RATIONALE AMS5759M revises condition (3.3.1.2), Properties (3.5.1.3) and Reports (4.4, 4.4.6, 4.4.7), and is a Five Year Review and update of th
6、is specification. 1. SCOPE 1.1 Form This specification covers a corrosion and heat-resistant cobalt 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 requiring high strengt
7、h up to 1500 F (816 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 following documents in effect on the date of the purchase order forms a part of this specification to the extent specified herein. The suppli
8、er 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 SAE Publications Available from SAE Internation
9、al, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or +1 724-776-4970 (outside USA), www.sae.org. AMS2261 Tolerances, Nickel, Nickel Alloy, and Cobalt Alloy Bars, Rods, and Wire AMS2269 Chemical Check Analysis Limits, Nickel, Nickel Alloys, and Cobalt Al
10、loys AMS2371 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steels and Alloys, Wrought Products and Forging Stock AMS2374 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steel and Alloy Forgings SAE INTERNATIONAL AMS5759M Page 2 of 7 AMS2750 Pyrometry AMS28
11、06 Identification Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and Alloy Steels and Corrosion and Heat-Resistant Steels and Alloys AMS2808 Identification Forgings AMS7490 Rings, Flash Welded, Corrosion and Heat-Resistant Austenitic Steels, Austenitic-Type Iron, Nickel, or Cobalt Alloys, or
12、Precipitation-Hardenable Alloys 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 E8/E8M Tension Testing of Metallic Materials ASTM E10 Brinell Hardness of Metallic Materials ASTM E13
13、9 Conducting Creep, Creep-Rupture, and Stress-Rupture Tests of Metallic Materials ASTM E354 Chemical Analysis of High-Temperature, Electrical, Magnetic, and Other Similar Iron, Nickel, and Cobalt Alloys 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the percentages by weight shown in Tab
14、le 1, determined by wet chemical methods in accordance with ASTM E354, by spectrochemical methods, or by other analytical methods acceptable to purchaser. Table 1 - Composition Element min max Carbon 0.05 0.15 Manganese 1.00 2.00 Silicon - 0.40 Phosphorus - 0.040 Sulfur - 0.030 Chromium 19.00 21.00
15、Nickel 9.00 11.00 Tungsten 14.00 16.00 Iron - 3.00 Cobalt remainder SAE INTERNATIONAL AMS5759M Page 3 of 7 3.1.1 Check Analysis Composition variations shall meet the applicable requirements of AMS2269. 3.2 Melting Practice Alloy shall be multiple melted using consumable electrode practice in the rem
16、elt cycle. 3.3 Condition The product shall be supplied in the following condition: 3.3.1 Bars, Forgings, and Flash Welded Rings Solution heat treated and descaled. 3.3.1.1 Bars shall be hot finished; round bars shall be ground or turned. 3.3.1.2 Bars shall not be cut from plate (also see 4.4.6). 3.3
17、.1.3 Flash welded rings shall not be supplied unless specified or permitted on purchasers part drawing. When supplied, rings shall be manufactured in accordance with AMS7490. 3.3.2 Stock for Forging, Flash Welded Rings, or Heading As ordered by the forging, flash welded ring, or heading manufacturer
18、. 3.4 Heat Treatment Bars, forgings, and flash welded rings shall be solution heat treated by heating to a temperature within the range 2150 to 2250 F (1177 to 1232 C), holding at the selected temperature within 25 F (14 C) for a time commensurate with section thickness, and cooling at a rate equiva
19、lent to an air cool or faster. Pyrometry shall be in accordance with AMS2750. 3.5 Properties The product shall conform to the following requirements: 3.5.1 Bars, Forgings, and Flash Welded Rings 3.5.1.1 Tensile Properties Shall be shown in Table 2, determined in accordance with ASTM E8/E8M. Table 2
20、- Minimum tensile properties Property Value Tensile Strength 125 ksi (862 MPa) Yield Strength at 0.2% Offset 45.0 ksi (310 MPa) Elongation in 4D 30% SAE INTERNATIONAL AMS5759M Page 4 of 7 3.5.1.2 Hardness Shall be as follows, determined in accordance with ASTM E10. Product shall not be rejected on t
21、he basis of hardness if the tensile properties of 3.5.1.1 are acceptable, determined on specimens taken from the same sample as that with nonconforming hardness or from another sample with similar nonconforming hardness. 3.5.1.2.1 Bars Not higher than 277 HB, or equivalent (see 8.2), taken approxima
22、tely midway between surface and center. 3.5.1.2.2 Forgings Not higher than 248 HB, or equivalent (see 8.2). 3.5.1.2.3 Flash Welded Rings Not higher than 302 HB, or equivalent (see 8.2). 3.5.1.3 Stress-Rupture Properties at 1,500 F (816 C) Product 0.1875 inch (4.76 mm) and greater in thickness or lea
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