SAE AMS 5708L-2015 Nickel Alloy Corrosion and Heat-Resistant Bars Wire Forgings and Rings 58Ni - 19 5Cr - 13 5Co - 4 3Mo - 3 0Ti - 1 4Al - 0 05Zr - 0 006B Consumable Electrode or V.pdf
《SAE AMS 5708L-2015 Nickel Alloy Corrosion and Heat-Resistant Bars Wire Forgings and Rings 58Ni - 19 5Cr - 13 5Co - 4 3Mo - 3 0Ti - 1 4Al - 0 05Zr - 0 006B Consumable Electrode or V.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 5708L-2015 Nickel Alloy Corrosion and Heat-Resistant Bars Wire Forgings and Rings 58Ni - 19 5Cr - 13 5Co - 4 3Mo - 3 0Ti - 1 4Al - 0 05Zr - 0 006B Consumable Electrode or V.pdf(7页珍藏版)》请在麦多课文档分享上搜索。
1、AEROSPACE MATERIAL SPECIFICATION AMS5708 REV. L Issued 1963-07 Revised 2015-01 Superseding AMS5708K Nickel Alloy, Corrosion and Heat-Resistant, Bars, Wire Forgings, and Rings 58Ni - 19.5Cr - 13.5Co - 4.3Mo - 3.0Ti - 1.4Al - 0.05Zr - 0.006B Consumable Electrode or Vacuum Induction Melted 1975 F (1079
2、 C) Solution Heat Treated (Composition similar to UNS N07001) RATIONALE AMS5708L revises the Title, Condition (3.3.1.1) and Reports (4.4), and is a Five Year Review and update of this specification. 1. SCOPE 1.1 Form This specification covers a corrosion and heat-resistant nickel alloy in the form o
3、f bars, wire, 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 bolts and turbine blades, requiring high strength up to 1500 F (816 C) and oxidation resistance up to 1750 F (954 C), but usag
4、e 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 a subsequent revision of a document unless a specific document i
5、ssue 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 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (insid
6、e USA and Canada) or 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 Alloys AMS2371 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant S
7、teels and Alloys, Wrought Products and Forging Stock AMS2374 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steel and Alloy Forgings _ SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences.
8、The use of this report is entirely voluntary, 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 revised, reaff
9、irmed, stabilized, or cancelled. SAE invites your written comments and suggestions. Copyright 2015 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, rec
10、ording, 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: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org SAE values your input. To provide feedback on
11、this Technical Report, please visit http:/www.sae.org/technical/standards/AMS5708L SAE INTERNATIONAL AMS5708L Page 2 of 7 AMS2750 Pyrometry AMS2806 Identification, Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and Alloy Steels and Corrosion and Heat Resistant Steels and Alloys AMS2808 Identi
12、fication, Forgings AMS7490 Rings, Flash Welded, Corrosion and Heat-Resistant Austenitic Steels, Austenitic-Type Iron, Nickel, or Cobalt Alloys, or Precipitation-Hardenable Alloys 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 1942
13、8-2959, Tel: 610-832-9585, www.astm.org. ASTM E10 Brinell Hardness of Metallic Materials ASTM E18 Rockwell Hardness of Metallic Materials ASTM E112 Determining Average Grain Size ASTM E139 Conducting Creep, Creep-Rupture, and Stress-Rupture Tests of Metallic Materials ASTM E354 Chemical Analysis of
14、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 Table 1, determined by wet chemical methods in accordance with ASTM E354, by spectrochemical methods, or by other an
15、alytical methods acceptable to purchaser. Table 1 - Composition Element min max Carbon 0.02 0.10 Manganese - 0.10 Silicon - 0.15 Phosphorus - 0.015 Sulfur - 0.015 Chromium 18.00 21.00 Cobalt 12.00 15.00 Molybdenum 3.50 5.00 Titanium 2.75 3.25 Aluminum 1.20 1.60 Boron 0.003 0.010 Zirconium 0.02 0.08
16、Iron - 2.00 Copper - 0.10 Lead - 0.0005 (5 ppm) Bismuth - 0.00003 (0.3 ppm) Selenium - 0.0003 (3 ppm) Nickel remainder 3.1.1 Check Analysis Composition variations shall meet the applicable requirements of AMS2269. No variation is permitted for lead, bismuth, and selenium. SAE INTERNATIONAL AMS5708L
17、Page 3 of 7 3.2 Melting Practice Alloy shall be multiple melted using consumable electrode practice in the remelt cycle or shall be multiple vacuum melted. If consumable electrode remelting is not performed in vacuum, electrodes which have been produced by vacuum induction melting shall be used for
18、remelting. 3.3 Condition The product shall be supplied in the following condition: 3.3.1 Bars Hot finished, solution heat treated and descaled except round bars shall be ground or turned. 3.3.1.1 Bars shall not be cut from plate (Also see 4.4.1). 3.3.2 Wire Solution heat treated and cold finished. 3
19、.3.3 Forgings and Flash Welded Rings Solution heat treated and descaled. 3.3.3.1 Flash welded rings shall not be supplied unless specified or permitted on purchasers part drawing. When supplied, rings shall be manufactured in accordance with AMS7490. 3.3.4 Stock for Forging or Flash Welded Rings As
20、ordered by the forging or flash welded ring manufacturer. 3.3.5 Stock for Heading Type 1 - Bar - Solution heat-treated, cold reduced and centerless ground. Type 2 - Bar - Solution heat treated and centerless ground. Wire - Solution heat treated and cold finished. 3.3.5.1 Unless a specific type is or
21、dered, type 1 shall be supplied for bar product. 3.4 Heat Treatment Shall be as follows; pyrometry shall be in accordance with AMS2750. 3.4.1 Bars, Wire, Forgings, and Flash Welded Rings Shall be solution heat treated by heating to 1975 F 25 (1079 C 14), holding at heat for 4 hours 0.5, and cooling
22、at a rate equivalent to an air cool or faster. SAE INTERNATIONAL AMS5708L Page 4 of 7 3.4.2 Stock for Heading Shall be solution heat treated by heating within the range 1900 to 1975 F (1038 to 1079 C), holding at the selected temperature within 25 F (14 C) for 1 to 4 hours, and cooling at a rate equ
23、ivalent to an air cool or faster. 3.5 Properties The product shall conform to the following requirements: 3.5.1 Bars, Wire, Forgings, and Flash Welded Rings 3.5.1.1 As Solution Heat Treated 3.5.1.1.1 Hardness (Bars 0.500 inch (12.7 mm) and Above) Shall be not higher than 302 HB, or equivalent (See 8
24、.2), determined in accordance with ASTM E10. 3.5.1.1.1.1 In lieu of 3.5.1.1.1, bars less than 0.500 inch (12.7 mm) shall have a tensile strength not higher than 145 ksi (1000 MPa). 3.5.1.1.2 Tensile (Wire) Shall have a tensile strength not higher than 145 ksi (1000 MPa). 3.5.1.1.3 Average grain size
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