SAE AMS 5716K-2016 Iron-Nickel Alloy Heat Resistant Bars Wire Forgings and Rings 44Fe - 18 5Cr - 35 5Ni - 1 1Si Solution Heat Treated (UNS N08330).pdf
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1、_ 6$(7HFKQLFDO6WDQGDUGV%RDUG5XOHVSURYLGHWKDW7KLV 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 therefrom, is
2、the sROHUHVSRQVLELOLWRIWKHXVHU 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 2016 SAE International All rights reserved. No part of this publication may b
3、e 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: +1 724-776-4970 (outside USA)
4、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:/standards.sae.org/AMS5716K AEROSPACE MATERIAL SPECIFICATION AMS5716 REV. K Issued 1964-01 Reaffirmed 2006-04 Revised 2016-10 Supe
5、rseding AMS5716J Iron-Nickel Alloy, Heat Resistant, Bars, Wire, Forgings, and Rings 44Fe - 18.5Cr - 35.5Ni - 1.1Si Solution Heat Treated (Composition similar to UNS N08330) RATIONALE AMS5716K revises Condition (3.2.1.2), Properties (3.4.1.1), and (Reports (4.4), and is a Five Year Review and update
6、of this specification. 1. SCOPE 1.1 Form This specification covers a heat-resistant iron-nickel alloy in the form of bars, wire, forgings, flash welded rings 8.0 inches (203 mm) and under in nominal diameter or least distance between parallel sides, and stock of any size for forging or flash welded
7、rings (see 8.5). 1.2 Application These products have been used typically for low-stressed parts requiring oxidation resistance up to 2100 F (1149 C), particularly where such parts may require welding during fabrication, but usage is not limited to such applications. 2. APPLICABLE DOCUMENT The issue
8、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 issue is specified. When the referenced document has been cancelled and no
9、 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 (inside USA and Canada) or +1 724-776-4970 (outside USA), www.sae.org. AMS2241
10、Tolerances, Corrosion and Heat-Resistant Steel, Iron Alloy, Titanium, and Titanium Alloy Bars and Wire AMS2248 Chemical Check Analysis Limits, Corrosion and Heat-Resistant Steels and Alloys, Maraging and Other Highly-Alloyed Steels, and Iron Alloys SAE INTERNATIONAL AMS5716K Page 2 of 6 AMS2371 Qual
11、ity 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 AMS2806 Identification Bars, Wire, Mechanical Tubing, and Extrusions, Carbon an
12、d 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 Precipitation-Hardenable Alloys ARP1917 Clarification of Terms Used in Aer
13、ospace Metals Specifications 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 E18 Rockwell Hardness of Metallic Materials ASTM E140
14、Standard Hardness Conversion Tables for Metals ASTM E353 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 i
15、n accordance with ASTM E353, by spectrochemical methods, or by other analytical methods acceptable to purchaser. Table 1 - Composition Element min max Carbon Manganese Silicon Phosphorus Sulfur Chromium Nickel Molybdenum Copper Tin Lead Iron - - 0.75 - - 17.00 34.00 - - - - remainder 0.08 2.00 1.50
16、0.030 0.030 20.00 37.00 0.75 0.50 0.025 0.005 SAE INTERNATIONAL AMS5716K Page 3 of 6 3.1.1 Check Analysis Composition variations shall meet the applicable requirements of AMS2248. 3.2 Condition The product shall be supplied in the following condition: 3.2.1 Bars, Wire, Forgings, and Flash Welded Rin
17、gs Solution heat treated. 3.2.1.1 Bars and wire may be hot or cold finished. 3.2.1.2 Bars shall not be cut from plate (also see 4.4.2). 3.2.1.3 Flash welded rings shall not be supplied unless specified or permitted on purchasers part drawing. When supplied, rings shall be manufactured in accordance
18、with AMS7490. 3.2.2 Stock for Forging or Flash Welded Rings As ordered by the forging or flash welded ring manufacturer. 3.3 Heat Treatment No specific heat treating instructions are specified, but bars, wire, forgings, and flash welded rings shall be solution heat treated to produce the properties
19、specified in 3.4.1 and 3.4.2. Recommended solution heat treatment is presented in 3.3.1. 3.3.1 Heat to a temperature not lower than 1900 F (1038 C), hold at heat for a time commensurate with section thickness and with heating equipment and procedures used, and cool at a rate equivalent to a rapid ai
20、r cool or faster. 3.4 Properties 3.4.1 Bars, Wire, Forgings and Flash Welded Rings Bars, wire, forgings, and flash welded rings, 8.0 inches (203 mm) and under in nominal diameter or least distance between parallel sides, shall conform to the following requirements. 3.4.1.1 Mechanical property requir
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