SAE AMS 5762G-2016 Steel Corrosion Resistant Bars Wire and Forgings 5 8Mn - 17Cr - 5 8Ni - 2 0Cu - 0 26S Free Machining Solution Heat Treated (UNS S20300).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 2016 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/AMS5762G AEROSPACE MATERIAL SPECIFICATION AMS5762 REV. G Issued 1971-05 Reaffirme
5、d 2006-04 Revised 2016-02 Superseding AMS5762F Steel, Corrosion Resistant, Bars, Wire, and Forgings 5.8Mn - 17Cr - 5.8Ni - 2.0Cu - 0.26S Free Machining, Solution Heat Treated (Composition similar to UNS S20300) RATIONALE AMS5762G revises Condition (3.2.1.3) and Reports (4.4), and is a Five Year Revi
6、ew and update of this specification. 1. SCOPE 1.1 Form This specification covers a free-machining, corrosion-resistant steel in the form of bars, wire, forgings, and forging stock. 1.2 Application This product has been used typically for parts on which the amount of machining warrants use of a free-
7、machining grade of steel, requiring corrosion resistance similar to the 18-8 type steels but not subjected to temperatures exceeding 700 F (371 C) during fabrication or in service, but usage is not limited to such applications. 2. APPLICABLE DOCUMENTS The issue of the following documents in effect o
8、n 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 document has been specifi
9、ed, 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 Tolerances, Corrosion and Heat-Resista
10、nt 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 AMS2371 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steels and A
11、lloys, Wrought Products and Forging Stock SAE INTERNATIONAL AMS5762G Page 2 of 5 AMS2374 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steel and Alloy Forgings AMS2806 Identification Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and Alloy Steels and Corrosion and Heat-
12、Resistant Steels and Alloys AMS2808 Identification Forgings 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 A370 Mechanical Testing of Steel Products ASTM E353 Chemical Analysis of
13、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 ASTM E353, by spectrochemical methods, or by other analytica
14、l methods acceptable to purchaser. Table 1 - Composition Element min max Carbon - 0.08 Manganese 5.00 6.50 Silicon 0.20 0.70 Phosphorus - 0.04 Sulfur 0.15 0.35 Chromium 16.00 18.00 Nickel 5.00 6.50 Copper 1.75 2.25 Molybdenum - 0.50 3.1.1 Check Analysis Composition variations shall meet the applicab
15、le requirements of AMS2248. 3.2 Condition The product shall be supplied in the following condition: 3.2.1 Bars, Wire, and Forgings Solution heat treated. 3.2.1.1 All hexagons, other bars 2.750 inches (69.85 mm) and under in nominal diameter or least distance between parallel sides, and wire shall be
16、 cold finished. 3.2.1.2 Bars, other than hexagons, over 2.750 inches (69.85 mm) in nominal diameter or least distance between parallel sides shall be hot finished or cold finished. 3.2.1.3 Bars shall not be cut from plate. (Also see 4.4.2). SAE INTERNATIONAL AMS5762G Page 3 of 5 3.2.2 Forging Stock
17、As ordered by the forging manufacturer. 3.3 Properties The product shall conform to the following requirements; hardness and tensile testing shall be performed in accordance with ASTM A370: 3.3.1 Tensile Properties of Wire Shall have tensile strength of 85 to 125 ksi (586 to 862 MPa). 3.3.2 Hardness
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