SAE AMS 5711E-2015 Nickel Alloy Corrosion and Heat-Resistant Bars Forgings and Rings 65Ni - 15 8Cr - 15 2Mo - 0 30Al - 0 05La Solution Heat Treated (UNS N06635).pdf
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1、AEROSPACE MATERIAL SPECIFICATION AMS5711 REV. E Issued 1973-12 Reaffirmed 2007-08 Revised 2015-01 Superseding AMS5711D Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 65Ni - 15.8Cr - 15.2Mo - 0.30Al - 0.05La Solution Heat Treated (Composition similar to UNS N06635) RATIONALE AM
2、S5711E revises Condition, (3.3), Stress Rupture Testing (3.5.1.3.1), 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 of bars, forgings, flash welded rings, and stock for
3、 forging, flash welded rings, or heading. 1.2 Application These products have been used typically for parts, such as turbine rotors and seals, flanges, and fasteners, requiring relatively high strength up to 1800 F (982 C) and oxidation resistance up to 2000 F (1093 C), but usage is not limited to s
4、uch 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 issue is specified. Wh
5、en 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 (inside USA and Canada) or
6、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 Steels and Alloys, Wro
7、ught Products and Forging Stock _ 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 p
8、atent 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, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions. Copyright 2015 SAE International All ri
9、ghts 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 DOCUMENT ORDER: Tel: 877-606-7323 (inside USA
10、 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 this Technical Report, please visit http:/www.sae.org/technical/standards/AMS5711E SAE INTERNATIONAL AMS5711E Page 2 of 7 A
11、MS2374 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steel and Alloy Forgings AMS2750 Pyrometry AMS2806 Identification, Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and Alloy Steels and Corrosion and Heat-Resistant Steels and Alloys AMS2808 Identification, Forgings AM
12、S7490 Rings, Flash Welded, Corrosion and Heat-Resistant Austenitic Steels and Austenitic-Type Alloys, or 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. A
13、STM E8/E8M Tension Testing of Metallic Materials ASTM E10 Brinell 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 High-Temperature, Electrical, Magnetic, a
14、nd 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 analytical methods acceptable to purchaser.
15、 Table 1 Composition Element min max Carbon - 0.02 Manganese 0.30 1.00 Silicon 0.20 0.75 Phosphorus - 0.020 Sulfur - 0.015 Chromium 14.50 17.00 Molybdenum 14.00 16.50 Aluminum 0.10 0.50 Lanthanum 0.01 0.10 Cobalt - 2.00 Tungsten - 1.00 Boron - 0.015 Iron - 3.00 Copper - 0.35 Nickel remainder 3.1.1 C
16、heck Analysis Composition variations shall meet the applicable requirements of AMS2269. SAE INTERNATIONAL AMS5711E Page 3 of 7 3.2 Melting Practice Alloy shall be multiple melted using consumable electrode practice in the remelt cycle. 3.3 Condition The product shall be supplied in the following con
17、dition: 3.3.1 Bars, Forgings, and Flash Welded Rings Solution heat treated and descaled. 3.3.1.1 Bars shall be hot finished. Bars, other than hexagons, over 2.75 inches (69.8 mm) in nominal diameter or least distance between parallel sides shall be hot finished or cold finished. Round bars shall be
18、ground or turned. 3.3.1.2 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. 3.3.1.3 Bar shall not be cut from plate (Also see 4.4.5). 3.3.2 Stock for Forging, Flash Welded Rings, o
19、r Heading As ordered by the forging, flash welded ring, or heading manufacturer. 3.4 Solution Heat Treatment Bars, forgings, and flash welded rings shall be solution heat treated by heating to 1950 F 25 (1066 C 14), holding at heat for a time commensurate with section thickness, and cooling at a rat
20、e equivalent 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 as shown in Table 2, determined in accordance with ASTM E8/E8
21、M. Table 2 - MInimum tensile properties Property Value Tensile Strength 105 ksi (724 MPa) Yield Strength at 0.2% Offset 40.0 ksi (276 MPa) Elongation in 4D 48% Reduction of Area 47% 3.5.1.2 Hardness Shall be not higher than 241 HB, or equivalent (See 8.2), determined in accordance with ASTM E10. Pro
22、duct shall not be rejected on the 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. SAE INTERNATIONAL AMS5711E Page 4 of 7 3.5.1.3 S
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