SAE AMS 5891B-2007 Nickel Alloy Corrosion and Heat-Resistant Bars Forgings and Rings 60Ni - 22Cr - 2 0Mo - 14W - 0 35Al - 0 03La Annealed (UNS N06230)《60Ni 22Cr 2 0Mo 14W 0 35Al 0 .pdf
《SAE AMS 5891B-2007 Nickel Alloy Corrosion and Heat-Resistant Bars Forgings and Rings 60Ni - 22Cr - 2 0Mo - 14W - 0 35Al - 0 03La Annealed (UNS N06230)《60Ni 22Cr 2 0Mo 14W 0 35Al 0 .pdf》由会员分享,可在线阅读,更多相关《SAE AMS 5891B-2007 Nickel Alloy Corrosion and Heat-Resistant Bars Forgings and Rings 60Ni - 22Cr - 2 0Mo - 14W - 0 35Al - 0 03La Annealed (UNS N06230)《60Ni 22Cr 2 0Mo 14W 0 35Al 0 .pdf(6页珍藏版)》请在麦多课文档分享上搜索。
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 2013 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/AMS5891B AEROSPACE MATERIAL SPECIFICATION AMS5891 REV. B Issued 1992-04 Revised 2
5、007-11 Reaffirmed 2013-12 Superseding AMS5891A Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 60Ni - 22Cr - 2.0Mo - 14W - 0.35Al - 0.03La Annealed (Composition similar to UNS N06230) RATIONALE AMS5891B has been reaffirmed to comply with the SAE five-year review policy. 1. SCOP
6、E 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 forging, flash welded rings, or heading. 1.2 Application These products have been used typically for parts, such as turbine rotors, shafts, flanges, blade
7、s, and bolts, requiring oxidation resistance up to 2100 F (1149 C) and relatively high strength up to 1800 F (982 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 specifica
8、tion 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 specified, the last published issue of that document shall apply. 2.1
9、SAE Publications Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org. AMS 2261 Tolerances, Nickel, Nickel Alloy, and Cobalt Alloy Bars, Rods, and Wire AMS 2269 Chemical Check Analysi
10、s Limits, Nickel, Nickel Alloys and Cobalt Alloys AMS 2371 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steels and Alloys, Wrought Products and Forging Stock AMS 2374 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steel and Alloy Forgings AMS 2750 Pyrome
11、try AMS 2806 Identification, Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and Alloy Steels and Corrosion and Heat-Resistant Steels and Alloys AMS 2808 Identification, Forgings AMS 7490 Rings, Flash Welded, Corrosion and Heat-Resistant Austenitic Steels and Austenitic-Type Alloys SAE INTERNA
12、TIONAL AMS5891B Page 2 of 6 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 E 8 Tension Testing of Metallic Materials ASTM E 8M Tension Testing of Metallic Materials (Metric) ASTM E
13、 10 Brinell Hardness of Metallic Materials ASTM E 112 Determining Average Grain Size ASTM E 139 Conducting Creep, Creep-Rupture, and Stress-Rupture Tests of Metallic Materials ASTM E 354 Chemical Analysis of High-Temperature, Electrical, Magnetic, and Other Similar Iron, Nickel, and Cobalt Alloys 3.
14、 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 E 354, by spectrochemical methods, or by other analytical methods acceptable to purchaser. TABLE 1 - COMPOSITION Element min max Carbon 0.05
15、 0.15 Manganese 0.30 1.00 Silicon 0.25 0.75 Phosphorus - 0.03 Sulfur - 0.015Chromium 20.00 24.00 Molybdenum 1.00 3.00 Tungsten 13.00 15.00 Aluminum 0.20 0.50 Lanthanum 0.005 0.05 Cobalt - 5.00 Titanium - 0.10 Boron - 0.015Iron - 3.00 Copper - 0.50 Nickel remainder3.1.1 Check Analysis Composition var
16、iations shall meet the applicable requirements of AMS 2269; check analysis limits for lanthanum shall be 0.002 under minimum and 0.01 over maximum. 3.2 Condition The product shall be supplied in the following condition: 3.2.1 Bars Hot finished and annealed; round bars shall be ground or turned. 3.2.
17、2 Forgings and Flash Welded Rings Annealed. SAE INTERNATIONAL AMS5891B Page 3 of 6 3.2.2.1 Flash welded rings shall not be supplied unless specified or permitted on purchasers part drawing. When supplied, rings shall be manufactured in accordance with AMS 7490. 3.2.3 Stock For Forging, Flash Welded
18、Rings, or Heading As ordered by the forging, flash welded rings, or heading manufacturer. 3.3 Heat Treatment Bars, forgings, and flash welded rings shall be solution heat treated by heating within the range 2150 to 2275 F (1177 to 1246 C), holding at the selected temperature within 25 F (14 C) for a
19、 time commensurate with section thickness but not less than 20 minutes, and water quenching or otherwise rapidly cooling. Pyrometry shall be in accordance with AMS 2750. 3.4 Properties The product shall conform to the following requirements: 3.4.1 Bars, Forgings, and Flash Welded Rings 3.4.1.1 Tensi
20、le Properties Specimens taken in the longitudinal direction from bars, in the circumferential direction from parent metal of flash welded rings, and from forgings in locations agreed upon by purchaser and vendor shall have the properties shown in Table 2, determined in accordance with ASTM E 8 or AS
21、TM E 8M. TABLE 2 - MINIMUM TENSILE PROPERTIES Property Value Tensile Strength 110.0 ksi (758 MPa)Yield Strength at 0.2% 45.0 ksi (310 MPa)Elongation in 4D 35% 3.4.1.2 Hardness shall be not higher than 241 HB, or equivalent (See 8.2), determined in accordance with ASTM E 10. Hardness of bars shall be
22、 determined at approximately midradius of rounds and at approximately T/4 of other shapes. 3.4.1.3 Stress Rupture Properties at 1700 F (927 C) A tensile specimen, maintained at 1700 F 3 (927 C 2) while a load sufficient to produce an initial axial stress of 9.0 ksi (62 MPa) is applied continuously,
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