SAE AMS 5771F-2009 Nickel Alloy Corrosion and Heat-Resistant Bars Forgings and Rings 74Ni C 7 0Cr C 16 5 Mo Solution Heat Treated (UNS N10003)《74Ni 7 0Cr 16 5Mo溶解热处理 耐腐蚀和耐热镍合金棒材 锻件.pdf
《SAE AMS 5771F-2009 Nickel Alloy Corrosion and Heat-Resistant Bars Forgings and Rings 74Ni C 7 0Cr C 16 5 Mo Solution Heat Treated (UNS N10003)《74Ni 7 0Cr 16 5Mo溶解热处理 耐腐蚀和耐热镍合金棒材 锻件.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 5771F-2009 Nickel Alloy Corrosion and Heat-Resistant Bars Forgings and Rings 74Ni C 7 0Cr C 16 5 Mo Solution Heat Treated (UNS N10003)《74Ni 7 0Cr 16 5Mo溶解热处理 耐腐蚀和耐热镍合金棒材 锻件.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 2014 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/AMS5771F AEROSPACE MATERIAL SPECIFICATION AMS5771 REV. F Issued 1971-05Revised 20
5、09-04 Reaffirmed 2014-06 Superseding AMS5771E Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 74Ni 7.0Cr 16.5 Mo Solution Heat Treated (Composition similar to UNS N10003) RATIONALE This document has been reaffirmed to comply with the SAE five-year review policy. 1. SCOPE 1.1 Fo
6、rm This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings. 1.2 Application These products have been used typically for parts, such as turbine air-sealing components, requiring moderate stren
7、gth up to 1400 F (760 C) and oxidation resistance up to 1600 F (871 C), particularly where a low coefficient of expansion is desirable, 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
8、 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 specified, the last published issue of that document
9、 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 724-776-4970 (outside USA), www.sae.org. AMS2261 Tolerances, Nickel, Nickel Alloy, and Cobalt Alloy Bars, Rods, and Wire AMS2269 Chemic
10、al Check Analysis Limits, Nickel, Nickel Alloys, and Cobalt Alloys AMS2371 Quality 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
11、AMS2750 Pyrometry AMS2806 Identification, Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and Alloy Steels and Corrosion and Heat-Resistant Steels and Alloys SAE INTERNATIONAL AMS5771F Page 2 of 6 AMS2808 Identification, Forgings AMS7490 Rings, Flash Welded, Corrosion and Heat-Resistant Austen
12、itic 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 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM E 10 Brinell Hardness of Metallic Mat
13、erials 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. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the percentages by we
14、ight 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 0.04 0.08 Manganese - 1.00 Silicon - 1.00 Phosphorus - 0.015 Sulfur - 0.020 Chromi
15、um 6.00 8.00 Molybdenum 15.75 17.25 Cobalt - 0.20 Tungsten - 0.50 Aluminum + Titanium - 0.50 Boron - 0.01 Iron - 5.00 Copper - 0.35 Nickel remainder 3.1.1 Check Analysis Composition variations shall meet the applicable requirements of AMS2269. 3.2 Condition The product shall be supplied in the follo
16、wing condition: 3.2.1 Bars, Forgings, and Flash Welded Rings Solution heat treated and descaled. 3.2.1.1 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. 3.2.2 Stock for Forging o
17、r Flash Welded Rings As ordered by the forging or flash welded ring manufacturer. SAE INTERNATIONAL AMS5771F Page 3 of 6 3.3 Solution Heat Treatment Bars, forgings, and flash welded rings shall be solution heat treated by heating to 2150 F 25 (1177 C 14), holding at heat for a time commensurate with
18、 section thickness but not less than 20 minutes, and cooling at a rate equivalent to an air cool or faster. Pyrometry shall be in accordance with AMS2750. 3.4 Properties The product shall conform to the following requirements: 3.4.1 Bars, Forgings, and Flash Welded Rings 3.4.1.1 Hardness Shall be no
19、t higher than 255 HB, or equivalent (See 8.2), determined in accordance with ASTM E 10. 3.4.1.2 Stress-Rupture Properties at 1500 F (816 C) A tensile specimen, maintained at 1500 F 3 (816 C 2) while a load sufficient to produce an initial axial stress of 13.5 ksi (93 MPa) or higher is applied contin
- 1.请仔细阅读文档,确保文档完整性,对于不预览、不比对内容而直接下载带来的问题本站不予受理。
- 2.下载的文档,不会出现我们的网址水印。
- 3、该文档所得收入(下载+内容+预览)归上传者、原创作者;如果您是本文档原作者,请点此认领!既往收益都归您。
下载文档到电脑,查找使用更方便
10000 积分 0人已下载
下载 | 加入VIP,交流精品资源 |
- 配套讲稿:
如PPT文件的首页显示word图标,表示该PPT已包含配套word讲稿。双击word图标可打开word文档。
- 特殊限制:
部分文档作品中含有的国旗、国徽等图片,仅作为作品整体效果示例展示,禁止商用。设计者仅对作品中独创性部分享有著作权。
- 关 键 词:
- SAEAMS5771F2009NICKELALLOYCORROSIONANDHEATRESISTANTBARSFORGINGSANDRINGS74NIC70CRC165MOSOLUTIONHEATTREATEDUNSN1000374NI70CR165MO

链接地址:http://www.mydoc123.com/p-1022175.html