SAE AMS 5391H-2014 Nickel Alloy Corrosion and Heat-Resistant Investment Castings 73Ni - 0 14C - 13Cr - 4 5Mo - 2 3Cb (Nb) - 0 75Ti - 6 0Al - 0 010B - 0 10Zr Vacuum Cast As-Cast (UN.pdf
《SAE AMS 5391H-2014 Nickel Alloy Corrosion and Heat-Resistant Investment Castings 73Ni - 0 14C - 13Cr - 4 5Mo - 2 3Cb (Nb) - 0 75Ti - 6 0Al - 0 010B - 0 10Zr Vacuum Cast As-Cast (UN.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 5391H-2014 Nickel Alloy Corrosion and Heat-Resistant Investment Castings 73Ni - 0 14C - 13Cr - 4 5Mo - 2 3Cb (Nb) - 0 75Ti - 6 0Al - 0 010B - 0 10Zr Vacuum Cast As-Cast (UN.pdf(9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/AMS5391H AEROSPACE MATERIAL SPECIFICATION AMS5391 REV. H Issued 1960-06 Revised 2
5、014-04 Superseding AMS5391G Nickel Alloy, Corrosion and Heat-Resistant, Investment Castings 73Ni - 0.14C - 13Cr - 4.5Mo - 2.3Cb (Nb) - 0.75Ti - 6.0Al - 0.010B - 0.10Zr Vacuum Cast, As-Cast (Composition similar to UNS N07713) RATIONALE AMS5391H corrects an error in the reports paragraph (4.5). 1. SCO
6、PE 1.1 Form This specification covers a corrosion and heat-resistant nickel alloy in the form of investment castings. 1.2 Application These castings have been used typically for parts, such as turbine blade, requiring high strength up to 1800 F (982 C) and oxidation resistance up to 2000 F (1093 C),
7、 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 specification to the extent specified herein. The supplier may work to a subsequent revision of a document unless a specific d
8、ocument issue is specified. When the referenced document has been canceled 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: 877-606-732
9、3 (inside USA and Canada) or 724-776-4970 (outside USA), www.ams.org. AMS2175 Castings, Classification and Inspection of AMS2269 Chemical Check Analysis Limits, Nickel, Nickel Alloys, and Cobalt Alloys AMS2360 Room Temperature Tensile Properties of Castings AMS2362 Stress-Rupture Properties of Casti
10、ngs SAE INTERNATIONAL AMS5391H Page 2 of 9 AMS2694 In-Process Welding of Castings AMS2804 Identification, Castings 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/E 8M Tension T
11、esting of Metallic Materials 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 ASTM E 1417/E 1417M Liquid Penetrant Examination ASTM E 17
12、42/E 1742M Radiographic Examination 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 E 354, by spectrochemical methods, or by other analytical methods acceptable to purchaser (See 8.2.1 a
13、nd 8.2.2). TABLE 1 COMPOSITION Element min max Carbon 0.08 0.20 Manganese - 0.25 Silicon - 0.50 Phosphorus - 0.015 Sulfur - 0.015 Chromium 12.00 14.00 Molybdenum 3.80 5.20 Columbium (Niobium) 1.80 2.80 Titanium 0.50 1.00 Aluminum 5.50 6.50 Boron 0.005 0.015 Zirconium 0.05 0.15 Cobalt - 1.00 Tantalum
14、 - 0.15 Iron - 0.50 Copper - 0.50 Other Elements (3.1.1) - - Nickel remainder 3.1.1 Vendor may test for any element not otherwise listed in Table 1 and include this analysis in the report of 4.5. Limits of acceptability may be specified by purchaser (See 8.2.3). 3.1.2 Check Analysis Composition vari
15、ations shall meet the requirements of AMS2269. SAE INTERNATIONAL AMS5391H Page 3 of 9 3.2 Melting Practice Castings and specimens shall be poured at casting vendors facility either from a melt (See 8.2.4) of a master heat, or directly from a master heat (See 3.4.2 and 8.2.5). 3.2.1 The metal for cas
16、tings and specimens shall be melted and poured under vacuum without loss of vacuum between melting and pouring. When authorized by purchaser (See 8.2.6), protective atmosphere may be used in lieu of vacuum for pouring of castings. 3.2.2 Revert (gates, sprues, risers, and rejected castings) may be us
17、ed only in the preparation of master heats; revert shall not be remelted directly without refining for pouring of castings. Melting of revert creates a new master heat. 3.2.3 Portions of two or more qualified master heats (See 3.4.2) may be melted together and poured into castings using a procedure
18、authorized by purchaser. 3.2.4 If melts (See 8.2.4) are modified by replenishment (See 8.2.7), vendor shall have a written procedure acceptable to purchaser which defines the controls, test, and traceability criteria for both castings and separately-cast specimens. Control factors of 4.4.2.2 shall a
19、pply. 3.3 Condition Castings shall be delivered in the as-cast condition. 3.4 Test Specimens Specimens shall be either separately-cast, integrally-cast (See 8.2.8), or machined from a casting, and shall conform to 3.2. 3.4.1 If specimens are separately-cast, vendor shall have a written procedure acc
20、eptable to purchaser. Control factors of 4.4.2.2 shall apply. 3.4.2 Each master heat shall be qualified by evaluation of chemical, tensile, and stress-rupture specimens. 3.4.2.1 If replenishments are made at remelt as in 3.2.4, frequency of sampling and testing used by the vendor for qualification t
21、o 3.4.2 shall be acceptable to purchaser. 3.4.2.2 Tensile and stress-rupture tests of 3.4.2 are not required if these tests are conducted using integrally-cast specimens (4.3.3.2) or specimens machined-from-casting (4.3.3.3). 3.4.3 Chemical Analysis Specimens Shall be of any convenient size and shap
22、e. 3.4.4 Tensile and Stress-Rupture Specimens Shall be of standard proportions in accordance with ASTM E 8/E 8M (See 8.3), and ASTM E 139, respectively. 3.4.4.1 Separately-cast and integrally-cast specimens may be either cast to size, and/or cast oversize and subsequently machined to 0.250-inch (6.3
23、5-mm) diameter. 3.4.4.2 When integrally-cast specimens and/or specimens machined-from-casting are specified, specimen size and location shall be agreed upon by purchaser and vendor (See 8.2.9 and 8.5). 3.5 Heat Treatment Not applicable. SAE INTERNATIONAL AMS5391H Page 4 of 9 3.6 Properties Conforman
24、ce shall be based upon testing of separately-cast specimens unless purchaser specifies integrally-cast specimens or specimens machined-from-casting. Properties for integrally-cast specimens and specimens machined-from-casting shall be as specified by purchaser (See 8.5). 3.6.1 Room Temperature Tensi
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