SAE AMS 5402C-2004 Nickel Alloy Corrosion and Heat-Resistant Investment Castings 62Ni - 21 5Cr - 9 0Mo - 3 6Cb (Nb) As Cast (UNS N26010)《采用62Ni 21 5Cr 9 0Mo 3 6Cb (Nb) 铸造的熔模铸造法的耐腐蚀.pdf
《SAE AMS 5402C-2004 Nickel Alloy Corrosion and Heat-Resistant Investment Castings 62Ni - 21 5Cr - 9 0Mo - 3 6Cb (Nb) As Cast (UNS N26010)《采用62Ni 21 5Cr 9 0Mo 3 6Cb (Nb) 铸造的熔模铸造法的耐腐蚀.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 5402C-2004 Nickel Alloy Corrosion and Heat-Resistant Investment Castings 62Ni - 21 5Cr - 9 0Mo - 3 6Cb (Nb) As Cast (UNS N26010)《采用62Ni 21 5Cr 9 0Mo 3 6Cb (Nb) 铸造的熔模铸造法的耐腐蚀.pdf(12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 reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 2011 SAE International All rights reserved. No part of this publication m
3、ay 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: +1 724-776-4970 (outside U
4、SA) 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/AMS5402C AEROSPACE MATERIAL SPECIFICATION AMS 5402 REV. C Issued 1980-01 Revised 2004-05 Reaf
5、firmed 2011-10 Superseding AMS 5402B Nickel Alloy, Corrosion and Heat-Resistant, Investment Castings 62Ni - 21.5Cr - 9.0Mo - 3.6Cb (Nb) As Cast (Composition similar to UNS N26010) 1. SCOPE: 1.1 Form: This specification covers a corrosion and heat-resistant, air-melted, nickel alloy in the form of in
6、vestment castings. 1.2 Application: These castings have been used typically for structural parts requiring high strength up to 1200 F (649 C) and oxidation and corrosion resistance up to 1800 F (982 C), but usage is not limited to such applications (See 8.4). 1.3 Classification: Castings conforming
7、to this specification are classified as follows: Class 1 - Trace element limits conforming to AMS 2280, Class 1 (AMS 2280-1) Class 2 - Trace element limits conforming to AMS 2280, Class 2 (AMS 2280-2) Class 3 - Trace element limits do not apply 1.3.1 Castings shall conform to Class 3 unless Class 1
8、or Class 2 is specified by purchaser. 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 i
9、ssue 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. SAE AMS 5402C Page 2 of 12 2.1 SAE Publications: Available from SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001 or www.sae.
10、org. AMS 2175 Castings, Classification and Inspection of AMS 2269 Chemical Check Analysis Limits, Nickel, Nickel Alloys, and Cobalt Alloys AMS 2280 Trace Element Control, Nickel Alloy Castings AMS 2360 Room Temperature Tensile Properties of Castings AMS 2694 Repair Welding of Aerospace Castings AMS
11、2804 Identification, Castings 2.2 ASTM Publications: Available from ASTM, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959 or www.astm.org. ASTM E 8 Tension Testing of Metallic Materials ASTM E 8M Tension Testing of Metallic Materials (Metric) ASTM E 354 Chemical Analysis of Hi
12、gh-Temperature, Electrical, Magnetic, and Other Similar Iron, Nickel, and Cobalt Alloys ASTM E 1417 Liquid Penetrant Examination ASTM E 1742 Radiographic Examination 3. TECHNICAL REQUIREMENTS: 3.1 Composition: Shall conform to the percentages by weight shown in Table 1, determined by wet chemical me
13、thods in accordance with ASTM E 354, by spectrochemical methods, or by other analytical methods acceptable to purchaser (See 8.2.1 and 8.2.2). SAE AMS 5402C Page 3 of 12 TABLE 1 - Composition Element min max Carbon - 0.10 Manganese - 0.50 Silicon - 0.50 Phosphorus - 0.03 Sulfur - 0.04 Chromium 20.00
14、 23.00 Molybdenum 8.00 10.00 Columbium (Niobium)(3.1.1) 3.15 4.15 Cobalt - 1.00 Titanium (3.1.2) - 0.10 Tantalum (3.1.1, 3.1.3) - 0.15 Aluminum (3.1.2) - 0.10 Iron - 5.00 Copper - 0.30 Other Elements (3.1.3) - - Nickel remainder 3.1.1 Sum of columbium (niobium) plus tantalum shall not exceed 4.15% b
15、y weight. 3.1.2 Shall be present but not in excess of maximum content specified. 3.1.3 Determination not required for routine acceptance. 3.1.4 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
16、purchaser (See 8.2.3). 3.1.5 Trace Elements: Shall conform to AMS 2280-1 or AMS 2280-2, when specified by purchaser (See 1.3). 3.1.6 Check Analysis: Composition variations shall meet the applicable requirements of AMS 2269. 3.2 Melting Practice: Castings and specimens shall be poured at casting vend
17、ors 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 Revert (gates, sprues, risers, and rejected castings) may be used only in the preparation of master heats; revert shall not be remelted directly without refining for pouring of ca
18、stings. Melting of revert creates a new master heat. 3.2.2 Portions of two or more qualified master heats (See 3.4.2) may be melted together and poured into castings using a procedure authorized by purchaser (See 8.2.6). SAE AMS 5402C Page 4 of 12 3.2.3 If melts (See 8.2.4) are modified by replenish
19、ment (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 apply. 3.3 Condition: Castings shall be delivered in the as-cast condition. 3.
20、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 acceptable to purchaser. Control factors of 4.4.2.2 shall apply. 3.4.2 Each ma
21、ster heat shall be qualified by evaluation of chemical and tensile specimens. 3.4.2.1 If replenishments are made at remelt as in 3.2.3, frequency of sampling and testing used by the vendor for qualification to 3.4.2 shall be acceptable to purchaser. 3.4.2.2 The tensile tests of 3.4.2 are not require
22、d if these tests are conducted using integrally-cast specimens (4.3.3.2) or machined-from-casting (4.3.3.3). 3.4.3 Chemical Analysis Specimens: Shall be of any convenient size and shape. 3.4.4 Tensile Specimens: Shall be of standard proportions in accordance with ASTM E 8 or ASTM E 8M (See 8.3) with
23、 0.250-inch (6.35-mm) diameter at the reduced parallel gage section. 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 (6.35-mm) diameter. 3.4.4.2 When integrally-cast specimens or specimens machined-from-ca
24、sting are specified, specimen size and location shall be agreed upon by purchaser and vendor (See 8.2.9 and 8.6). 3.5 Heat Treatment: Not applicable. 3.6 Properties: Conformance shall be based upon testing of separately-cast specimens unless purchaser specifies integrally-cast specimens or specimens
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