SAE AMS 5376G-2002 Alloy Corrosion and Heat Resistant Investment Castings 30Fe - 21Cr - 20Ni - 20Co - 3 0Mo - 2 5W - 1 0Cb - 0 15N As Cast (UNS R30155)《UNS R30155实型铸造的30Fe-21Cr-20N.pdf
《SAE AMS 5376G-2002 Alloy Corrosion and Heat Resistant Investment Castings 30Fe - 21Cr - 20Ni - 20Co - 3 0Mo - 2 5W - 1 0Cb - 0 15N As Cast (UNS R30155)《UNS R30155实型铸造的30Fe-21Cr-20N.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 5376G-2002 Alloy Corrosion and Heat Resistant Investment Castings 30Fe - 21Cr - 20Ni - 20Co - 3 0Mo - 2 5W - 1 0Cb - 0 15N As Cast (UNS R30155)《UNS R30155实型铸造的30Fe-21Cr-20N.pdf(11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/AMS5376G AEROSPACE MATERIAL SPECIFICATION AMS5376 REV. G Issued 1948-07 Revised 2
5、002-08 Reaffirmed 2013-08 Superseding AMS5376F Alloy, Corrosion and Heat Resistant, Investment Castings 30Fe - 21Cr - 20Ni - 20Co - 3.0Mo - 2.5W - 1.0Cb - 0.15N As Cast (Composition similar to UNS R30155) RATIONALE AMS5376G has been reaffirmed to comply with the SAE 5-year review policy. 1. SCOPE: 1
6、.1 Form: This specification covers a corrosion and heat resistant iron alloy in the form of investment castings. 1.2 Application: These castings been used typically for small parts, such as turbine blades and vanes, requiring high strength up to 1350 F (732 C) and oxidation resistance up to 1800 F (
7、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 specification to the extent specified herein. The supplier may work to a subsequent revision of a document unless a sp
8、ecific document 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. SAE INTERNATIONAL AMS5376G Page 2 of 11 2.1 SAE Publications: Available from SAE, 400 Commonwealth Drive, Warrenda
9、le, PA 15096-0001 or www.sae.org. AMS 2248 Chemical Check Analysis Limits, Corrosion and Heat-Resistant Steels and Alloys, Maraging and Other Highly-Alloyed Steels, and Iron Alloys AMS 2360 Room Temperature Tensile Properties of Castings AMS 2361 Elevated Temperature Tensile Properties of Castings A
10、MS 2694 Repair Welding of Aerospace Castings AMS 2804 Identification, Castings AMS-STD-2175 Castings, Classification and Inspection of 2.2 ASTM Publications: Available from ASTM, 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959 or www.astm.org. ASTM E 8 Tension Testing of Metallic Materials A
11、STM E 8M Tension Testing of Metallic Materials (Metric) ASTM E 18 Rockwell Hardness and Rockwell Superficial Hardness of Metallic Materials ASTM E 21 Elevated Temperature Tension Tests for Metallic Materials ASTM E 354 Chemical Analysis of High-Temperature, Electrical, Magnetic, and Other Similar Ir
12、on, Nickel, and Cobalt Alloys ASTM E 1417 Liquid Penetrant Examination ASTM E 1742 Radiographic Examination SAE INTERNATIONAL AMS5376G Page 3 of 11 3. TECHNICAL REQUIREMENTS: 3.1 Composition: Castings shall conform to the percentages by weight shown in Table 1, determined by wet chemical methods in
13、accordance with ASTM E 354, by spectrochemical methods, or by other analytical methods acceptable to purchaser (See 8.2.1 and 8.2.2). TABLE 1 COMPOSITION Element min max Carbon - 0.20 Manganese 1.00 2.00 Silicon - 1.00 Phosphorus - 0.04 Sulfur - 0.03 Chromium 20.00 22.50 Nickel 19.00 21.00 Cobalt 18
14、.50 21.00 Molybdenum 2.50 3.50 Tungsten 2.00 3.00 Columbium 0.75 1.25 Nitrogen 0.10 0.20 Tantalum - 0.05 Iron remainder 3.1.1 Vendor may test for any element not 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
15、 Check Analysis: Composition variations shall meet the applicable requirements of AMS 2248. 3.2 Melting Practice: Castings and specimens shall be poured at the casting vendors facility either from a melt (See 8.2.4) of a master heat or directly from a master heat (See 8.2.5). 3.2.1 Revert (gates, sp
16、rues, 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 castings. 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 togeth
17、er and poured into castings using a procedure authorized by purchaser (See 8.2.6). 3.2.3 If modifications, such as alloy additions or replenishments, are made by the vendor at remelt, vendor shall have a written procedure acceptable to purchaser which defines the controls, test, and traceability cri
18、teria for both castings and separately-cast specimens. Control factors of 4.4.2.2 shall apply. SAE INTERNATIONAL AMS5376G Page 4 of 11 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 8.2.7), or m
19、achined 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 master heat shall be qualified by evaluation of chemical, hardness, and tensile specimens. 3.4.2
20、.1 If alloy additions or replenishments are made at remelt as in 3.2.3, the frequency of sampling and testing used by the vendor for qualification to 3.4.2 shall be acceptable to purchaser. 3.4.2.2 Tensile tests of 3.4.2 are not required if these tests are conducted using integrally-cast specimens (
21、4.3.3.2) or specimens machined from a 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 0.250-inch (6.35-mm) diameter at the reduced parall
22、el gage section. 3.4.4.1 Separately-cast and integrally-cast specimens may be either cast to size 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 a casting are specified, specimen size and location shall b
23、e agreed upon by purchaser and vendor (See 8.2.8 and 8.5). 3.4.5 Hardness Specimens for Response to Heat Treatment: May be a representative specimen or a casting. 3.5 Response to Heat Treatment: Casting shall have hardness not higher than 28 HRC after being heated to 1475 F 10 (802 C 6), held at hea
24、t for 50 hours 1, and cooled to room temperature. 3.6 Properties: Conformance shall be based upon testing of separately-cast specimens unless purchaser specifies integrally-cast specimens or specimens machined from a casting. Properties for integrally-cast specimens and specimens machined from a cas
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