SAE AMS 5655E-2001 Steel Corrosion and Heat Resistant Bars Wire and Forgings 12 5Cr - 0 75Ni - 1 0Mo - 1 0W - 0 24V (0 20-0 25C) Hardened and Tempered (UNS S42200)《调质的含12 5Cr-0 75N.pdf
《SAE AMS 5655E-2001 Steel Corrosion and Heat Resistant Bars Wire and Forgings 12 5Cr - 0 75Ni - 1 0Mo - 1 0W - 0 24V (0 20-0 25C) Hardened and Tempered (UNS S42200)《调质的含12 5Cr-0 75N.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 5655E-2001 Steel Corrosion and Heat Resistant Bars Wire and Forgings 12 5Cr - 0 75Ni - 1 0Mo - 1 0W - 0 24V (0 20-0 25C) Hardened and Tempered (UNS S42200)《调质的含12 5Cr-0 75N.pdf(8页珍藏版)》请在麦多课文档分享上搜索。
1、AEROSPACE MATERIAL SPECIFICATIONAMS 5655ESuperseding AMS 5655DSteel, Corrosion and Heat Resistant, Bars, Wire, and Forgings12.5Cr - 0.75Ni - 1.0Mo - 1.0W - 0.24V (0.20-0.25C)Hardened and Tempered(Composition similar to UNS S42200)1. SCOPE:1.1 Form: This specification covers a corrosion and heat resi
2、stant steel in the form of bars, wire, forgings, and forging stock. 1.2 Application: These products have been used typically for parts requiring strength and oxidation resistance up to 1000 F (538 C), but usage is not limited to such applications.2. APPLICABLE DOCUMENTS: The issue of the following d
3、ocuments 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 issue is specified. When the referenced document has been canceled and no superseding docume
4、nt has been specified, the last published issue of that document shall apply.2.1 SAE Publications: Available from SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001 or www.sae.org.AMS 2241 Tolerances, Corrosion and Heat Resistant Steel, Iron Alloy, Titanium, and Titanium Alloy Bars and WireMAM 2
5、241 Tolerances, Metric, Corrosion and Heat Resistant Steel, Iron Alloy, Titanium, and Titanium Alloy Bars and WireRATIONALE This document has been reaffirmed to comply with the SAE 5-year Review policy. Issued 1959-01 Revised 2001-11Reaffirmed 2010-10 SAE Technical Standards Board Rules provide that
6、: “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 therefrom, is the sole responsibility of the user.” SAE
7、 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 2010 SAE International All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or
8、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 USA) Fax: 724-776-0790 Email: CustomerServicesae.or
9、g 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/AMS5655E Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without licens
10、e from IHS-,-,-AMS 5655E SAE AMS 5655E- 2 -2.1 (Continued):AMS 2374 Quality Assurance Sampling and Testing, Corrosion and Heat Resistant Steel and Alloy ForgingsAMS 2750 PyrometryAMS 2806 Identification, Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and Alloy Steels and Corrosion and Heat Re
11、sistant Steels and AlloysAMS 2808 Identification, ForgingsAS1182 Standard Machining Allowance, Aircraft-Quality and Premium Aircraft-Quality Steel Bars and Mechanical Tubing2.2 ASTM Publications: Available from ASTM, 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959 or www.astm.org.ASTM A 370
12、Mechanical Testing of Steel ProductsASTM E 353 Chemical Analysis of Stainless, Heat-Resisting, Maraging, and Other Similar Chromium-Nickel-Iron AlloysASTM E 381 Macroetch Testing, Steel Bars, Billets, Blooms, and Forgings3. TECHNICAL REQUIREMENTS: 3.1 Composition:Shall conform to the percentages by
13、weight shown in Table 1, determined by wet chemical methods in accordance with ASTM E 353, by spectrochemical methods, or by other analytical methods acceptable to purchaser.TABLE 1 - CompositionElement min maxCarbonManganeseSiliconPhosphorusSulfurChromiumNickelMolybdenumTungstenVanadiumCopper0.20-0
14、.20-11.000.500.750.750.17-0.251.000.600.0400.03013.501.001.251.250.300.50AMS 2248 Chemical Check Analysis Limits, Corrosion and Heat Resistant Steels and Alloys, Maraging and Other Highly-Alloyed Steels, and Iron AlloysAMS 2371 Quality Assurance Sampling and Testing, Corrosion and Heat Resistant Ste
15、els and Alloys, Wrought Products and Forging StockCopyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AMS 5655E SAE AMS 5655E- 3 -3.2 Condition:The product shall be supplied in the following condition:3.
16、2.1 Bars and Wire: Hardened and tempered. Bars 2.750 inches (69.85 mm) and under in nominal diameter or least distance between parallel sides and wire shall be cold finished. Larger bars shall be hot finished.3.2.2 Forgings: Hardened, tempered, and descaled.3.2.3 Forging Stock: As ordered by the for
17、ging manufacturer.3.3 Heat Treatment: Bars, wire, and forgings shall be hardened by heating to 1925 F 25 (1052C 14), holding at heat for not less than one hour, and suitably quenching, and tempered by heating to a temperature not lower than 1100 F (593 C), holding at heat for not less than four hour
18、s, cooling in air, reheating to a temperature not lower than 1000 F (538 C), holding at heat for not less than four hours, and cooling in air. Pyrometry shall be in accordance with AMS 2750.3.4 Properties:The product shall conform to the following requirements; hardness, tensile, and impact testing
19、shall be performed in accordance with ASTM A 370:3.4.1 Macrostructure: Visual examination of transverse full cross-sections from bars, billets, and forging stock, etched in accordance with ASTM E 381, shall show no pipe or cracks. When specified, porosity, segregation, inclusions, and other imperfec
20、tions shall be no worse than the macrographs of ASTM E 381 agreed upon by purchaser and vendor.3.4.2 Bars, Wire, and Forgings: 3.4.2.1 Tensile Properties: Shall be as shown in Table 2.3.4.2.2 Hardness: Shall be 293 to 341 HB, or equivalent (See 8.2).TABLE 2 - Minimum Tensile PropertiesProperty Value
21、Tensile StrengthYield Strength at 0.2% OffsetElongation in 4DReduction of Area140 ksi (965 MPa)115 ksi (793 MPa)13%25%3.1.1 Check Analysis: Composition variations shall meet the applicable requirements of AMS 2248.Copyright SAE International Provided by IHS under license with SAENot for ResaleNo rep
22、roduction or networking permitted without license from IHS-,-,-AMS 5655E SAE AMS 5655E- 4 -3.4.2.3 Charpy Impact Strength (Notch Sensitivity): Shall be not lower than 10 foot-pounds (13.5J), determined at room temperature using a V-notched Charpy specimen.3.4.2.4 Decarburization:3.4.2.4.1 Bars and w
23、ire ordered ground, turned, or polished shall be free from decarburization on the ground, turned, or polished surfaces.3.4.2.4.2 Allowable decarburization of bars, wire, and billets ordered for forging or to specified microstructural requirements shall be as agreed upon by purchaser and vendor.3.4.2
24、.4.3 Decarburization of bars and wire to which 3.4.2.4.1 or 3.4.2.4.2 is not applicable shall be not greater than shown in Table 3.TABLE 3A - Maximum Decarburization, Inch/Pound UnitsNominal Diameter or DistanceBetween Parallel SidesInchesTotal Depth ofDecarbrizationInchUp to 0.500, inclOver 0.500 t
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