SAE AMS 5810B-2008 Steel Corrosion and Heat Resistant Flat Wire 15Cr - 25 5Ni - 1 2Mo - 2 1Ti - 0 006B - 0 30V 1800 (982 Solution Treated Cold Drawn or Cold Rolled and Aged Consuma.pdf
《SAE AMS 5810B-2008 Steel Corrosion and Heat Resistant Flat Wire 15Cr - 25 5Ni - 1 2Mo - 2 1Ti - 0 006B - 0 30V 1800 (982 Solution Treated Cold Drawn or Cold Rolled and Aged Consuma.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 5810B-2008 Steel Corrosion and Heat Resistant Flat Wire 15Cr - 25 5Ni - 1 2Mo - 2 1Ti - 0 006B - 0 30V 1800 (982 Solution Treated Cold Drawn or Cold Rolled and Aged Consuma.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 2015 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/AMS5810B AEROSPACE MATERIAL SPECIFICATION AMS5810 REV. B Issued 1994-08 Revised 2
5、008-11 Reaffirmed 2015-12 Superseding AMS5810A Steel, Corrosion and Heat Resistant, Flat Wire 15Cr - 25.5Ni - 1.2Mo - 2.1Ti - 0.006B - 0.30V 1800 F (982 C) Solution Treated, Cold Drawn or Cold Rolled and Aged, Consumable Electrode Remelted (Composition similar to UNS S66286) RATIONALE AMS5810B has b
6、een reaffirmed to comply with the SAE five-year review policy. 1. SCOPE 1.1 Form This specification covers a corrosion and heat resistant steel in the form of flat wire. 1.2 Application This wire has been used typically for retaining rings requiring corrosion and heat resistance up to 900 F (482 C)
7、and which may require moderate to severe forming and bending, 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 wo
8、rk 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 shall apply. 2.1 SAE Publications Available from SAE International, 400 C
9、ommonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org. AMS2248 Chemical Check Analysis Limits, Corrosion and Heat-Resistant Steels and Alloys, Maraging and Other Highly-Alloyed Steels, and Iron Alloys AMS2371 Quality Assura
10、nce Sampling and Testing, Corrosion and Heat-Resistant Steels and Alloys, Wrought Products and Forging Stock AMS2750 Pyrometry 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 A 370
11、Mechanical Testing of Steel Products ASTM E 353 Chemical Analysis of Stainless, Heat-Resisting, Maraging, and Other Similar Chromium-Nickel-Iron Alloys 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the percentages by weight as shown in Table 1, determined by wet chemical methods in acco
12、rdance with ASTM E 353, by spectrochemical methods, or by other analytical methods acceptable to purchaser. TABLE 1 - COMPOSITION Element min max Carbon Manganese Silicon Phosphorus Sulfur Chromium Nickel Molybdenum Titanium Boron Vanadium Cobalt Aluminum Copper - - - - - 13.50 24.00 1.00 1.90 0.003
13、 0.10 - - - 0.08 2.00 1.00 0.025 0.025 16.00 27.00 1.50 2.30 0.010 0.50 1.00 0.35 0.50 3.1.1 Check Analysis Composition variations shall meet the applicable requirements of AMS2488. 3.2 Melting Practice Steel shall be produced by multiple melting using consumable electrode practice in the remelt cyc
14、le. 3.3 Condition Wire shall be solution heat treated, descaled if necessary, cold drawn or cold rolled to required size, and aged. 3.4 Heat Treatment 3.4.1 Heating Equipment Furnaces may be of any type. The heating medium or atmosphere shall be dry nitrogen or other atmospheres that will not alter
15、the surface composition. 3.4.2 Solution Heat Treatment Except as specified in 3.4.2.1, wire shall be solution heat treated by heating to 1800 F 25 (982 C 14), holding at heat for not less than one hour, and quenching in oil. Pyrometry shall conform to AMS2750. SAE INTERNATIONAL AMS5810B Page 2 of 6_
16、 3.4.2.1 Continuous Heat Treating: Process parameters (e.g., furnace temperature set points, heat input, travel rate, etc.) for continuous heat treating lines shall be established by the material producer and validated by testing of product to the other requirements of this specification. 3.4.3 Agin
17、g Heat Treatment Wire, cold drawn or cold rolled to required size, shall be aged by heating to a temperature within the range 1150 to 1325 F (621 to 718 C), holding at the selected temperature within 25 F (14 C) for 4 to 6 hours, and cooling at a rate equivalent to cooling in air. Pyrometry shall co
18、nform to AMS2750. 3.5 Properties After Aging Heat Treatment The product shall conform to the following requirements, determined in accordance with ASTM A 370: 3.5.1 Tensile Strength Shall be within the range 185 to 240 ksi (1276 to 1655 MPa). 3.5.1.1 The rectangular cross-section area of the wire sp
19、ecimen for the tensile test shall be determined from measurements of thickness and width taken prior to the tensile test. The area on which stress is based shall be determined as shown in Equation 1. 2)T(12.0TWA = (Eq. 1) where: A = area (for this test) of wire cross-section, inch2(mm2) T = thicknes
20、s of wire specimen, inch (mm) W = width of wire specimen, inch (mm) 3.5.2 Hardness Shall be as shown in Table 2, or equivalent (See 8.2), but the product shall not be rejected on the basis of hardness if the tensile properties of 3.5.1 are acceptable, determined on specimens taken from the same samp
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