SAE AMS 5866E-2016 Steel Corrosion-Resistant Flat Wire 18Cr - 9 0Ni (302) Spring Temper (UNS S30200).pdf
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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 2016 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/AMS5866E AEROSPACE MATERIAL SPECIFICATION AMS5866 REV. E Issued 1989-07 Reaffirme
5、d 2012-04 Revised 2016-06Superseding AMS5866D Steel, Corrosion-Resistant, Flat Wire 18Cr - 9.0Ni (302) Spring Temper (Composition similar to UNS S30200)RATIONALE AMS5866E introduces a new class of product to cover square-edged wire (1.3), and revises Properties (3.3.1, Tables 2, 3), Dimensions and T
6、olerances (3.5.1.2), and Reports (4.4). 1. SCOPE 1.1 Form This specification covers a corrosion-resistant steel in the form of flat wire 0.005 to 0.095 inch (0.13 to 2.41 mm) thick, inclusive (see 8.6). 1.2 Application This wire has been used typically for retaining rings requiring corrosion and hea
7、t-resistance up to 400 F (204 C) and which require moderate to severe forming and bending, but usage is not limited to such applications. 1.3 Classification Wire covered by this specification is classified by edge configuration as follows: Type 1 Round edged wire Type 2 Square edged wire. 1.3.1 Type
8、 1 shall be supplied unless Type 2 is specified by purchaser (see 8.6). 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 docu
9、ment 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. SAE INTERNATIONAL AMS5866E Page 2 of 7 2.1 SAE Publications Available from SAE International, 400
10、 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or +1 724-776-4970 (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 A
11、ssurance Sampling and Testing, Corrosion and Heat-Resistant Steels and Alloys, Wrought Products and Forging Stock ARP1917 Clarification of Terms Used in Aerospace Metals Specifications 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, P
12、A 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM A370 Mechanical Testing of Steel Products ASTM E140 Hardness Conversion Tables for Metals Relationship Among Brinell Hardness, Vickers Hardness, Rockwell Hardness, Superficial Hardness, Knoop Hardness, Scleroscope Hardness, and Leeb Hardness ASTM E
13、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 shown in Table 1, determined by wet chemical methods in accordance with ASTM E353, by spectrochemical metho
14、ds, or by other analytical methods acceptable to purchaser. Table 1 - Composition Element min max Carbon Manganese Silicon Phosphorus Sulfur Chromium Nickel Molybdenum Copper - - - - - 17.00 8.00 - - 0.15 2.00 1.00 0.040 0.030 19.00 10.00 0.75 0.75 SAE INTERNATIONAL AMS5866E Page 3 of 7 3.1.1 Check
15、Analysis Composition variations shall meet the applicable requirements of AMS2248. 3.2 Condition Spring temper; cold drawn or rolled, descaled, and rerolled to required size. 3.3 Properties Wire shall conform to the following requirements, determined in accordance with ASTM A370: 3.3.1 Tensile Prope
16、rties Square wire, and rectangular wire having nominal width not greater than ten times the nominal thickness, shall have tensile properties as shown in Table 2. Table 2A - Tensile properties, inch/pound units (see 8.3) Nominal Thickness Inch Tensile Strength ksi Elongation in 2 Inches %, min 0.005
17、to 0.022, incl Over 0.022 to 0.047, incl Over 0.047 to 0.062, incl Over 0.062 to 0.074, incl Over 0.074 to 0.089, incl Over 0.089 to 0.095, incl 210 to 250 200 to 240 185 to 235 175 to 225 165 to 215 155 to 205 - 3 3 3 3 3 Table 2B - Tensile properties, SI units (see 8.3) Nominal Thickness Millimete
18、rs Tensile Strength MPa Elongation in 50.8 mm % min 0.13 to 0.56, incl Over 0.56 to 1.19, incl Over 1.19 to 1.57, incl Over 1.57 to 1.88, incl Over 1.88 to 2.26, incl Over 2.26 to 2.41, incl 1448 to 1724 1379 to 1655 1276 to 1620 1207 to 1551 1138 to 1482 1069 to 1413 - 3 3 3 3 3 The cross-sectional
19、 area of round edged wire (Type 1) shall be determined from measurements of thickness and width taken prior to the tensile test. The area on which stress is based, adjusted for rounded edges, shall be determined as shown in Equation 1. A T W u 0.12 T 2 = (Eq. 1)where: A = area (for this test) or wir
20、e cross-section, square inches, (mm2) T = thickness of wire specimen, inch, (mm) W = width of wire specimen, inch, (mm). SAE INTERNATIONAL AMS5866E Page 4 of 7 3.3.2 Hardness Shall be as shown in Table 3, or equivalent (see 8.2). Product shall not be rejected on the basis of hardness if the tensile
21、properties of 3.3.1 are acceptable, determined on specimens taken from the same sample as that with nonconforming hardness or from another sample with similar nonconforming hardness. Table 3 - Hardness Nominal Thickness Inch Nominal Thickness Millimeters Hardness 0.005 to 0.015, incl Over 0.015 to 0
22、.022, incl Over 0.022 to 0.047, incl Over 0.047 to 0.062, incl Over 0.062 to 0.074, incl Over 0.074 to 0.089, incl Over 0.089 to 0.095, incl 0.13 to 0.38, incl Over 0.38 to 0.56, incl Over 0.56 to 1.19, incl Over 1.19 to 1.57, incl Over 1.57 to 1.88, incl Over 1.88 to 2.26, incl Over 2.26 to 2.41, i
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