SAE AMS 5698G-2003 Nickel Alloy Corrosion and Heat-Resistant Wire 72Ni - 15 5Cr - 0 95Cb - 2 5Ti - 0 70Al - 7 0Fe No 1 Temper Precipitation Hardenable (UNS N07750)《1号回火 脱溶淬硬的含72Ni-.pdf
《SAE AMS 5698G-2003 Nickel Alloy Corrosion and Heat-Resistant Wire 72Ni - 15 5Cr - 0 95Cb - 2 5Ti - 0 70Al - 7 0Fe No 1 Temper Precipitation Hardenable (UNS N07750)《1号回火 脱溶淬硬的含72Ni-.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 5698G-2003 Nickel Alloy Corrosion and Heat-Resistant Wire 72Ni - 15 5Cr - 0 95Cb - 2 5Ti - 0 70Al - 7 0Fe No 1 Temper Precipitation Hardenable (UNS N07750)《1号回火 脱溶淬硬的含72Ni-.pdf(7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/AMS5698G AEROSPACE MATERIAL SPECIFICATION AMS5698 REV. G Issued 1953-06 Revised 2
5、003-01 Reaffirmed 2013-12 Superseding AMS5698F Nickel Alloy, Corrosion and Heat-Resistant, Wire 72Ni - 15.5Cr - 0.95Cb - 2.5Ti - 0.70Al - 7.0Fe No. 1 Temper, Precipitation Hardenable (Composition similar to UNS N07750) RATIONALE AMS5698G has been reaffirmed to comply with the SAE five-year review po
6、licy. 1. SCOPE:1.1 Form: This specification covers a corrosion and heat-resistant nickel alloy in the form of round, square, and flat wire 0.500 inch (12.70 mm) and under in nominal diameter or thickness.1.2 Application: This wire has been used typically for helical springs requiring optimum resista
7、nce to relaxation up to 1000 F (538 C) with moderate or relatively low stresses, 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.
8、The supplier may work 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,
9、400 Commonwealth Drive, Warrendale, PA 15096-0001 or www.sae.org.AMS 2269 Chemical Check Analysis Limits, Nickel, Nickel Alloys and Cobalt AlloysAMS 2371 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steels and Alloys, Wrought Products and Forging StockSAE INTERNATIONAL AMS569
10、8G Page 2 of 7 2.2 ASTM Publications: Available from ASTM, 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959 orwww.astm.org.ASTM E 8 Tension Testing of Metallic MaterialsASTM E 8M Tension Testing of Metallic Materials (Metric)ASTM E 354 Chemical Analysis of High-Temperature, Electrical, Magnet
11、ic, and Other Similar Iron, Nickel, and Cobalt Alloys3. 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 E 354, by spectrochemical methods, or by other analytical methods acceptable to pur
12、chaser.3.1.1 Check Analysis: Composition variations shall meet the applicable requirements of AMS 2269.3.2 Condition: Cold drawn from hot finished wire or rod which has had suitable surface preparation for removal of scale, seams, and other injurious surface imperfections. Wire shall be solution hea
13、t treated by heating within the range 2000 to 2200 F (1093 to 1204 C) before reducing to the size ordered.3.2.1 Wire in the size range 0.025 to 0.500 inch (0.64 to 12.70 mm) in nominal diameter or thickness shall be cold reduced approximately 15% following solution heat treatment.3.2.2 All traces of
14、 lubricant shall be removed after cold reduction.TABLE 1 - CompositionElement min maxCarbonManganeseSiliconSulfurChromiumNickelColumbiumTitaniumAluminumIronCobaltTantalumCopper-14.0070.000.702.250.405.00-0.08 1.00 0.50 0.01017.00 -1.20 2.75 1.00 9.00 1.00 0.05 0.50 SAE INTERNATIONAL AMS5698G Page 3
15、of 7 3.3 Properties: Wire shall conform to the following requirements; tensile testing shall be performed in accordance with ASTM E 8 or ASTM E 8M:3.3.1 As Received: 3.3.1.1 Tensile Properties: Shall be as shown in Table 2.3.3.1.2 Wrapping: Wire shall withstand, without cracking, wrapping at room te
16、mperature five full, closely-spaced turns around a diameter as shown in Table 3.3.3.2 After Precipitation Heat Treatment: Wire shall have tensile properties as shown in Table 4 after being precipitation heat treated by heating to 1350 F 25 (732 C 14), holding at heat for 16 hours 0.5, and cooling at
17、 a rate equivalent to air cooling.TABLE 2A - Tensile Strength, Inch/Pound UnitsNominalDiameter or ThicknessInchTensileStrengthksi, minTensileStrengthksi, maxUp to 0.025, inclOver 0.025 to 0.500, incl-130150165TABLE 2B - Tensile Strength, SI UnitsNominalDiameter or ThicknessMillimetersTensileStrength
18、MPa, minTensileStrengthMPa, maxUp to 0.64, inclOver 0.64 to 12.70, incl-89610341138TABLE 3 - Wrapping ParametersWire Shape Wrapping DiameterRound SquareFlat Nominal diameter of wireNominal diagonal of wireNominal width of wire TABLE 4A - Minimum Tensile Strength, Inch/Pound UnitsNominalDiameter or T
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