SAE AMS 5671G-2003 Nickel Alloy Corrosion and Heat-Resistant Bars Forgings and Rings 72Ni - 15 5Cr - 0 95Cb - 2 5Ti - 0 70Al - 7 0Fe Consumable Electrode or Vacuum Induction Melted.pdf
《SAE AMS 5671G-2003 Nickel Alloy Corrosion and Heat-Resistant Bars Forgings and Rings 72Ni - 15 5Cr - 0 95Cb - 2 5Ti - 0 70Al - 7 0Fe Consumable Electrode or Vacuum Induction Melted.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 5671G-2003 Nickel Alloy Corrosion and Heat-Resistant Bars Forgings and Rings 72Ni - 15 5Cr - 0 95Cb - 2 5Ti - 0 70Al - 7 0Fe Consumable Electrode or Vacuum Induction Melted.pdf(8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/AMS5671G AEROSPACE MATERIAL SPECIFICATION AMS5671 REV. G Issued 1965-09 Revised 2
5、003-01 Reaffirmed 2013-12 Superseding AMS5671F Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 72Ni - 15.5Cr - 0.95Cb - 2.5Ti - 0.70Al - 7.0Fe Consumable Electrode or Vacuum Induction Melted 1800 F (982 C) Solution Heat Treated, Precipitation Hardenable (Composition similar to
6、UNS N07750) RATIONALE AMS5671G has been reaffirmed to comply with the SAE five-year review policy. 1. SCOPE:1.1 Form: This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.1.2 Application:
7、These products have been used typically for parts requiring high strength at temperatures in the range 800 to 1100 F (427 to 593 C), particularly those parts which are formed or welded, but usage is not limited to such applications.2. APPLICABLE DOCUMENTS: The issue of the following documents in eff
8、ect 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 cancelled and no superseding document has been sp
9、ecified, 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 2261 Tolerances, Nickel, Nickel Alloy, and Cobalt Alloy Bars, Rods, and WireAMS 2269 Chemical Check Analysis Limits, Nickel, N
10、ickel Alloys, and Cobalt AlloysAMS 2371 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steels and Alloys, Wrought Products and Forging StockSAE INTERNATIONAL AMS5671G Page 2 of 8 2.1 (Continued):AMS 2374 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steel
11、 and Alloy ForgingsAMS 2750 PyrometryAMS 2806 Identification, Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and Alloy Steels, and Corrosion and Heat-Resistant Steels and AlloysAMS 2808 Identification, ForgingsAMS 7490 Rings, Flash Welded, Corrosion and Heat-Resistant Austenitic Steels and Au
12、stenitic-Type Alloys, or Precipitation Hardenable Alloys2.2 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 10 Brinell Hardness
13、of Metallic MaterialsASTM E 354 Chemical Analysis of High-Temperature, Electrical, Magnetic, 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
14、 ASTM E 354, by spectrochemical methods, or by other analytical methods acceptable to purchaser.TABLE 1 - CompositionElement min maxCarbonManganeseSiliconPhosphorusSulfurChromiumNickelColumbiumTitaniumAluminumIronCobaltTantalumCopper-14.0070.000.702.250.405.00-0.080.350.350.0150.01017.00-1.202.751.0
15、09.001.000.050.50SAE INTERNATIONAL AMS5671G Page 3 of 8 3.1.1 Check Analysis: Composition variations shall meet the applicable requirements of AMS 2269.3.2 Melting Practice: Alloy shall be multiple melted using consumable electrode practice in the remelt cycle or shall be induction melted under vacu
16、um. If consumable electrode remelting is not performed in vacuum, electrodes which have been produced by vacuum induction melting shall be used for remelting.3.3 Condition: The product shall be supplied in the following condition:3.3.1 Bars, Forgings, and Flash Welded Rings: Solution heat treated.3.
17、3.1.1 Bars shall be hot finished unless otherwise ordered; round bars shall be ground or turned.3.3.1.2 Forgings: Shall be descaled.3.3.1.3 Flash welded rings shall not be supplied unless specified or permitted on purchasers part drawing. When supplied, rings shall be manufactured in accordance with
18、 AMS 7490. During manufacture of flash welded rings, the stock shall not be heated to a temperature higher than 1825 F (996 C).3.3.2 Stock for Forging or Flash Welded Rings: As ordered by the forging or flash welded ring manufacturer.3.4 Heat Treatment: Bars, forgings, and flash welded rings shall b
19、e solution heat treated by heating to 1800 F 25 (982 C 14), holding at heat for a time commensurate with cross-sectional thickness, and cooling at a rate equivalent to an air cool or faster. Pyrometry shall be in accordance with AMS 2750.3.5 Properties: The product shall conform to the following req
20、uirements:3.5.1 Bars, Forgings, and Flash Welded Rings: 3.5.1.1 As Solution Heat Treated: 3.5.1.1.1 Hardness: Shall be as follows; determined in accordance with ASTM E 10:3.5.1.1.1.1 Bars: Not higher than 320 HB, or equivalent (See 8.2), determined approximately midway between outer surface and cent
21、er.3.5.1.1.1.2 Forgings and Flash Welded Rings: Not higher than 320 HB, or equivalent (See 8.2).SAE INTERNATIONAL AMS5671G Page 4 of 8 3.5.1.2 Response to Heat Treatment: The product shall have the following properties after being precipitation heat treated by heating to 1350 F 15 (732 C 8), holding
22、 at heat for 8 hours 0.25, cooling at a rate of 100 F 15 (56 C 8) degrees per hour to 1150 F 15 (621 C 8), holding at 1150 F 15 (621 C 8) for 8 hours 0.25, and air cooling. Instead of the 100 F (56 C) degrees per hour cooling rate to 1150 F 15 (621 C 8), product may be furnace cooled at any rate pro
23、vided the time at 1150 F 15 (621 C 8) is adjusted to give a total precipitation heat treatment time of 18 hours.3.5.1.2.1 Room Temperature Tensile Properties: Shall be as follows, determined in accordance with ASTM E 8 or ASTM E 8M.3.5.1.2.1.1 Shall be as shown in Table 2 for bars under 2.50 inches
24、(63.5 mm) in nominal diameter or thickness, for forgings under 2.50 inches (63.5 mm) in nominal thickness, and for flash welded rings under 2.50 inches (63.5 mm) in nominal radial thickness.3.5.1.2.1.2 Shall be as shown in Table 3 for bars 2.50 to 4.00 inches (63.5 to 101.6 mm), exclusive, in nomina
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