SAE AMS 5922B-2015 Steel Corrosion-Resistant Bars and Forgings 10Cr - 5 5Ni - 14Co - 2Mo - 1W (0 19-0 23C) Vacuum Induction Melted Vacuum Arc Remelted Normalized Annealed (UNS S105.pdf
《SAE AMS 5922B-2015 Steel Corrosion-Resistant Bars and Forgings 10Cr - 5 5Ni - 14Co - 2Mo - 1W (0 19-0 23C) Vacuum Induction Melted Vacuum Arc Remelted Normalized Annealed (UNS S105.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 5922B-2015 Steel Corrosion-Resistant Bars and Forgings 10Cr - 5 5Ni - 14Co - 2Mo - 1W (0 19-0 23C) Vacuum Induction Melted Vacuum Arc Remelted Normalized Annealed (UNS S105.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 theref
2、rom, 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 InternationalAll rights reserved. No part of this publi
3、cation 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: +1 724-776-4970 (out
4、side USA)Fax: 724-776-0790Email: CustomerServicesae.orgSAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedbackon this Technical Report, please visithttp:/www.sae.org/technical/standards/AMS5922BAEROSPACEMATERIAL SPECIFICATIONAMS5922 REV. BIssued 2008-01Revised 2015-12Superseding
5、 AMS5922ASteel, Corrosion-Resistant, Bars, and Forgings 10Cr - 5.5Ni - 14Co - 2Mo - 1W (0.19-0.23C)Vacuum Induction Melted, Vacuum Arc Remelted, Normalized, Annealed(Composition similar to UNS S10500)RATIONALEAMS5922B revises heat treatment (3.4) macrostructure (3.5.1), Micro-inclusion rating (3.5.2
6、), response to heat treatment(3.5.3), average grain size (3.5.3.4), and Reports (4.4), and is a Five Year Review and update of this specification.1. SCOPE1.1 FormThis specification covers a corrosion-resistant, premium aircraft-quality alloy steel in the form of bars, forgings, and stock for forging
7、.1.2 ApplicationThese products have been used typically for heat treated parts requiring a combination of high strength, good toughness, weldability, and stress corrosion resistance, but usage is not limited to such applications. Product after heat treatment should attain a minimum tensile strength
8、of 280 ksi (1931 MPa).2. APPLICABLE DOCUMENTSThe 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 document unless a specific document issue is specified.
9、 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 PublicationsAvailable from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or
10、 +1 724-776-4970 (outside USA), www.sae.org.AMS2241 Tolerances, Corrosion and Heat-Resistant Steel, Iron Alloy, Titanium, and Titanium Alloy Bars and WireAMS2248 Chemical Check Analysis Limits, Corrosion and Heat-Resistant Steels and Alloys, Maraging and Other Highly-Alloyed Steels, and Iron AlloysA
11、MS2300 Steel Cleanliness, Premium Aircraft-Quality Magnetic Particle Inspection ProcedureSAE INTERNATIONAL AMS5922B Page 2 of 7AMS2315 Determination of Delta Ferrite ContentAMS2371 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steels and Alloys, Wrought Products and Forging St
12、ockAMS2374 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steel and Alloy ForgingsAMS2750 PyrometryAMS2806 Identification Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and Alloy Steels and Corrosion and Heat-Resistant Steels and AlloysAMS2808 Identification ForgingsAS11
13、82 Standard Stock Removal Allowance Aircraft-Quality and Premium Aircraft-Quality Steel Bars and Mechanical Tubing2.2 ASTM PublicationsAvailable from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org.ASTM A370 Definitions for
14、Mechanical Testing of Steel ProductsASTM A604 Macroetch Testing of Consumable Electrode Remelted Steel Bars and BilletsASTM E45 Determining the Inclusion Content of SteelASTM E353 Chemical Analysis of Stainless, Heat-Resisting, Maraging, and Other Similar Chromium-Nickel-Iron AlloysASTM E399 Plane-S
15、train Fracture Toughness of Metallic MaterialsASTM E1181 Characterizing Duplex Grain Sizes3. TECHNICAL REQUIREMENTS3.1 CompositionShall conform to the percentages by weight shown in Table 1, determined by wet chemical methods in accordance with ASTM E353, by spectrochemical methods, or by other anal
16、ytical methods acceptable to purchaser.Table 1 - CompositionElement min maxCarbon 0.19 0.23Manganese - 0.10Silicon - 0.10Phosphorus - 0.008Sulfur - 0.005Chromium 9.50 10.50Nickel 5.20 5.80Cobalt 13.50 14.50Molybdenum 1.80 2.20Tungsten 0.80 1.20Titanium - 0.015Aluminum - 0.01Vanadium 0.25 0.35Oxygen
17、- 0.0020 (20 ppm)Nitrogen - 0.0015 (15 ppm)SAE INTERNATIONAL AMS5922B Page 3 of 73.1.1 Check AnalysisComposition variations shall meet the applicable requirements of AMS2248. No variation is permitted for oxygen and nitrogen.3.2 Melting PracticeSteel shall be multiple melted using vacuum induction m
18、elting followed by vacuum arc remelting.3.3 ConditionThe product shall be supplied in the following condition; hardness shall be determined in accordance with ASTM A370:3.3.1 Bars and ForgingsNormalized and annealed having hardness not higher than 372 HB, or equivalent (see 8.2), and descaled.3.3.2
19、Stock for ForgingAs ordered by the forging manufacturer.3.4 Heat TreatmentBars and forgings shall be normalized by heating to 1976 F 36 F (1080 C 20 C), holding at the selected temperature for a time commensurate with section thickness, 60 minutes minimum, cooling in air to room temperature, cooling
20、 to -100 F (-73 C) or lower, holding at temperature for a minimum of 60 minutes, and air warming to room temperature, and annealed by heating to 1256 F 25 F (680 C 14 C), holding at temperature for 8 hours +2 hours, -0.5 hour, and cooling in air.Pyrometry shall be in accordance with AMS2750.3.5 Prop
21、ertiesThe product shall conform to the following requirements; tensile and hardness testing shall be performed in accordance with ASTM A370:3.5.1 MacrostructureVisual examination of transverse full cross-sections from bars, billets, and stock for forging, flash welded rings, or extrusions, etched in
22、 hot hydrochloric acid in accordance with ASTM A604, shall show no pipe or cracks. Porosity, segregation, inclusions, and other imperfections shall be no worse than the macrographs of ASTM A604 shown in Table 2.Table 2 - Macrostructure limitsClass Condition Severity1Freckles A2 White Spots A3 Radial
23、 Segregation B4 Ring Pattern B3.5.2 Micro-Inclusion RatingNo specimen shall exceed the limits shown in Table 3, determined in accordance with ASTM E45, Method D.SAE INTERNATIONAL AMS5922B Page 4 of 7Table 3 Micro-inclusion rating limitsAThinAHeavyBThinBHeavyCThinCHeavyDThinDHeavyWorst Field Severity
24、 1.5 1.0 1.5 1.0 1.5 1.0 1.5 1.0Worst Field Frequency, maximum (a) 1 (a) 1 (a) 1 3 1Total Rateable Fields, Frequency, maximum (b) 1 (b) 1 (b) 1 8 1(a) Combined A+B+C; not more than 3 fields(b) Combined A+B+C; not more than 8 fields3.5.2.1 A rateable field is defined as one which has a type A, B, C,
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