SAE AMS 5609D-1999 Steel Corrosion and Heat Resistant Bars Wire Forgings Tubing and Rings 12Cr - 0 12Cb (SAE 51410 Modified) Ferrite Controlled Annealed (UNS S41040)《UNS S41040 含12.pdf
《SAE AMS 5609D-1999 Steel Corrosion and Heat Resistant Bars Wire Forgings Tubing and Rings 12Cr - 0 12Cb (SAE 51410 Modified) Ferrite Controlled Annealed (UNS S41040)《UNS S41040 含12.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 5609D-1999 Steel Corrosion and Heat Resistant Bars Wire Forgings Tubing and Rings 12Cr - 0 12Cb (SAE 51410 Modified) Ferrite Controlled Annealed (UNS S41040)《UNS S41040 含12.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 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 2013 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/AMS5609DAEROSPACE MATERIAL SPECIFICATIONAMS5609 REV. DIssued 1964-01Revised 1999-10Reaffirmed
5、 2013-08Superseding AMS5609CSteel, Corrosion and Heat Resistant, Bars, Wire,Forgings, Tubing, and Rings12Cr - 0.12Cb (SAE 51410 Modified)Ferrite Controlled, Annealed(Composition similar to UNS S41040)RATIONALEAMS5609D has been reaffirmed to comply with the SAE 5-year Review policy.1. SCOPE1.1 FormTh
6、is specification covers an aircraft-quality, corrosion and heat resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings, and stock for forging or flash welded rings.1.2 ApplicationThese products have been used typically for parts requiring a combination of high roo
7、m temperature tensile properties with oxidation resistance up to 1000 F (538 C) and where control of ferrite content is necessary, but usage is not limited to such applications.1.2.1 Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking;
8、 ARP1110 recommends practices to minimize such conditions.2. APPLICABLE DOCUMENTSThe issue of the following documents in effect on the date of the purchase order form a part of this specification to the extent specified herein. The supplier may work to a subsequent revision of a document unless a sp
9、ecific document issue is specified. When the referenced document has been canceled and no superseding document has been specified, the last published issue of that document shall apply.SAE INTERNATIONAL AMS5609D Page 2 of 82.1 SAE PublicationsAvailable from SAE, 400 Commonwealth Drive, Warrendale, P
10、A 15096-0001.AMS 2241 Tolerances, Corrosion and Heat Resistant Steel, Iron Alloy, Titanium, and Titanium Alloy Bars and WireMAM 2241 Tolerances, Metric, Corrosion and Heat Resistant Steel, Iron Alloy, Titanium, and Titanium Alloy Bars and WireAMS 2243 Tolerances, Corrosion and Heat Resistant Steel T
11、ubingMAM 2243 Tolerances, Metric, Corrosion and Heat Resistant Steel TubingAMS 2248 Chemical Check Analysis Limits, Corrosion and Heat Resistant Steels and Alloys, Maraging and Other Highly-Alloyed Steels, and Iron AlloysAMS 2303 Aircraft Quality Steel Cleanliness, Martensitic Corrosion-Resistant St
12、eels, Magnetic Particle Inspection ProcedureMAM 2303 Aircraft Quality Steel Cleanliness, Martensitic Corrosion-Resistant Steels, Magnetic Particle Inspection Procedure, Metric (SI) MeasurementAMS 2315 Determination of Delta Ferrite ContentAMS 2371 Quality Assurance Sampling and Testing, Corrosion an
13、d Heat Resistant Steels and Alloys, Wrought Products and Forging StockAMS 2374 Quality Assurance Sampling and Testing, Corrosion and Heat Resistant Steel and Alloy ForgingsAMS 2806 Identification, Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and Alloy Steels and Corrosion and Heat Resistant
14、 Steels and AlloysAMS 2808 Identification, ForgingsAMS 7493 Rings, Flash Welded, Non-Austenitic, Corrosion Resistant SteelsARP1110 Minimizing Stress Corrosion Cracking in Wrought Forms of Steels and Corrosion Resistant Steels and AlloysAS1182 Standard Machining Allowance, Aircraft-Quality and Premiu
15、m Aircraft-Quality Steel Bars and Mechanical TubingSAE INTERNATIONAL AMS5609D Page 3 of 82.2 ASTM PublicationsAvailable from ASTM, 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959.ASTM A 370 Mechanical Testing of Steel ProductsASTM E 112 Determining the Average Grain SizeASTM E 340 Macroetchi
16、ng Metals and AlloysASTM E 353 Chemical Analysis of Stainless, Heat-Resisting, Maraging, and Other Similar Chromium-Nickel-Iron Alloys3. TECHNICAL REQUIREMENTS3.1 CompositionShall conform to the percentages by weight shown in Table 1, determined by wet chemical methods in accordance with ASTM E 353,
17、 by spectrochemical methods, or by other analytical methods acceptable to purchaser.TABLE 1 - COMPOSITIONElement min maxCarbon 0.12 0.15Manganese - 0.60Silicon - 0.50Phosphorus - 0.025Sulfur - 0.025Chromium 11.50 12.50Columbium 0.05 0.20Nickel - 0.75Molybdenum - 0.20Aluminum - 0.05Copper - 0.50Tin -
18、 0.05Nitrogen - 0.083.1.1 Check AnalysisComposition variations shall meet the requirements of AMS 2248 except that check analysis limits for columbium shall be 0.02 under minimum and 0.05 over maximum.3.2 ConditionThe product shall be supplied in the following condition:3.2.1 BarsAnnealed.SAE INTERN
19、ATIONAL AMS5609D Page 4 of 83.2.1.1 Round BarGround or turned.3.2.1.2 Bars other than rounds, over 0.500 to 2.750 inches (12.70 to 69.85 mm), inclusive, in nominal distance between parallel sides and all hexagons shall be cold finished.3.2.1.3 Bars, other than rounds and hexagons, over 2.750 inches
20、(69.85 mm) in nominal diameter or distance betweenparallel sides shall be hot finished.3.2.2 WireAnnealed and cold drawn.3.2.3 Forging and Flash Welded RingsAnnealed.3.2.3.1 Flash welded rings shall not be supplied unless specified or permitted on the purchasers part drawing. When supplied, rings sh
21、all be manufactured in accordance with AMS 7493. 3.2.4 Mechanical TubingAnnealed and cold finished.3.2.5 Stock for Forging or Flash Welded RingsAs ordered by the forging or flash welded ring manufacturer.3.3 PropertiesThe product shall conform to the following requirements; hardness and tensile test
22、ing shall be performed in accordance with ASTM A 370.3.3.1 Tensile Properties and Hardness as Received3.3.1.1 Bars, Forging, Mechanical Tubing, and Flash Welded RingsHardness shall not be higher than 241 HB or equivalent (See 8.2).3.3.1.2 WireTensile strength shall not be higher than 115 ksi (793 MP
23、a) or equivalent hardness (See 8.3).3.3.2 MacrostructureVisual examination of transverse sections from bars, wire, billets, tube rounds, and stock for forging or flash welded rings,etched in hot hydrochloric acid in accordance with ASTM E 340, shall show no pipe or cracks. Porosity, segregation, inc
24、lusions, and other imperfections shall be no worse than macrostructure standards acceptable to purchaser.3.3.3 DecarburizationBars, wire, and tubing ordered ground, turned, or polished shall be free from decarburization on the ground, turned, or polished surfaces, determined microscopically at a mag
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