SAE AMS 6361F-2014 Steel Tubing Seamless 0 95Cr - 0 20Mo (0 28 - 0 33C) (SAE 4130) 125 ksi (862 MPa) Tensile Strength (UNS G41300)《拉伸强度125 ksi (862 MPa)的无缝钢管0 95Cr-0 20Mo (0 28-0 3.pdf
《SAE AMS 6361F-2014 Steel Tubing Seamless 0 95Cr - 0 20Mo (0 28 - 0 33C) (SAE 4130) 125 ksi (862 MPa) Tensile Strength (UNS G41300)《拉伸强度125 ksi (862 MPa)的无缝钢管0 95Cr-0 20Mo (0 28-0 3.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 6361F-2014 Steel Tubing Seamless 0 95Cr - 0 20Mo (0 28 - 0 33C) (SAE 4130) 125 ksi (862 MPa) Tensile Strength (UNS G41300)《拉伸强度125 ksi (862 MPa)的无缝钢管0 95Cr-0 20Mo (0 28-0 3.pdf(6页珍藏版)》请在麦多课文档分享上搜索。
1、AEROSPACE MATERIAL SPECIFICATIONAMS6361 REV. FIssued 1942-06Reaffirmed 2009-06Revised 2014-06Superseding AMS6361ESteel Tubing, Seamless0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130)125 ksi (862 MPa) Tensile Strength(Composition similar to UNS G41300)RATIONALEAMS6361F results from a Five Year Review and u
2、pdate of this specification.1. SCOPE1.1 FormThis specification covers an aircraft-quality, low-alloy steel in the form of round, seamless tubing having a wall thickness not greater than 0.188 inch (4.78 mm).1.2 ApplicationThis tubing has been typically used in thin-walled sections where a minimum te
3、nsile strength of 125 ksi (862 MPa) is required, but usage is not limited to such applications.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 subsequ
4、ent 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 PublicationsAvailable from SAE International, 400 Commonwealth Drive
5、, Warrendale, PA 15096-0001, Tel: 877-606-7323 (outside USA and Canada) or 724-776-4970 (outside USA), www.sae.org.AMS2253 Tolerances, Carbon and Alloy Steel TubingAMS2259 Chemical Check Analysis Limits, Wrought Low-Alloy and Carbon SteelsAMS2301 Steel Cleanliness, Aircraft Quality, Magnetic Particl
6、e Inspection ProcedureAMS2370 Quality Assurance Sampling and Testing, Carbon and Low-Alloy Steel Wrought Products and Forging Stock_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
7、 entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefrom, 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 canc
8、elled. SAE invites your written comments and suggestions.Copyright 2014 SAE InternationalAll rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, withou
9、t the prior written permission of SAE.TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada)Tel: +1 724-776-4970 (outside USA)Fax: 724-776-0790Email: CustomerServicesae.orgSAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedbackon this Technical Report, please visit
10、http:/www.sae.org/technical/standards/AMS6361FSAE INTERNATIONAL AMS6361F Page 2 of 6AMS2807 Identification, Carbon and Low-Alloy Steels, Corrosion and Heat-Resistant Steels and Alloys, Sheet, Strip, Plate and Aircraft Tubing2.2 ASTM PublicationsAvailable from ASTM International, 100 Barr Harbor Driv
11、e, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org.ASTM A 370 Mechanical Testing of Steel ProductsASTM E 112 Determining Average Grain SizeASTM E 350 Chemical Analysis of Carbon Steel, Low-Alloy Steel, Silicon Electrical Steel, Ingot Iron, and Wrought IronASTM E 384
12、Knoop and Vickers Hardness of MaterialsASTM E 1444 Magnetic Particle Testing3. TECHNICAL REQUIREMENTS3.1 CompositionShall conform to the percentages by weight shown in Table 1, determined by wet chemical methods in accordance with ASTM E 350, by spectrochemical methods, or by other analytical method
13、s acceptable to purchaser.TABLE 1 - COMPOSITIONElement min maxCarbon 0.28 0.33Manganese 0.40 0.60Silicon 0.15 0.35Phosphorus - 0.025Sulfur - 0.025Chromium 0.80 1.10Molybdenum 0.15 0.25Nickel - 0.25Copper - 0.353.1.1 Check AnalysisComposition variations shall meet the applicable requirements of AMS22
14、59.3.2 ConditionHardened by quenching from a temperature within the range 1500 to 1600 F (816 to 871 C) and tempered to meet the requirements of 3.4.1.3.3 FabricationTubing shall be produced by a seamless process. Any surface finishing operation applied to remove objectionable pits and surface blemi
15、shes shall be performed prior to final heat treatment. A light polish to improve surface appearance may be employed after final heat treatment.3.4 PropertiesTubing shall conform to the following requirements; tensile testing shall be performed in accordance with ASTM A 370:SAE INTERNATIONAL AMS6361F
16、 Page 3 of 63.4.1 Tensile PropertiesShall be as shown in Table 2.TABLE 2 - MINIMUM TENSILE PROPERTIESProperty ValueTensile Strength 125.0 ksi (862 MPa)Yield Strength at 0.2% Offset 100.0 ksi (689 MPa)Elongation in 2 inches (50.8 mm), Full Elongation in 2 inches (50.8mm), Tube Strip12%7%3.4.1.1 Mecha
17、nical property requirements for product outside the size range covered by Table 2 (See 1.1) shall be agreed upon between purchaser and producer.3.4.2 Average Grain SizeShall be ASTM No. 5 or finer, determined in accordance with ASTM E 112.3.4.3 Decarburization3.4.3.1 Tubing ordered ground, turned, o
18、r polished shall be free from decarburization on the ground, turned, or polished surfaces. Decarburization on tubing ID shall not exceed the maximum depth specified in Table 3.3.4.3.2 Allowable decarburization of pierced billets, of tubing for redrawing, or of tubing ordered to specified microstruct
19、ural requirements shall be as agreed upon by purchaser and vendor.3.4.3.3 Tubing to which 3.4.3.1 or 3.4.3.2 is not applicable shall be free from complete decarburization. Partial decarburization shall be not greater than shown in Table 3.TABLE 3A - MAXIMUM DECARBURIZATION, INCH/POUND UNITSNominal W
20、allThickness (T)InchDepth of Partial DecarburizationInchIDDepth of Partial DecarburizationInchODDepth of Partial DecarburizationInchID+ODUp to 0.040, incl 0.18T 0.18T 0.25TOver 0.040 to 0.050, incl 0.009 0.009 0.012Over 0.050 to 0.070, incl 0.010 0.010 0.014Over 0.070 to 0.080, incl 0.012 0.012 0.01
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