SAE AMS 6325K-2015 Steel Bars and Forgings 0 50Cr - 0 55Ni - 0 25Mo (0 38 - 0 43C) (SAE 8740) Heat Treated 105 ksi (724 MPa) Tensile Strength (UNS G87400).pdf
《SAE AMS 6325K-2015 Steel Bars and Forgings 0 50Cr - 0 55Ni - 0 25Mo (0 38 - 0 43C) (SAE 8740) Heat Treated 105 ksi (724 MPa) Tensile Strength (UNS G87400).pdf》由会员分享,可在线阅读,更多相关《SAE AMS 6325K-2015 Steel Bars and Forgings 0 50Cr - 0 55Ni - 0 25Mo (0 38 - 0 43C) (SAE 8740) Heat Treated 105 ksi (724 MPa) Tensile Strength (UNS G87400).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/AMS6325KAEROSPACEMATERIAL SPECIFICATIONAMS6325 REV. KIssued 1942-08Reaffirmed 2000-08Revised
5、2015-12Superseding AMS6325JSteel, Bars, and Forgings0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740)Heat Treated, 105 ksi (724 MPa) Tensile Strength(Composition similar to UNS G87400)RATIONALEAMS6325K results from a Five Year Review and update of this specification that revises macrostructure, gra
6、in size testing, decarburization testing methods, and reporting.1. SCOPE1.1 FormThis specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars and forgings.1.2 ApplicationThese products have been used typically for parts, such as nuts, bolts, and screws, 1.750 inches
7、 (44.45 mm) and under in section thickness requiring a minimum tensile strength of 105 ksi (724 MPa), 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
8、 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 specified, the last published issue of that document shall apply.2.1 SAE PublicationsAva
9、ilable from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or +1 724-776-4970 (outside USA), www.sae.org.AMS2251 Tolerances, Low-Alloy Steel BarsAMS2259 Chemical Check Analysis Limits, Wrought Low-Alloy and Carbon SteelsAMS2301 Steel C
10、leanliness, Aircraft Quality, Magnetic Particle Inspection ProcedureAMS2370 Quality Assurance Sampling and Testing, Carbon and Low-Alloy Steel Wrought Products and Forging StockSAE INTERNATIONAL AMS6325K Page 2 of 7AMS2372 Quality Assurance Sampling and Testing, Carbon and Low-Alloy Steel ForgingsAM
11、S2750 PyrometryAMS2759/1 Heat Treatment of Carbon and Low-Alloy Steel Parts Minimum Tensile Strength Below 220 ksi (1517 MPa)AMS2806 Identification, Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and Alloy Steels and Corrosion and Heat-Resistant Steels and AlloysAMS2808 Identification Forging
12、sAS1182 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 Mechanical
13、 Testing of Steel ProductsASTM E112 Determining Average Grain SizeASTM E350 Chemical Analysis of Carbon Steel, Low-Alloy Steel, Silicon Electrical Steel, Ingot Iron, and Wrought IronASTM E381 Macroetch Testing Steel Bars, Billets, Blooms, and ForgingsASTM E384 Knoop and Vickers Hardness of Materials
14、3. TECHNICAL REQUIREMENTS3.1 CompositionShall conform to the percentages by weight shown in Table 1, determined by wet chemical methods in accordance with ASTM E350, by spectrochemical methods, or by other analytical methods acceptable to purchaser.Table 1 - CompositionElement min maxCarbon 0.38 0.4
15、3Manganese 0.75 1.00Silicon 0.15 0.35Phosphorus - 0.025Sulfur - 0.025Chromium 0.40 0.60Nickel 0.40 0.70Molybdenum 0.20 0.30Copper - 0.353.1.1 Aluminum, vanadium and columbium are optional grain refining elements and need not be determined or reported unless used to satisfy the average grain size req
16、uirements of 3.4.2.2.3.1.2 Check AnalysisComposition variations shall meet the applicable requirements of AMS2259.SAE INTERNATIONAL AMS6325K Page 3 of 73.2 ConditionThe product shall be supplied in the following condition:3.2.1 BarsBar shall not be cut from plate (also see 4.4.2).3.2.1.1 Bars 0.500
17、Inch (12.70 mm) and Under in Nominal Diameter or Least Distance Between Parallel SidesCold finished, hardened, and tempered.3.2.1.2 Bars Over 0.500 Inch (12.70 mm) in Nominal Diameter or Least Distance Between Parallel SidesHot finished, (or cold finished when so ordered), hardened, and tempered.3.2
18、.2 ForgingsHardened and tempered in accordance with AMS2759/1.3.3 Heat TreatmentThe product shall be austenitized and hardened by quenching from 1550 F 25 F (843 C 14 C) and tempered as required to meet the requirements of 3.4.4 and 3.4.5. Pyrometry shall be in accordance with AMS2750.3.4 Properties
19、The product shall conform to the following requirements; hardness and tensile testing shall be performed in accordance with ASTM A370:3.4.1 MacrostructureVisual examination of transverse full cross-sections from bars and forging stock etched in hot hydrochloric acid in accordance with ASTM E381, sha
20、ll show no pipe or cracks. Porosity, segregation, inclusions, and other imperfections shall be no worse than the macrographs of ASTM E381 shown in Table 2.Table 2 - Macrostructure limitsCross-Section AreaSquare InchesCross-Section AreaSquare Centimeters MacrographsUp to 36, incl Up to 232, incl S2 -
21、 R1 - C2Over 36 to 133, incl Over 232 to 858, incl S2 - R2 - C3Over 133 Over 858 Note 1Note 1: Limits for larger sizes shall be agreed upon by purchaser and producer. The purchaser shall have written approval of the agreement from the cognizant engineering organization.3.4.2 Average Grain SizeAverag
22、e grain size shall be determined by either 3.4.2.1 or 3.4.2.2.3.4.2.1 Shall be ASTM No. 5 or finer, determined in accordance with ASTM E112 on specimens following heat treatment per 3.3 and the specimen shall be without further heat treatment that involves re-austenitization.3.4.2.2 The product of a
23、 heat shall be considered to have an ASTM No. 5 or finer austenitic grain size if one or more of the following are determined by heat analysis (see 8.5):3.4.2.2.1 A total aluminum content of 0.020 to 0.050%.SAE INTERNATIONAL AMS6325K Page 4 of 73.4.2.2.2 An acid soluble aluminum content of 0.015 to
24、0.050%.3.4.2.2.3 A vanadium content of 0.02 to 0.08%.3.4.2.2.4 A columbium content of 0.02 to 0.05%.3.4.3 Decarburization3.4.3.1 Bars ordered ground, turned, or polished shall be free from decarburization on the ground, turned, or polished surfaces.3.4.3.2 Decarburization of bars that 3.4.3.1 is not
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