SAE AMS 6340B-2014 Steel Bars Forgings and Tubing 0 88Cr - 1 8Ni - 0 42Mo - 0 08V (0 28 - 0 33C) (4330 Mod) Consumable Electrode Vacuum Remelted (UNS K23080)《0 88Cr-1 8Ni-0 42Mo-0 .pdf
《SAE AMS 6340B-2014 Steel Bars Forgings and Tubing 0 88Cr - 1 8Ni - 0 42Mo - 0 08V (0 28 - 0 33C) (4330 Mod) Consumable Electrode Vacuum Remelted (UNS K23080)《0 88Cr-1 8Ni-0 42Mo-0 .pdf》由会员分享,可在线阅读,更多相关《SAE AMS 6340B-2014 Steel Bars Forgings and Tubing 0 88Cr - 1 8Ni - 0 42Mo - 0 08V (0 28 - 0 33C) (4330 Mod) Consumable Electrode Vacuum Remelted (UNS K23080)《0 88Cr-1 8Ni-0 42Mo-0 .pdf(9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 2014 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/AMS6340BAEROSPACE MATERIAL SPECIFICATIONAMS6340 REV. BIssued 2006-03Revised 2014-07Supersedin
5、g AMS6340ASteel Bars, Forgings, and Tubing0.88Cr - 1.8Ni - 0.42Mo - 0.08V (0.28 - 0.33C) (4330 Mod)Consumable Electrode Vacuum Remelted(Composition similar to UNS K23080)RATIONALEAMS6340B results from a Five Year Review and update of this specification that revises macrostructure, steel cleaniness,
6、decarburization, and reporting requirements.1. SCOPE1.1 FormThis specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.1.2 ApplicationThese products have been used typically for parts requiring high tensile strength and g
7、ood ductility with relatively high impact strength, superior transverse properties, and hardness, but usage is not limited to these applications. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking after heat treatment; ARP1110 recomme
8、nds practices to minimize such conditions.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
9、 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, Warrendale, PA 15096-0001, Tel: 877-606-7323 (insid
10、e USA and Canada) or 724-776-4970 (outside USA), www.sae.org.AMS2251 Tolerances, Low-Alloy Steel BarsAMS2253 Tolerances, Carbon and Alloy Steel TubingAMS2259 Chemical Check Analysis Limits, Wrought Low-Alloy and Carbon SteelsSAE INTERNATIONAL AMS6340B Page 2 of 9AMS2300 Steel Cleanliness, Premium Ai
11、rcraft-Quality, Magnetic Particle Inspection ProcedureAMS2310 Qualification Sampling and Testing of Steelsfor Transverse Tensile PropertiesAMS2370 Quality Assurance Sampling and Testing, Carbon and Low-Alloy Steel Wrought Products and Forging StockAMS2372 Quality Assurance Sampling and Testing, Carb
12、on and Low-Alloy Steel ForgingsAMS2806 Identification, Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and Alloy Steels and Corrosion and Heat -Resistant Steels and AlloysAMS2808 Identification, ForgingsAS1182 Standard Stock Removal Allowance, Aircraft-Quality and Premium Aircraft-Quality Stee
13、l Bars and Mechanical TubingARP1110 Minimizing Stress Corrosion Cracking in Wrought Forms of Steels and Corrosion Resistant Steels and Alloys2.2 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.
14、ASTM A 255 End-Quench Test for Hardenability of SteelASTM A 370 Mechanical Testing of Steel ProductsASTM A 604 Macroetch Testing of Consumable Electrode Remelted Steel Bars and BilletsASTM E 45 Determining the Inclusion Content of SteelASTM E 112 Determining Average Grain SizeASTM E 350 Chemical Ana
15、lysis of Carbon Steel, Low-Alloy Steel, Silicon Electrical Steel, Ingot Iron, and Wrought IronASTM E 384 Knoop and Vickers Hardness of Materials3. TECHNICAL REQUIREMENTS3.1 CompositionShall conform to the percentages by weight shown in Table 1, determined by wet chemical methods in accordance with A
16、STM E 350, by spectrochemical methods, or by other analytical methods acceptable to purchaser.SAE INTERNATIONAL AMS6340B Page 3 of 9TABLE 1 - COMPOSITIONElement min maxCarbon 0.28 0.33Manganese 0.65 1.00Silicon 0.15 0.35Phosphorus - 0.015Sulfur - 0.015Chromium 0.75 1.00Nickel 1.65 2.00Molybdenum 0.3
17、5 0.50Vanadium 0.05 0.10Copper - 0.353.1.1 Check AnalysisComposition variations shall meet the applicable requirements of AMS2259.3.2 Melting PracticeSteel shall be multiple melted using consumable electrode vacuum process in the remelt cycle.3.3 ConditionThe product shall be supplied in the followi
18、ng condition; hardness and tensile strength shall be determined in accordance with ASTM A 370:3.3.1 Bars3.3.1.1 Bars 0.500 Inch (12.70 mm) and Under in Nominal Diameter or Least Distance Between Parallel SidesCold finished having tensile strength not higher than 130 ksi (896 MPa), or equivalent hard
19、ness (See 8.2).3.3.1.2 Bars Over 0.500 Inch (12.70 mm) in Nominal Diameter or Least Distance Between Parallel SidesHot finished, and annealed if necessary, unless otherwise ordered, having hardness not higher than 241 HB, or equivalent (See 8.3). Bars ordered cold finished may have hardness as high
20、as 248 HB, or equivalent (See 8.3). 3.3.1.3 Bar shall not be cut from plate (Also see 4.4.2).3.3.2 ForgingsNormalized and tempered having hardness not higher than 269 HB, or equivalent (See 8.3). 3.3.3 Mechanical TubingCold finished, unless otherwise ordered, having hardness not higher than 25 HRC,
21、or equivalent (See 8.3). Tubing ordered hot finished and annealed shall have hardness not higher than 99 HRB, or equivalent (See 8.3).3.3.4 Forging StockAs ordered by the forging manufacturer.3.4 PropertiesThe product shall conform to the following requirements; hardness and tensile testing shall be
22、 performed in accordance with ASTM A 370:SAE INTERNATIONAL AMS6340B Page 4 of 93.4.1 MacrostructureVisual examination of transverse full cross-sections from bars, billets, tube rounds, or forging stock, etched in accordance with ASTM A 604 in hot hydrochloric acid, shall show no pipe or cracks. Poro
23、sity, segregation, inclusions, and other imperfections shall be no worse than macrographs of ASTM A 604 shown in Table 2.TABLE 2 - MACROSTRUCTURE LIMITSClass Condition Severity1Freckles A2 White Spots A3 Radial Segregation B4 Ring Pattern B3.4.2 Micro-Inclusion RatingNo specimen shall exceed the lim
24、its shown in Table 3, determined in accordance with ASTM E 45, Method D.TABLE 3 - MICRO-INCLUSION RATING LIMITSAABBCCDDType Thin Heavy Thin Heavy Thin Heavy Thin HeavyWorst Field Severity 2.0 1.0 1.5 1.0 1.5 1.0 1.5 1.0Worst Field Frequency,maxmum a1a1a153Total Rateable Fields,Frequency, maximum b 1
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