SAE AMS 6382P-2014 Steel Bars Forgings and Rings 0 95Cr - 0 20Mo (0 38 - 0 43C) (SAE 4140) Annealed (UNS G41400)《0 95Cr-0 20Mo(0 38-0 43C)(SAE 4140)煅烧的钢棒、钢铸件和钢环》.pdf
《SAE AMS 6382P-2014 Steel Bars Forgings and Rings 0 95Cr - 0 20Mo (0 38 - 0 43C) (SAE 4140) Annealed (UNS G41400)《0 95Cr-0 20Mo(0 38-0 43C)(SAE 4140)煅烧的钢棒、钢铸件和钢环》.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 6382P-2014 Steel Bars Forgings and Rings 0 95Cr - 0 20Mo (0 38 - 0 43C) (SAE 4140) Annealed (UNS G41400)《0 95Cr-0 20Mo(0 38-0 43C)(SAE 4140)煅烧的钢棒、钢铸件和钢环》.pdf(8页珍藏版)》请在麦多课文档分享上搜索。
1、AEROSPACE MATERIAL SPECIFICATION AMS6382 REV. P Issued 1939-12 Reaffirmed 2006-02 Revised 2014-08 Superseding AMS6382N Steel, Bars, Forgings, and Rings 0.95Cr - 0.20Mo (0.38 - 0.43C) (SAE 4140) Annealed (Composition similar to UNS G41400) RATIONALE AMS6382P results from a Five Year Review and update
2、 of this specification that revises macrostructure, decarburization, and reporting requirements. 1. SCOPE 1.1 Form This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings. 1.2 Application These prod
3、ucts have been used typically for parts 0.50 inch (12.7 mm) and under in nominal section thickness at time of heat treatment, requiring a through-hardened steel capable of developing hardness as high as 50 HRC when appropriately heat treated and for parts of greater thickness but requiring proportio
4、nately lower hardness, 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 after heat treatment; ARP1110 recommends practices to minimize such conditions. 2. APPLICABLE DOCUMENTS The
5、 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. When the referenced document has been cancelled
6、 and no superseding document has been specified, the last published issue of that document shall apply. _ 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 i
7、ts 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 cancelled. SAE invites your w
8、ritten comments and suggestions. Copyright 2014 SAE International All 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, without the prior written per
9、mission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: +1 724-776-4970 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org SAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.o
10、rg/technical/standards/AMS6382P SAE INTERNATIONAL AMS6382P Page 2 of 8 2.1 SAE Publications Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org. AMS2251 Tolerances, Low-Alloy Steel B
11、ars AMS2259 Chemical Check Analysis Limits, Wrought Low-Alloy and Carbon Steels AMS2301 Steel Cleanliness, Aircraft Quality, Magnetic Particle Inspection Procedure AMS2370 Quality Assurance Sampling and Testing, Carbon and Low-Alloy Steel Wrought Products and Forging Stock AMS2372 Quality Assurance
12、Sampling and Testing, Carbon and Low-Alloy Steel Forgings AMS2806 Identification, Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and Alloy Steels and Corrosion and Heat-Resistant Steels and Alloys AMS2808 Identification, Forgings AMS7496 Rings, Flash Welded, Carbon and Low-Alloy Steels AS1182
13、 Standard Stock Removal Allowance, Aircraft-Quality and Premium Aircraft-Quality Steel Bars and Mechanical Tubing ARP1110 Minimizing Stress Corrosion Cracking in Wrought Forms of Steels and Corrosion Resistant Steels and Alloys 2.2 ASTM Publications Available from ASTM International, 100 Barr Harbor
14、 Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM A 255 Determining the Hardenability of Steel ASTM A 370 Mechanical Testing of Steel Products ASTM E 112 Determining Average Grain Size ASTM E 350 Chemical Analysis of Carbon Steel, Low-Alloy Steel, Silicon
15、 Electrical Steel, Ingot Iron, and Wrought Iron ASTM E 381 Macroetch Testing Steel Bars, Billets, Blooms, and Forgings ASTM E 384 Knoop and Vickers Hardness of Materials 3. TECHNICAL REQUIREMENTS 3.1 Composition Shall conform to the percentages by weight shown in Table 1, determined by wet chemical
16、methods in accordance with ASTM E 350, by spectrochemical methods, or by other analytical methods acceptable to purchaser. SAE INTERNATIONAL AMS6382P Page 3 of 8 TABLE 1 - COMPOSITION Element min max Carbon 0.38 0.43 Manganese 0.75 1.00 Silicon 0.15 0.35 Phosphorus - 0.025 Sulfur - 0.025 Chromium 0.
17、80 1.10 Molybdenum 0.15 0.25 Nickel - 0.25 Copper - 0.35 3.1.1 Check Analysis Composition variations shall meet the applicable requirements of AMS2259. 3.2 Condition The product shall be supplied in the following condition; hardness and tensile strength shall be determined in accordance with ASTM A
18、370: 3.2.1 Bars 3.2.1.1 Bars 0.500 Inch (12.70 mm) and Under in Nominal Diameter or Least Distance Between Parallel Sides Annealed and cold finished having tensile strength not higher than 125 ksi (862 MPa) or equivalent hardness (See 8.2). 3.2.1.2 Bars Over 0.500 Inch (12.70 mm) in Nominal Diameter
19、 or Least Distance Between Parallel Sides Hot finished and annealed, unless otherwise ordered, having hardness not higher than 229 HB, or equivalent (See 8.3). Product ordered annealed and cold finished shall have hardness not higher than 241 HB, or equivalent (See 8.3). 3.2.1.3 Bar shall not be cut
20、 from plate (Also see 4.4.2). 3.2.2 Forgings and Flash Welded Rings As ordered. 3.2.2.1 Flash welded rings shall not be supplied unless specified or permitted on purchasers part drawing. When supplied, rings shall be manufactured in accordance with AMS7496. 3.2.3 Stock for Forging or Flash Welded Ri
21、ngs As ordered by the forging or flash welded ring manufacturer. 3.3 Properties The product shall conform to the following requirements; hardness testing shall be performed in accordance with ASTM A 370: 3.3.1 Macrostructure Visual examination of transverse full cross-sections from bars, billets, an
22、d stock for forging or flash welded rings, etched in hot hydrochloric acid in accordance with ASTM E 381, shall show no pipe or cracks. Porosity, segregation, inclusions, and other imperfections shall be no worse than the macrographs of ASTM E 381 shown in Table 2. SAE INTERNATIONAL AMS6382P Page 4
23、of 8 TABLE 2 - MACROSTRUCTURE LIMITS Cross-Sectional Area Square Inches Cross-Sectional Area Square Centimeters Macrographs Up to 36, incl Up to 232, incl S2 - R1 - C2 Over 36 to 133, incl Over 232 to 858, incl S2 - R2 - C3 Over 133 Over 858 Note 1 Note 1 Limits for larger sizes shall be agreed upon
24、 by producer and purchaser. The purchaser shall have written approval of the agreement from the cognizant engineering organization. 3.3.2 Average Grain Size of Bars, Forgings and Flash Welded Rings Shall be ASTM No. 5 or finer determined in accordance with ASTM E 112. 3.3.3 Hardenability of Each Hea
- 1.请仔细阅读文档,确保文档完整性,对于不预览、不比对内容而直接下载带来的问题本站不予受理。
- 2.下载的文档,不会出现我们的网址水印。
- 3、该文档所得收入(下载+内容+预览)归上传者、原创作者;如果您是本文档原作者,请点此认领!既往收益都归您。
下载文档到电脑,查找使用更方便
10000 积分 0人已下载
下载 | 加入VIP,交流精品资源 |
- 配套讲稿:
如PPT文件的首页显示word图标,表示该PPT已包含配套word讲稿。双击word图标可打开word文档。
- 特殊限制:
部分文档作品中含有的国旗、国徽等图片,仅作为作品整体效果示例展示,禁止商用。设计者仅对作品中独创性部分享有著作权。
- 关 键 词:
- SAEAMS6382P2014STEELBARSFORGINGSANDRINGS095CR020MO038043CSAE4140ANNEALEDUNSG41400095CR020MO038043CSAE4140

链接地址:http://www.mydoc123.com/p-1022395.html