SAE ARP 4715-2000 Induction Hardening of Steel Components《钢部件的感应淬火》.pdf
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1、AEROSPACE RECOMMENDEDPRACTICEARP4715Issued 2000-12Reaffirmed 2011-04Induction Hardening of Steel ComponentsRATIONALEThis document has been reaffirmed to comply with the SAE 5-year Review policy.1. SCOPE:This recommended practice provides guidelines for the establishment of an induction hardening pro
2、cess for steel components. It is intended to be used as a guide for designers of induction hardened parts, for process auditors, and for purchase specifications and/or process sheets as applicable.Induction heat treatment is intended for hardening of only selected areas of plain carbon or alloy stee
3、l components. A prior heat treatment may be specified for improved response of the overall component to induction hardening, or for control of properties in the balance of the part. AMS 2759 is recommended for such prior heat treatment.2. APPLICABLE DOCUMENTS:The following documents are often used i
4、n conjunction with induction hardening and should be considered when induction hardening is needed:2.1 SAE Publications:Available from SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001.AMS 2759 Heat Treatment of Steel Parts, General RequirementsAMS 2649 Etch Inspection of High Strength Steel Pa
5、rtsSAE J423 Methods of Measuring Case DepthARP1820 Chord Method of Evaluating Surface Microstructural CharacteristicsSAE 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 volun
6、tary, 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 reaffirmed, revised, or cancelled. SAE invites your wr
7、itten comments and suggestions. Copyright 2011 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 perm
8、ission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: 724-776-4970 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/tec
9、hnical/standards/ARP4715SAE ARP4715 - 2 -2.2 ASTM Documents:Available from ASTM, 100 Barr Harbor Drive, West Conshohocken, PA 19248-2959.ASTM E 18 Rockwell Hardness and Rockwell Superficial Hardness of Metallic MaterialsASTM E 92 Vickers Hardness of Metallic MaterialsASTM E 112 Determining the Avera
10、ge Grain SizeASTM E 384 Microhardness of Materials3. TECHNICAL:3.1 Specifying Induction Hardening:The extent of the induction hardening pattern should be fully defined on the engineering drawing. The definition should include:The minimum and maximum lengths or widths of the hardened zone or case (so
11、metimes calledinduction harden pattern or IHP)The minimum and maximum depth of the hardened zone or caseThe minimum (and in some cases, the maximum) hardness of the caseThe hardness of the core or unaffected base metalThe maximum extent of the heat affected, transition, or intermediate zones. These
12、terms are oftenused interchangeably.The minimum hardness permitted in the overtempered zone (In some cases, the width of theintermediate or transition zone may also be limited.)Locations where hardness measurements or traverses should be taken.Examples of ways to specify the extent and requirements
13、of induction hardening are shown in Figure 1.3.1.1 The transition or overtempered zone is located beneath the hardened zone. Having been exposed to temperatures not high enough to harden it, but substantially higher than the core or base metal tempering temperature, this area may be softer than the
14、core or base metal. The designer may limit the extent of softening, either by specifying a minimum hardness, or by specifying the maximum width of the zone, or both. It is recommended that the permissible hardness reduction in the overtempered or transition zone be 4 to 8 points HRC below the origin
15、al core or base metal hardness. A minimum width of 0.03 inch (0.76 mm) is often obtainable for smaller sections, but specifying the maximum width that can be tolerated in the design is recommended. A transition zone equal to the minimum case depth required by the specification or drawing is consider
16、ed reasonable.3.1.2 Hardness at the surface of the induction hardened range is generally measured by direct Rockwell or Superficial Rockwell hardness testing in accordance with ASTM E 18. However, depth of hardening and extent of heat affected zone are normally determined destructively, on a cross-s
17、ection of the part, using microhardness techniques such as those of ASTM E 384, ARP1820 or SAE J423.SAE ARP4715 - 3 -3.1.3 Material:3.1.3.1 Type of Steel: In general, steels with carbon contents of 0.35% or more will respond to induction hardening, although a carbon content approaching 0.5% may be n
18、ecessary to obtain hardnesses exceeding 55 HRC. A fine grained steel (ASTM No. 5 to 8 determined in accordance with ASTM E 112) is desirable. In general, low alloy steels that have been normalized and tempered or quenched and tempered in accordance with AMS 2759 are desirable.3.1.3.2 Tempering After
19、 Induction Hardening: The as-induction hardened microstructure is dependent on material composition, hardenability, prior structure and quench rate, and will generally consist of a martensitic structure. Since the martensitic structure is normally crack sensitive after cooling from the hardening tem
20、perature, the entire part is invariably tempered after induction hardening, at temperatures ranging from 300 to 1000 F (149 to 538 C). The designer may specify a specific tempering temperature or may specify a maximum or minimum case hardness. However, in all instances, the drawing must require temp
21、ering after hardening.3.1.3.3 Microstructure: Unless the designer specifies otherwise, the resultant microstructure should consist of tempered martensite at the surface and throughout the case or induction hardened zone. All areas of the induction hardened case should meet the minimum case hardness,
22、 with a relatively sudden drop to below the base metal hardness at the start of the transition zone (See Figure 2). Typically, grain size, when determined, which is often equated with toughness, should not increase by more than one or two ASTM grain size numbers, but in no instance should the design
23、er expect grain sizes larger than ASTM No. 3 when starting with a grain size of ASTM No. 5 to 8, nor evidence of free ferrite at the surface, both indicative of excessive heating and detrimental to performance or reliability.An insufficient quench may result in a portion of the material remaining un
24、transformed. Standards for such untransformed material, called retained austenite, may be specified by the designer.3.1.4 Recommended Case Depths: The case depth selected by the designer depends on the application and section size. For surface hardening, the depth should be less than one third of th
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