AGMA 938-A05-2005 Shot Peening of Gears《齿轮的喷丸强化》.pdf
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1、AGMAINFORMATIONSHEET(This Information Sheet is NOT an AGMA Standard)AGMA938-A05AGMA 938-A05AMERICAN GEAR MANUFACTURERS ASSOCIATIONShot Peening of GearsiiShot Peening of GearsAGMA 938-A05CAUTION NOTICE: AGMA technical publications are subject to constant improvement,revision or withdrawal as dictated
2、 by experience. Any person who refers to any AGMAtechnicalpublicationshouldbesurethatthepublicationisthelatestavailablefromtheAs-sociation on the subject matter.Tablesorotherself-supportingsectionsmaybereferenced. Citationsshouldread: SeeAGMA938-A05,ShotPeeningofGears,publishedbytheAmericanGearManuf
3、acturersAssociation, 500 Montgomery Street, Suite 350, Alexandria, Virginia 22314,http:/www.agma.org.Approved May 3, 2005ABSTRACTThisinformationsheetprovidesatoolforgeardesignersinterestedintheresidualcompressivestressproper-tiesproduced byshot peening and itsrelationship to gearing. It also discuss
4、es shot media materials, deliverymethods, and process controls.Published byAmerican Gear Manufacturers Association500 Montgomery Street, Suite 350, Alexandria, Virginia 22314Copyright 2005 by American Gear Manufacturers AssociationAll rights reserved.No part of this publication may be reproduced in
5、any form, in an electronicretrieval system or otherwise, without prior written permission of the publisher.Printed in the United States of AmericaISBN: 1-55589-847-5AmericanGearManufacturersAssociationAGMA 938-A05AMERICAN GEAR MANUFACTURERS ASSOCIATIONiii AGMA 2005 - All rights reservedContentsPageF
6、oreword iv.1 Scope 1.2 Normative references 1.3 Theory of shot peening 14 Effects of shot peening 25 Shot delivery methods 5.6 Shot media 67 Shot peening process controls 68 Recommendations for specifying shot peening parameters 10Bibliography 14.AnnexesA Graphs and figures expressed in U.S. customa
7、ry units 12Figures1 Bending fatigue improvements from shot peening 2.2 Typical residual stress curve from shot peening 3.3 Approximate depth of compressive layer in steel versus Almen intensity 44 Extrapolation of depth of shot peened compressive layer when surfacehas residual compressive stress pri
8、or to shot peening 4.5 Relative changes from various shot peening intensities using the sameshot size 5.6 Spiral separator for removing broken shot media 77 Shot intensity measurement using Almen strip 88 Comparable intensity values between N, A, and C scales 89 Examples of Almen block mounting on a
9、n actual gear part and on arepresentative geometry 9.10 Saturation curve 9Tables1 Shot size versus intensity range 5AGMA 938-A05 AMERICAN GEAR MANUFACTURERS ASSOCIATIONiv AGMA 2005 - All rights reservedForewordThe foreword, footnotes and annexes, if any, in this document are provided forinformationa
10、l purposes only and are not to be construed as a part of AGMA InformationSheet 938-A05, Shot Peening of Gears.Thepurposeofthisinformationsheetistoprovideacentralizedreferenceforshotpeeninginformation for other AGMA documents. Previously, multiple AGMA documents hadvarying descriptions of the shot pe
11、ening process. This information sheet provides athorough process description to assist the gear designer in understanding andimplementing the shot peening process.ThefirstdraftofAGMA938-A05wasmadeinAugust2003. ItwasapprovedbytheAGMATechnical Division Executive Committee in May 2005.Suggestionsforimp
12、rovementofthisdocumentwillbewelcome. TheyshouldbesenttotheAmericanGearManufacturersAssociation,500MontgomeryStreet,Suite350,Alexandria,Virginia 22314.AGMA 938-A05AMERICAN GEAR MANUFACTURERS ASSOCIATIONv AGMA 2005 - All rights reservedPERSONNEL of the AGMA Metallurgy and Materials CommitteeChairman:
13、Phil Terry Lufkin Industries, Inc.Vice Chairman: Dale J. Weires Boeing Defense therefore, this docu-ment is classified as an information sheet and not astandard. This document intentionally avoids anyreference to quantifying potential increases in gearratingsthroughtheuseofshotpeening. Anyratingsinc
14、reaseattributedtoshotpeeningshouldbeagreedupon between the gear manufacturer and purchas-er, and preferably verified through testing.This document is intended for use by those experi-encedingearmaterialsanddesign. Itisnotintendedfor use by the engineering public at large.Annex A provides figures and
15、 tables in U.S.customary units.2 Normative referencesThe following documents contain provisions which,throughreferenceinthistext,constituteprovisionsofthisinformationsheet. Atthetimeofpublication,theeditions were valid. All publications are subject torevision, and the users of this information sheet
16、 areencouraged to investigate thepossibility ofapplyingthe most recent editions of the publications listed.ANSI/AGMA1012-G05,GearNomenclature,Defi-nitions of Terms with Symbols.AMS-S-13165, Shot Peening of Metal Parts (for-merly MIL-S-13165).3 Theory of shot peeningThe primary purpose for shot peeni
17、ng is to inducebeneficial residual compressive stresses in thesubsurfacelayerofapart. Thisoccursbybombard-ing a metals surface with small, round particlescalled shot. Each impact of the shot media has theeffect of leaving a small hemisphere of residualcompressivestressthatoccursfrom localizedyield-i
18、ng of the base material at the point of shot impact.The materials surface attempts to restore itself, butis restrained by adjacent material, resulting in aresidual compressive stress. Through repeatedimpacts that create overlapping dimples, a uniformlayer of residual compressive stress can be ex-pec
19、ted, provided the shot peening process andmedia are carefully controlled.Duringservice,agearrootfilletissubjecttorepeatedbendingloads. Theseloadsgenerateappliedtensilestresses which are highest in the materials subsur-facelayer. Withtheadditionofshotpeening,appliedbendingstressesareopposedbyresidual
20、compres-sive stresses that have the effect of resisting fatiguecrack initiation and growth throughout the compres-sive layer. For bending fatigue improvement, shotpeening should extend, as a minimum, from thebottom of the root fillet past the tangent pointbetween the root and flank.The beneficial ch
21、aracteristics of residual compres-sive surface stresses are associated with theireffects on fatigue crack initiation behavior. Netstress is the summation of applied and residualstress. When the magnitude of the residual com-pressive stress is greater than the magnitude of theapplied tensile stress,
22、a net compressive stress iscreated. In theory, fatigue cracks will notinitiate inanet compressive stress zone. In addition, fatiguecracksdonotpropagateasreadilyinacompressivestress zone.Residualcompressivesurfacestressesareeffectivein improving bending fatigue life in the elasticmaterial behavior (h
23、igh cycle fatigue) regime.Loading in the plastic material behavior (low cycle)regimeeliminateslifeimprovementeffectsofresidu-al compressive stresses. Failures in the elasticmaterial regime generally initiate at the surface,making surface compressive stresses effective.AGMA 938-A05 AMERICAN GEAR MANU
24、FACTURERS ASSOCIATION2 AGMA 2005 - All rights reservedResidual compressive stress can fractionally in-creasetheelasticendurancestrengthorsignificant-ly increase high cycle fatigue life. Endurancestrengthimprovementswithcompressivestressarenot a direct correlation and only applicable in theelastic be
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