AGMA 06FTM09-2006 Opportunities to Replace Wrought Gears with High Performance PM Gears in Automotive Applications《在汽车应用中用高性能PM齿轮替换精加工齿轮的时机》.pdf

上传人:progressking105 文档编号:422030 上传时间:2018-11-06 格式:PDF 页数:9 大小:293.55KB
下载 相关 举报
AGMA 06FTM09-2006 Opportunities to Replace Wrought Gears with High Performance PM Gears in Automotive Applications《在汽车应用中用高性能PM齿轮替换精加工齿轮的时机》.pdf_第1页
第1页 / 共9页
AGMA 06FTM09-2006 Opportunities to Replace Wrought Gears with High Performance PM Gears in Automotive Applications《在汽车应用中用高性能PM齿轮替换精加工齿轮的时机》.pdf_第2页
第2页 / 共9页
AGMA 06FTM09-2006 Opportunities to Replace Wrought Gears with High Performance PM Gears in Automotive Applications《在汽车应用中用高性能PM齿轮替换精加工齿轮的时机》.pdf_第3页
第3页 / 共9页
AGMA 06FTM09-2006 Opportunities to Replace Wrought Gears with High Performance PM Gears in Automotive Applications《在汽车应用中用高性能PM齿轮替换精加工齿轮的时机》.pdf_第4页
第4页 / 共9页
AGMA 06FTM09-2006 Opportunities to Replace Wrought Gears with High Performance PM Gears in Automotive Applications《在汽车应用中用高性能PM齿轮替换精加工齿轮的时机》.pdf_第5页
第5页 / 共9页
亲,该文档总共9页,到这儿已超出免费预览范围,如果喜欢就下载吧!
资源描述

1、06FTM09Opportunities to Replace Wrought Gears withHigh Performance PM Gears in AutomotiveApplicationsby: U. Engstrm and D. Milligan, North American Hgans, USAand P. Johansson and S. Dizdar, Hgans AB, SwedenTECHNICAL PAPERAmerican Gear Manufacturers AssociationOpportunities to Replace Wrought Gears w

2、ith HighPerformance PM Gears in Automotive ApplicationsUlf Engstrm and David Milligan, North American Hgans, USAand Pernilla Johansson and Senad Dizdar, Hgans AB, SwedenThe statements and opinions contained herein are those of the author and should not be construed as anofficial action or opinion of

3、 the American Gear Manufacturers Association.AbstractPowder metallurgy (PM) enables cost effective production of components with complex geometries such asgears. During the last decades the use of PM components in automotive applications has show continuousgrowth. In order to continue this growth it

4、 is important to maintain the strong points of PM, i.e. the net shapecapabilitywhileperformanceisfurtherimprovedtofulfillmoreandmoredemandingrequirements.Gearsforautomotive applications are complex in shape and require both very high geometrical accuracy in terms ofgear quality and very high mechani

5、cal performance in terms of durability of tooth flank and root. By utilizingselective densification of the teeth the accuracy and mechanical performance requirements can be met at avery low added cost.In this paper a PM process route consisting of compaction, sintering, surface densification and fin

6、ally heattreatment has been studied to assess the feasibility of producing high performance gears by powdermetallurgy.Helicalandspurgearswereusedinthestudywherethedensificationaswellastheresultinggearquality and durability were tested.Copyright 2006American Gear Manufacturers Association500 Montgome

7、ry Street, Suite 350Alexandria, Virginia, 22314October, 2006ISBN: 1-55589-891-21Opportunities to Replace Wrought Gears with High PerformancePM Gears in Automotive ApplicationsUlf Engstrm and David Milligan, North American Hgans, USAand Pernilla Johansson, Senad Dizdar, Hgans AB, SwedenIntroductionPo

8、wder metallurgy enables cost effective produc-tion of parts with complex geometries such asgears. The amount of waste material is often negli-gible as a consequence of the minimal necessity tomachinethepartsandthe useof ecologicallyharm-ful cutting fluids is avoided.The growthof thePM markethas alon

9、g historyandwe have not seen significant downturns in thisgrowth. In order to continue this growth it is impor-tant to maintain the PM strong points, i.e. the netshape capability while performance is improved. Inorder to expand the PM market new applicationscouldbewonbycombiningtheinherentadvantages

10、of PM while performance is increased by surfacedensification.Gear rolling is a well-known technology for improv-ing the shape and surface finish of solid steel gears1,2,3,4. When applied on PM gears, rolling alsoenhances the fatigue properties since the densityandhencethestrengthinthehighly loadedre

11、gions,i.e. the surface regions, increases to full density 2,3, 5, 6, 7. This technique was first developed morethan 20 years ago, but has not reachedwidespreaduse due to several reasons. The difficulty in obtain-ing good densification and good gear quality simul-taneously has limited the applicabili

12、ty and cost ef-fectivenessoftheprocess.Alsothelongdevelopingtimes have hindered the utilization of the surfacedensified gears. Improvements in rolling machinesand increase in knowledge and experience havesignificantlychangedthesituation7.Severalpartsproducers have after significant and committed de-

13、velopment work started to offer surface densifiedcomponents to the market 5, 8, 9. Another factorlimiting the use of surface densification technologyhas been the continuous market growth. In fact aslong as the requirements fromthe moredemandingapplications could be met using existingtechnologies the

14、 driving force for developing sur-face densification technology was limited.This paper aims atpointing outsome possibilitiesinusing the combination of powder metallurgy andsurface densification. It will be demonstrated thatthe performance oftwo surfacedensified gearscanbe adequate for highly loaded

15、applications. Thegear quality is also presented and discussed.Gears studiesThe gears examined in this study are the fifth gearused in a manual gearbox in a passenger car andthe planetary gear in the reduction unit in a heavytruckgearbox.ThetwogearsareshowninFigure1.Figure 1a. Fifth gear of a manualt

16、ransmission in a Volvo passenger car.Figure 1b. Planetary gear of a reduction unitin a Scania heavy truck gearbox.Typicaldataofthegearsarepresentedintable1. Inthis study both gears were manufactured by com-bining the PM process route with gear rolling. Thehelical gear was redesigned in order to faci

17、litatetesting in a pitting test rig. The clutch gear was re-moved,thediameteroftheborewasenlargedandakeyway was introduced.2Table 1. Gear data.Spur gear HelicalgearNumber of teethZ20 28Normal modulemn(mm) 3.650 2Pressure anglen22.5_ 15_Helix angle 0_ 32_Addendummodification co-efficient x0.471 0.136

18、Over ball diam-eter (mm) 89.350 74.46ExperimentalThe investigated gears were pressed and sinteredto cylindrical blanks. The cylinders were machinedto larger dimensions than on the drawing to havesome stock material to compress during surfacedensification. The work piece was rolled betweentwo dies in

19、 order to densify the surface of the toothflank and root regions. The surface of the compo-nentwascompressedandthedensityinthesurfaceincreased to full density. The tooth-root-fatigueproperties of the gears were tested in an electro-magnetic pulsator.MaterialsReference gears of wrought steels were ma

20、nufac-tured by turning, hobbing, shaving and heat treat-ment.Thematerialsusedforthesegearsareofsim-ilar type (designation) as the material for the gearsused in production. The planetary gear is manufac-tured using the Swedish standard steel SS92506which corresponds to DIN 20NiCrMo2 and AISI8620. The

21、 helical gear is made in DIN 16MnCr5,which corresponds to AISI 5115 and is very similarto AISI 5120.The powder mix selected for this study was Astaloy85 Mo (Fe-0.85Mo, FL4400) with low graphite con-tent. The compositions in the sintered condition aregivenintable2.Table 2. Chemical composition of sin

22、teredand solid steel.Gear MaterialC(%)Mo(%)Cr(%)Mn(%)Ni(%)Spur gearReference SS 92506DIN 20NiCrMo2AISI 86200.20 0.20 0.55 0.50 0.55PM gear(SG)Astaloy 85MoFe-0.85MoFL44000.28 0.85 - - -Helical gearReference DIN 16MnCr5AISI 51150.16 - 0.95 1.15 -PM gear(HG)Astaloy 85MoFe-0.85MoFL44000.20 0.85 - - -Man

23、ufacture of PM gear blanksPM gear blanks were manufactured by compactionofcylindricalblanksfollowedbysinteringat1120_Cfor 30 min in a mixture of 90% N2and 10% H2gasatmosphere. The blank densities were 7.15 g/cm3forthespurgearand7.20and7.10g/cm3forthehe-licalgear.Thesinteredblankswerethenturnedandhob

24、bed to the desired preform shape. The amountof stock material is estimated using simple calcula-tions of material needed to achieve the requireddensification.Surface densification by rollingIn the present work a HC20CN rolling machine(Escofier Technologie SA. Chalon. France) wasusedforthedensificati

25、ontrialsasshowninFigure2.Figure 2. Surface densification of a helicaltransmission gearTherollingcyclecanbedividedintothreeparts;theinitiation where the tool and the gear mesh andmakecontact.Thesecondphaseiswhentheloadisapplied and the tools deform the gear until a presetcenter distance has been reac

26、hed. The third phaseisthetoolwithdrawalwhere thetools moveoutwardsothatthegearcanbeunloaded.Inaserialproduc-3tion set-up a cycle time including loading and un-loading would be 8-15 seconds.Heat treatmentThe heat treatments selected for the two differentgearswerenotthesame.The spurgear wascarbu-rized

27、 at940oCwith acarbon potentialof 0.8%Cfol-lowed by quenching in oil. A stress relieving opera-tion was performed at 160 _C for 60 minutes.The helical gear was gas carburized at 920_Cfol-lowed by a quench in oil at 80 _C. The stress reliev-ing was performed at 170 _C for 60 minutes in air.The side fa

28、ces of the gear were masked using acommercialmaskingpasteinordertolimitthepene-tration of carbon through the low-density sidefaces.Ineachcaseisthecarburizing timeselected sothatthe required case depth should be reached for thedifferent gears. The case depth is defined as thedepth below the surface w

29、here the hardness hasdropped to 550 HV0.1.Gear qualityThe geometrical quality of the gears was measuredby a Klingelnberg P26 3D measuring center. In allcases were the reference axis defined by the gearteeth themselves. The target gear quality for all thegears was DIN quality 8. Some limited trials w

30、ereperformed in order to assess the consistency of theprocess. The diameter over balls was measured onthe blanks and on rolled gears. The densification ofthegearswasassessedbyusingimageanalysisonpolished samples. The response to the heat treat-ment was examined using etched microstructuresof tooth f

31、lank and root regions. The heat treatmentwas further examined using micro hardness mea-surements. Adensification depthwas arbitrarilyde-finedasthedistancefromthesurfacewherethepo-rosity has increased to 2%.TestingThe spur gear was tested in a servo-hydraulic test-ing machine. The load was applied on

32、 the flank ofthetooth.The loadratio was0.1. Samplesreaching2 million cycles were considered as run outs. In all15 tests were performed. The helical HG-Mo gearwas tested in an electro-magnetic pulsator. Thetestrigwasfittedwithaspecialclampingdevicethatappliedtheloadatthetopofthegearteeth.Further-more

33、, a fixture ensured that the gear could not turnor twist during loading. The load ratio was also herekept at 0.1 in order to ensure contact between theclamping device and the gear teeth at all times. Asthe load is applied at the tooth top and not on thetoothflankandthedifferenceingeometryintherootre

34、gion it was not attempted to calculate the maxi-mum bending stresses in the root region. In thiscase the specimens are considered run-outs whenthey reach 30 million cycles.ResultsDensificationThe result of the densification of the spur gear canbe seen in Figure 3. The densification depth isapproxima

35、tely 0.5 mm on the flank and slightly low-er in the root region. For the helical gear the situa-tion is the reverse as can be seen in Figures 4. Thedeepest densification is in the root region reaching0.4-0.5 mm. On the flank the densification depth isapproximately 0.2 mm.2mmFigure 3. Metallographic

36、cross section of thesurface densified spur gear.Figure 4. Metallographic cross section of thesurface densified helical gear.Gear qualityThe gear quality obtained for the two gears areshown in table 3. The quality of the spur gear afterrollingisestimatedtoDINquality8.Thereisonepa-rameter that falls o

37、utside DIN 8. The total profiledeviation reaches 26 mm and the requirement forDIN 8 is 25 mm. DIN 9 allows 36 mm of total profiledeviation. The gear quality ofthe helicalgear isDIN8 or better.4Table 3. Measured gear quality after rolling.Spur PMgearHelicalPM gearProfileForm deviation ff?88Angular de

38、viation FH?68Total deviation F?9* 7HelixForm deviation ff?78Profile deviation fH?77Total deviation F?87Single normal pitchdeviationfu6 6Difference betweenadjacent pitchesfp74Total cumulative pitchdeviationFp55Cum. circular pitcherror over z/8 pitchesFpz/855Tooth thicknessvariationRs7 4Runout toleran

39、ce * Fr62* 1 mm from gear class 8* The gear bore is not used as reference. The rotationaxis is calculated by measurements on the tooth flanksConsistency of gear qualityMeasuring the diameter over balls before and afterrolling makes it possible to assess the consistencyof the rolling process. After h

40、obbing of the helicalgear the scatter in diameter over balls was approxi-mately 0.0225 mm as can be seen in Figure 5. Afterrolling the standard deviation dropped to 0.0031mm. The helical gear was also used to assess theconsistency in gear profile. Four teeth were mea-suredforeachgearandtheresultsare

41、plottedinthescatter diagram in Figure 6.Case hardeningThe hardness profiles for the tested gears areshown in Figures 7 and 8. The target case depth ontheflankwas0.7-1.2mmforthespurgearwhiletheprofiles for the helical gear had a target of 0.3 0.4mm. The case depth for the spur gear is 1.0 mmwhich is

42、well within the target range. The helicalgear had a higher surface hardness compared tothe reference gear. On the other hand it exhibits amore shallow case depth of approximately 0.5 mmcompared to 0.70 mm for the reference gear.74,3574,4074,4574,5074,5574,6074,650 1020304050Gear #Overballdiameter(mm

43、)before rollingafter rollingFigure 5. Scatter in diameter over ballsmeasurement before (diamonds) and afterrolling (circles). Scatterband3 m is indicatedby shadowing. Upper and lower tolerancesare shown as solid lines.0246810121416180 5 10 15 20 25Gear #DIN 9DIN 8DIN 7Profileformdeviation(ff)3 scatt

44、erbandFigure 6. Scatter in profile form deviation.Four teeth are measured on each gear.020040060080010000,0 1,0 2,0 3,0 4,0Distance from surface (mm)Hardness(HV0.1)PM spur gearReference spur gearFigure 7. Micro hardness profile for the spurgear.5020040060080010000 0,5 1 1,5 2 2,5Distance from surfac

45、e (mm)Hardness(HV0.1)Helical PM gearHelical reference gearFigure 8. Micro hardness profile for the helicalgear.Distortion after heat treatmentThe profile and lead traces of the helical HG-Crgear is shown in Figure 9. The hobbed gear has aquality of DIN 10 regarding the profile form devi-ation,whilee

46、.g.theprofileangulardeviation isquitegood at DIN 7. The lead errors are better betweenDIN 7 and 9. After rolling some improvements canbe seen. The profile form deviation has decreasedto DIN 8 near DIN 7, while the profile angular devi-ation is a DIN 8 near DIN 9. In the lead trace thechamfering can

47、be clearly seen. After heat treat-ment it can be seen that the profileform deviationisvirtually unaffected, while the profile angular devi-ation and the profile total deviation changes signifi-cantly. The lead trace shows a similar behavior inthat the helix form deviation is unaffected while theheli

48、x total deviation and helix angular deviationchanges slightly.DiscussionDensificationIdeally a larger densification depth would be pre-ferred. However, especially in the flank region it isdifficulttoreachdeeperdensificationdepthswithouttoo severe deformations. If too much densificationis attempted,

49、the work piece may break due to frac-tureofteethnearthetop.Thismayleadtobreakageof the rolling dies. In the present investigation wehave reached a densification depth of 0.5 mm forthe spur gear and 0.2 mm for the helical gear. How-ever, the densification depth isarbitrarily definedasthe depth where 2% porosity is reached. From acasehardeningpointofviewitissufficienttoreachastateofclosedporosity(around7.2g/cm3)werethematerialstartstobehavelikesolidsteel.Thisregionis significantly thicker in fact it is in the same rangeasthetarget

展开阅读全文
相关资源
猜你喜欢
  • AECMA PREN 4458-2000 Aerospace Series Studs MJ Threads in Titanium Alloy TI-P64001 MoS2 Coated with Serrated Locking Ring in Corrosion Resisting Steel Strength Class 1 100 MPa (at .pdf AECMA PREN 4458-2000 Aerospace Series Studs MJ Threads in Titanium Alloy TI-P64001 MoS2 Coated with Serrated Locking Ring in Corrosion Resisting Steel Strength Class 1 100 MPa (at .pdf
  • AECMA PREN 4459-2000 Aerospace Series Studs in Titanium Alloy TI-P64001 with Serrated Locking Ring in Corrosion Resisting Steel Design Standard Edition P 1《航空航天系列.带有耐腐钢齿形锁紧环的TI-P64.pdf AECMA PREN 4459-2000 Aerospace Series Studs in Titanium Alloy TI-P64001 with Serrated Locking Ring in Corrosion Resisting Steel Design Standard Edition P 1《航空航天系列.带有耐腐钢齿形锁紧环的TI-P64.pdf
  • AECMA PREN 4460-2000 Aerospace Series Studs in Titainium Alloy TI-P64001 with Serrated Locking Ring in Corrosion Resisting Steel Installation and Removal Procedure Edition P 1《航空航天.pdf AECMA PREN 4460-2000 Aerospace Series Studs in Titainium Alloy TI-P64001 with Serrated Locking Ring in Corrosion Resisting Steel Installation and Removal Procedure Edition P 1《航空航天.pdf
  • AECMA PREN 4461-1999 Aerospace Series Steel FE-PM1506 (X5CrNiMoAl13-8-2) Vacuum Induction Melted and Consumable Electrode Remelted Solution Treated and Precipitation Treated Bar a n.pdf AECMA PREN 4461-1999 Aerospace Series Steel FE-PM1506 (X5CrNiMoAl13-8-2) Vacuum Induction Melted and Consumable Electrode Remelted Solution Treated and Precipitation Treated Bar a n.pdf
  • AECMA PREN 4462-1999 Aerospace Series Steel FE-PM1506 (X5CrNiMoAl13-8-2) Vacuum Induction Melted and Consumable Electrode Remelted Solution Treated and Precipitation Treated Bar a n.pdf AECMA PREN 4462-1999 Aerospace Series Steel FE-PM1506 (X5CrNiMoAl13-8-2) Vacuum Induction Melted and Consumable Electrode Remelted Solution Treated and Precipitation Treated Bar a n.pdf
  • AECMA PREN 4463-1999 Aerospace Series Steel FE-PM1506 (X5CrNiMoAl13-8-2) Vacuum Induction Melted and Consumable Electrode Remelted Solution Treated and Precipitation Treated Bar a n.pdf AECMA PREN 4463-1999 Aerospace Series Steel FE-PM1506 (X5CrNiMoAl13-8-2) Vacuum Induction Melted and Consumable Electrode Remelted Solution Treated and Precipitation Treated Bar a n.pdf
  • AECMA PREN 4464-1999 Aerospace Series Steel FE-PM1506 (X5CrNiMoAl13-8-2) Vacuum Induction Melted and Consumable Electrode Remelted Solution Treated and Precipitation Treated Forginr.pdf AECMA PREN 4464-1999 Aerospace Series Steel FE-PM1506 (X5CrNiMoAl13-8-2) Vacuum Induction Melted and Consumable Electrode Remelted Solution Treated and Precipitation Treated Forginr.pdf
  • AECMA PREN 4465-1999 Aerospace Series Steel FE-PM1506 (X5CrNiMoAl13-8-2) Vacuum Induction Melted and Consumable Electrode Remelted Solution Treated and Precipitation Treated Forginr.pdf AECMA PREN 4465-1999 Aerospace Series Steel FE-PM1506 (X5CrNiMoAl13-8-2) Vacuum Induction Melted and Consumable Electrode Remelted Solution Treated and Precipitation Treated Forginr.pdf
  • AECMA PREN 4466-1999 Aerospace Series Steel FE-PM1506 (X5CrNiMoAl13-8-2) Vacuum Induction Melted and Consumable Electrode Remelted Solution Treated and Precipitation Treated Forginr.pdf AECMA PREN 4466-1999 Aerospace Series Steel FE-PM1506 (X5CrNiMoAl13-8-2) Vacuum Induction Melted and Consumable Electrode Remelted Solution Treated and Precipitation Treated Forginr.pdf
  • 相关搜索

    当前位置:首页 > 标准规范 > 国际标准 > 其他

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1