AGMA 10FTM06-2010 Finite Element Analysis of High Contact Ratio Gear《高重合度齿轮的有限元分析》.pdf
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1、10FTM06AGMA Technical PaperFinite Element Analysisof High Contact RatioGearBy M. Rameshkumar, G.Venkatesan and P. Sivakumar,DRDO, Ministry of DefenceFinite Element Analysis of High Contact Ratio GearM. Rameshkumar, G. Venkatesan and P. Sivakumar, DRDO, Ministry of DefenceThe statements and opinions
2、contained herein are those of the author and should not be construed as anofficial action or opinion of the American Gear Manufacturers Association.AbstractModern day vehicles demand higher load carrying capacity with less installed volume and weight. The gearsused in the vehicles should also have l
3、esser noise and vibration. Even though helical gears will meet therequirement, they are prone for additional axial thrust problem. High contact ratio (HCR) is one such gearingconcept used for achieving high load carrying capacity with less volume and weight. Contact ratio greater than2.0 in HCR gear
4、ing results in lower bending and contact stresses. Previously published literature deal withstudies on various parameters affecting performance of HCR gears but a comparison of HCR and normalcontact ratio (NCR) gears with same module and center distance has not been carried out so for. This paperdea
5、ls with finite element analysis of HCR, NCR gears with same module, center distance and the comparisonof bending, contact stress for both HCR, NCR gears. A two dimensional deformable body contact model ofHCR and NCR gears is analyzed in ANSYS software. ANSYS Parametric Designlanguage (APDL) is usedf
6、orstudying the bending and contact stress variation on complete mesh cycle of the gear pair for identical loadconditions. The study involves design, modeling, meshing and post processing of HCR and NCR gears usingsingle window modeling concept to avoid contact convergence and related numerical probl
7、ems.Copyright 2010American Gear Manufacturers Association500 Montgomery Street, Suite 350Alexandria, Virginia, 22314October 2010ISBN: 978-1-55589-981-33Finite Element Analysis of High Contact Ratio GearM. Rameshkumar, G. Venkatesan and P. Sivakumar, DRDO, Ministry of DefenceIntroductionA majority of
8、 the heavily loaded transmissions usedin military applications use gears with a contact ratioless than 2.0. The contact ratios of these transmis-sions are in the range of 1.3 to 1.8. So, the numberof teeth in engagement at any instant is either one ortwo. Many gear designs use increased pressureangl
9、e for increasing the load carrying capacity ofgears with fixed module and center distance, but thecontact ratio decreases. Tooth dynamic loads andnoise increase due to decreased pressure angle.Hence increasing the load carrying capacity ofgears for the above conditions can be done by thedesign of ge
10、ars with a contact ratio greater than 2.0.High contact ratio gears having a contact ratiogreater than 2.0 have load sharing between two orthree teeth during engagement and less load pertooth 1. The high contact ratio (HCR) gearsguarantees that a minimum of two teeth alwaysshare the load. The variati
11、on of gear mesh stiffnessfor HCR gears is less than the normal contact ratio(NCR) gears; the transmission error for HCR gearsis minimum compared to NCR gears.The literature survey indicated that HCR gearingwas designed 2 and successfully used in heli-copter transmissions 3, to improve power toweight
12、 ratio of the gear trains. This study deals withestimation and comparison of tooth root bendingstress and contact stress over the path of contactfor high contact ratio gears 1, 4 and normal contactratio gears designed with identical module, centerdistance, gear ratio and face width using FiniteEleme
13、nt Analysis. In order to overcome the numer-ical and convergence difficulties 5 involved a newsingle window modeling approach 6 using ANSYSParametric Design Language (APDL). The contactstress and bending stress are compared and plottedfor identical load conditions.Design for HCR gear pairContact rat
14、io of a gear pair is defined as the averagenumber of teeth in contact during the course of en-gagement. The contact ratio of the gear pair playsan important role in increasing the load carrying ca-pacity of gears.The contact ratio (CR) for any gear pair is given byequation 1.+r2+ a2 r22cos2r1+ r2sin
15、 m cosCR =r1+ a2 r21cos2 m cos(1)wherer1,r2are the operating pitch radius of the pinionand gear, is the operating pressure angle;m is the module and a is the addendum(based on the operating pitch radius)which is equal to one module for standardgears.High contact ratio can be achieved by different wa
16、ysnamely:S Increasing the number of teeth;S Lowering the pressure angle;S Increasing the addendum factor.Figure 1, Figure 2 and Figure 3 show the variationsof contact ratio with respect to above parameters.In order to achieve a contact ratio more than 2.0 fora gear pair with identical module, center
17、 distance,gear ratio and pressure angle the addendum factorof the gears pair is increased from a standard 1.0 mto 1.25 m. The entire tooth parameters of a HCRgear pair are calculated using a Matlab code andtabulated in Table 1.4Figure 1. Contact ratio versus number ofteethFigure 2. Contact ratio ver
18、sus pressure angleFigure 3. Contact ratio versus addendumfactorGeneration of gear pair modelSpur gear geometryThe profile of an involute spur gear tooth is com-prised of two curves. The working portion is the in-volute and the fillet portion is the trochoid. Thetrochoid tooth fillet as generated by
19、a rack cutter ismodeled exactly using the procedure suggested byBuckingham 7. An “APDL” computer languagecode in ANSYS was developed for generating anexact tooth profile with a trochoidal fillet. The troch-oidal fillet form is generated from the dedendumcircle up to the limiting circle, where it mee
20、ts the in-volute profile at the common point of tangency andthe involute profile extends up to the addendumcircle.Table 1. Gear parametersSI No. Parameters NCR HCR1. Profile Involute Involute2. DIN accuracy class 7 73. Module, m 2.5 mm 2.5 mm4. Number of teeth ingear, Z150 505. Number of teeth inpin
21、ion, Z247 477. Profile correction ingear, X10.1552 0.15528. Profile correction inpinion, X20.152 0.15210. Center distance, Cd122 mm 122 mm11. Reduction ratio, Gr1.06383 1.0638312. Addendum factor,Ya1.0 1.2513. Contact ratio, CR 1.6860 2.0626614. Face width, F 18 mm 18 mmFigure 4 shows generation of
22、a trochoidal fillet bythe tip of the basic rack with a = 0 (sharp cutter).Coordinates of the trochoid are calculated using theAPDL program using equation 2 through 8 as notedin 7. The type of Trochoidal fillet changes withparameters of the cutter like type of cutter (pinion orrack), edge radius (a),
23、 addendum (b), pressureangle and profile correction required in the gear.t= tan1R2t (R b)2(R b)R2t (R b)2R(2)tan t=RR b2 R2tRR2tR b22(3)5Figure 4. Trochoid profile generationThe co-ordinates of the actual fillet are determinedfrom:Rf= R2t+ A2 2 ARtsint(4)f= t+ cos1Rt A sintRf (5)xi= Rfsin f(6)yi= Rf
24、cos f(7)f= t+ f(8)whereA is the cutter tip edge radius;b is the distance between the pitch line ofthe cutter and the center of the outeredge;R is the operating pitch circle radius;Rt,Rfis the radius vector of the trochoid and rootfillet; is the angle between the radius vector andtangent to trochoid;
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