The Study of Half-tooth Master Gear Structure Optimization Yazhou Xie a, Zhiliang Qian b

Similar documents
Finite Element Modal Analysis of Twin Ball Screw Driving Linear Guide Feed Unit Table

Dynamic Characteristics of the End-effector of a Drilling Robot for Aviation

STRESS ANALYSIS OF BICYCLE PADDLE AND OPTIMIZED BY FINITE ELEMENT METHOD. S. Abeygunasekara 1, T. M. M. Amarasekara 2

KISSsoft 03/2016 Tutorial 9

FEA ANALYSIS OF PRESSURE VESSEL WITHDIFFERENT TYPE OF END CONNECTIONS

Design and Analysis of Rotary Lawn Mower

Fatigue Life Evaluation of Cross Tubes of Helicopter Skid Landing Gear System

Analysis of Shear Lag in Steel Angle Connectors

The Relationship between the Depth Embedded Pipe Pile and the Force of Clamping Jaw

Center Distance Change of Silent Chain Drive Effect on Sprocket Tooth Profile Modification Wei Sun 1,a, Xiaolun Liu 1,b, Jiajun Liu 1 and Wei Zhang 1

Lateral Load Analysis Considering Soil-Structure Interaction. ANDREW DAUMUELLER, PE, Ph.D.

Structural Analysis of Mast of Special Rotary Drilling Rig for Transmission Line

Sample Solution for Problem 1.a

67. Sectional normalization and recognization on the PV-Diagram of reciprocating compressor

σ = force / surface area force act upon In the image above, the surface area would be (Face height) * (Face width).

Analysis of Steady-state Characteristics of Aerodynamic Bearing Based on FLUENT JIA Chenhui 1,a, Du Caifeng 2,b and QIU Ming 3,c

Tightening Evaluation of New 400A Size Metal Gasket

Design and Analysis of Pressure Safety Release Valve by using Finite Element Analysis

Modal Analysis of Propulsion Shafting of a 48,000 tons Bulk Carrier

The Application of ANSYS Contact Analysis in Cable Crane Load Conversion Device

Gear hobs Accuracy requirements

Investigation of Stresses in Ring Stiffened Circular Cylinder

COMPUTATIONAL FLOW MODEL OF WESTFALL'S LEADING TAB FLOW CONDITIONER AGM-09-R-08 Rev. B. By Kimbal A. Hall, PE

Keywords: contra-rotating fan, air pressure, deformation of blades.

machine design, Vol.6(2014) No.3, ISSN pp

Modal Analysis of Barrels for Assault Rifles

STRESS ANALYSIS OF RATCHET PAWL DESIGN IN HOIST USING FINITE ELEMENT ANALYSIS

Numerical simulation of radial compressor stages with seals and technological holes

New Highly Productive Phased Array Ultrasonic Testing Machine for Aluminium Plates for Aircraft Applications

Design and Optimization of Weld Neck Flange for Pressure Vessel

Preliminary study of moored power cables

Novel empirical correlations for estimation of bubble point pressure, saturated viscosity and gas solubility of crude oils

Available online at ScienceDirect. Procedia Engineering 84 (2014 )

Research on ESC Hydraulic Control Unit Property and Pressure Estimation

Optimize Nozzle Location For Minimization Of Strees In Pressure Vessel

Vibration Analysis and Test of Backup Roll in Temper Mill

Engineering Practice on Ice Propeller Strength Assessment Based on IACS Polar Ice Rule URI3

FEA case Study: Rubber expansion joint for piping systems

Stress evaluation of a bicycle crank arm connection using BEM

Mechanical Stabilisation for Permanent Roads

Study on the shape parameters of bulbous bow of. tuna longline fishing vessel

Elastic-Plastic Finite Element Analysis for Zhongwei--guiyang Natural Gas Pipeline Endangered by Collapse

Journal of Chemical and Pharmaceutical Research, 2016, 8(6): Research Article. Walking Robot Stability Based on Inverted Pendulum Model

DESIGN OPTIMIZATION OF WORK ROLL CHOCK AND BACKUP ROLL CHOCK IN COLD ROLLING MILL

Modeling of Hydraulic Hose Paths

Optimization of rotor profiles for energy efficiency by using chamber-based screw model

Calibration and Validation of the Shell Fatigue Model Using AC10 and AC14 Dense Graded Hot Mix Asphalt Fatigue Laboratory Data

Coupling and Analysis of 981 Deep Water Semi-submersible. Drilling Platform and the Mooring System

Aerodynamic Performance of Trains with Different Longitudinal Section Lines under Crosswind

An Indian Journal FULL PAPER ABSTRACT KEYWORDS. Trade Science Inc.

Numerical simulation of three-dimensional flow field in three-line rollers and four-line rollers compact spinning systems using finite element method

METROLOGY LAB. I DEVICES BASED ON VERNIER SCALE


STUDY OF UNDERWATER THRUSTER (UT) FRONT COVER OF MSI300 AUTONOMOUS UNDERWATER VEHICLE (AUV) USING FINITE ELEMENT ANALYSIS (FEA)

PRESSURE DISTRIBUTION OF SMALL WIND TURBINE BLADE WITH WINGLETS ON ROTATING CONDITION USING WIND TUNNEL

ENTUCKY RANSPORTATION C ENTER. College of Engineering

An Innovative Solution for Water Bottling Using PET

Study to Establish Relations for the Relative Strength of API 650 Cone Roof Roof-to-Shell and Shell-to- Bottom Joints

WIND-INDUCED LOADS OVER DOUBLE CANTILEVER BRIDGES UNDER CONSTRUCTION

United States Patent (19) shikawa

Analyses of the fuel cell stack assembly pressure

RELIABILITY ASSESSMENT, STATIC AND DYNAMIC RESPONSE OF TRANSMISSION LINE TOWER: A COMPARATIVE STUDY

Structural Design and Analysis of the New Mobile Refuge Chamber

Linear Compressor Suction Valve Optimization

A COMPARATIVE STUDY OF MIX FLOW PUMP IMPELLER CFD ANALYSIS AND EXPERIMENTAL DATA OF SUBMERSIBLE PUMP

Design Project 2 Sizing of a Bicycle Chain Ring Bolt Set ENGR 0135 Sangyeop Lee November 16, 2016 Jordan Gittleman Noah Sargent Seth Strayer Desmond

Cost reduction for conveyor systems through self-adjusting chain wheel

Modeling of thin strip profile during cold rolling on roll crossing and shifting mill

Computer Aided Drafting, Design and Manufacturing Volume 26, Number 2, June 2016, Page 53. The design of exoskeleton lower limbs rehabilitation robot

Design and Static Structural Analysis of Cylinder and Piston of Two Stage Reciprocating Compressors Using ANSYS

OPTIMIZATION OF SINGLE STAGE AXIAL FLOW COMPRESSOR FOR DIFFERENT ROTATIONAL SPEED USING CFD

Finite Element Analysis of an Aluminium Bike Frame

ISO INTERNATIONAL STANDARD

Hardware Triaxial and Consolidation Testing Systems Pressure Measurement and Control

The Criticality of Cooling

Design Guide MSW from M20 to M70. Original version of the design guide

A parametric study of metal-to-metal contact flanges with optimised. geometry for safe stress and no-leak conditions

Faults Diagnosis and Design of the Sprockets for Dispenser in Ginning Industries

Combined impacts of configurational and compositional properties of street network on vehicular flow

Effects of Changes of Spokes in the Operation of a Rimmed Flywheel

A Chiller Control Algorithm for Multiple Variablespeed Centrifugal Compressors

Analysis and Optimization of Stress on Horizontal Pressure Vessel by Varying Opening Angle and Location

NUMERICAL SIMULATION OF STATIC INTERFERENCE EFFECTS FOR SINGLE BUILDINGS GROUP

A NEW GOLF-SWING ROBOT MODEL UTILIZING SHAFT ELASTICITY

International Journal of Modern Trends in Engineering and Research e-issn No.: , Date: 2-4 July, 2015

Numerical simulation on down-hole cone bit seals

DESIGN AND MANUFACTURING OF A MORPHING FLAP FOR WIND TURBINE BLADES

APPLICATION OF PUSHOVER ANALYSIS ON EARTHQUAKE RESPONSE PREDICATION OF COMPLEX LARGE-SPAN STEEL STRUCTURES

The 9th International Symposium on Automation and Robotic in Construction June 3-5,1992 Tokyo, Japan

(12) Patent Application Publication (10) Pub. No.: US 2005/ A1

Research on Small Wind Power System Based on H-type Vertical Wind Turbine Rong-Qiang GUAN a, Jing YU b

Hermetic Compressor Manifold Analysis With the Use of the Finite Element Method

FINITE ELEMENT ANALYSIS OF BICYCLE WHEEL

DOE Golfer Experiment

STRESS ANALYSIS OF BELL CRANK LEVER

Inlet Swirl on Turbocharger Compressor Performance

The Study on the Influence of Gust Wind on Vehicle Stability Chen Wang a, Haibo Huang b*, Shaofang Xu c

DEPARTMENT OF THE NAVY DIVISION NEWPORT OFFICE OF COUNSEL PHONE: FAX: DSN:

World Journal of Engineering Research and Technology WJERT

Tutorial on Flange Qualification using CAEPIPE

Transcription:

X 3rd International Conference on Mechatronics, Robotics and Automation (ICMRA 2015) The Study of Half-tooth Master Gear Structure Optimization Yazhou Xie a, Zhiliang Qian b School of Mechanical and Electric Engineering, Soochow University, China, 215006 a e-mail: 1401785122@qq.com, b e-mail: qianzhiliang@suda.edu.cn Key words: Half-tooth master gear; Tooth; deformation; Depth of half-tooth groove; Empirical equation Abstract. Aimed at the half-tooth master gear which is used for single and double flank gear roll testing synchronously. By gear structure analysis, it was discovered that the half-tooth groove depth is the main factor to determine gear tooth stiffness. On the basis, through the finite element analysis of gear with same module and several half-tooth groove depths, the relation between the maximal gear tooth deformation and the half-tooth groove depth was obtained and the optimal half-tooth groove depth corresponding the minimal gear tooth deformation was deduced. Then optimal half-tooth groove depths of several gears with different modules were obtained by the above methods, and an empirical equation was found by which the optimal half-tooth groove depth of a gear can be determined according to its module. Finally, the accuracy and applicability of the empirical equation were verified by example. Introduction Single and double flank gear roll testing are two common gear measuring methods.but measuring principle, measuring elements and measuring results of the two testing are different, and the master gears and measuring instruments used by the two testing are also different, cannot be used interchangeably. Half-tooth master gear is an original gear with distinctive structure [1]. Two half-tooth master gears can make up a variable-tooth-thickness master gears by which single and double flank gear roll can be tested synchronously, and radial composite deviation and tangential composite deviations of both tooth flanks can be obtained with an instrument and one measuring process[1,2]. This article studied structure optimization of half-tooth master gear to improve its stiffness and applicability. Tooth Stiffness of the Half-tooth Master Gear Structure of the Half-tooth MasterGgear. Half-tooth master gear(fig. 1) has following features: it only preserve half of traditional gear tooth on the cross section, the other half and partial gear body are cut off to form half-tooth groove; it only preserve half of the traditional gear s spoke and hub on the axial section, the half on the other side of axial symmetric plane is cut off to form a cavity. Obviously, tooth of half-tooth master gear is cantilever-like, its stiffness is evidently weaker than the traditional gear tooth. half-tooth half-tooth groove Fig.1.Half-tooth master gear Fig.2. Depth of half-tooth groove X Factors Influencing Tooth Stiffness.Because a variable-tooth-thickness master gears are comprised of two half-tooth master gears, the spoke and hub of half-tooth master gaer on one side of axial symmetric plane must be cut off to form a cavity. That means tooth of half-tooth master gear mst be cantilever-like in half a tooth width along axial direction. Thus, the depth of half-tooth groove X is the variable structure parameter only (Fig. 2). Obviously, the cross-sections of tooth overhung end and half-tooth groove on a half-tooth master gear are 2015. The authors - Published by Atlantis Press 1280

identical in shape. With other conditions being same, the depth of half-tooth groove X directly decides the shape and size of gear tooth overhung end, and sequentially it will directly affect the gear tooth stiffness. Influence of Tooth Deformation.Under the same loading condition, the weaker the gear stiffness, the more serious the deformation of gear tooth [3]. In the process of single and double flank gear roll testing synchronously, the load deformation of master gear tooth can be transmitted to tangential and radial composite deviation s of product gear, and directly affects the accuracy of measuring result. Analysis Method of Tooth Deformation Analysis Method of Tooth Deformation. Computing gear tooth stiffness, gear tooth is usually simplified as variable cross-section cantilever beam. However, half-tooth master gear tooth is cantilevered along radial and axial directions, the problem of its stiffness is far more complicated than the traditional gear tooth s. The computing method of traditional gear tooth stiffness can t be applied here. In view of that the functions of CAE software have been quite perfect and the accuracy of its analysis results has also been verified by lots of engineering examples. The half-tooth master gear tooth stiffness is analyzed by ANSYS workbench in this article. The specific methods are as follows: 1) Under the same constraint and load conditions, the half-tooth master gears with different depths of half-tooth groove are analyzed by ANSYS workbench, and tooth deformation values of gears with different depths of half-tooth groove are obtained. 2) The discrete deformation data are fitted and analyzed to obtain the optimal half-tooth groove depth X m with which the gear tooth deformation is minimum. 3) Repeat steps 1) and 2) for the half-tooth master gears with different modules tp find out the relationship between X m and gear module M. Settings of Gear Deformation Analysis.The deformation of half-tooth master gear is affected not only by gear structure, but also by gear material, constraints and loads, and so on. In this article, the half-tooth master gear tooth deformation is analyzed by ANSYS workbench under following specific settings:: 1) Gear material and material properties. The half-tooth master gear belongs to high-precision and wearable master gears, 38CrMoAlA is selected as gear material according to Gear Design Manual[4], elasticity modules and Poisson's ratio are set respectively as 2.09 105N/mm2 and 0.3. After gear material is selected, physical properties of material can be inherited directly by the solid model of the component. 2) Mapped Meshing. In order to obtain the higher precision of analysis and consider the computation speed, set the mapped meshing size as 2mm and the element as tetrahedron unit in this article. 3) Constraint Condition. Restrain six freedom degrees of the axle hole on the half-tooth master gear. Set the constraint of the axis hole as fixed support. 4) Contact Load. During the roll testing of master gear and product gear, the contact load acted on gearing flanks only needs to overcome the friction in supporting shafts and gearing flanks, the specific load value is relevant to the structure of the gear roll testing instrument. On the other hand, the article studies the influence of half-tooth master gear structure on gear tooth stiffness through analyzing the deformation of gears with different depth of half-tooth groove under the same contact load. In the elastic range, the magnitude of load can change the value of tooth deformation, can t change the relation between tooth deformation and gear structure. Thus, the article sets contact load as 10N in the following deformation analyses,. 5) Acting Location and Acting Mode of Load. In the deformation analyses, the contact force is set as concentrated load and it is acted at the top point of tooth overhung end, the acting direction of force is perpendicular to tooth flank. During gear roll testing, the root defect of product gear tooth end(for example, convex burr) will produce the above loading effect on master gear. Meanwhile, this is the worst loading situation for the deformation of half-tooth master gear. The Relationship Between Module and Optimal Depth of Half-tooth Groove The half-tooth master gear posesses particular structure(fig. 1), its tooth is overhung along both axial and radial directions, and the cantilever length L along radial direction is equal to the depth of half-tooth groove X (Fig. 2). The longer the depth of half-tooth groove X, the larger the cross section area of overhung gear tooth 1281

A, and the longer the cantilever length L (Fig. 3). Obviously, the increase of A can improve the stiffness of tooth overhung end, and the increase of L will reduce rasial bending stiffness of gear tooth. Giving consideration to both, there is an optimal depth of half-tooth groove X m which will make the gear deformation minimal at the same load. Namely, it will make the gear tooth stiffness (the overhung end of gear tooth) maximal. Then, this article studies the relationship between module M and the optimal depth of half-tooth groove X m with the above analysis methods. Table 1 The maximal deformationy Fig.3.The radial cantilever length L X[mm] Y[μm] 8 38.065 10 24.753 12 19.712 14 17.696 16 16.945 18 17.077 20 17.758 22 19.033 24 21.044 The Optimal Depth of Half-tooth Groove underspecific Module. For the half-tooth master gear of which module M, pressure angle, number of teeth, addendum coefficient and tooth width respectively equals to 3[mm], 20, 30, 1.0 and 60[mm], the article establishes the nine models with nine different depth of half-tooth groove X i, and analyzes the maximal comprehensive deformation of the tooth overhung end by ANSYS workbench. The maximal comprehensive deformation Y of tooth overhung end related to the different depth of half-tooth groove X is shown in Table 1. The data in Table 1 are fitted according to the least square sextic polynomial fitting by Matlab., The fitting equation and the relationship curve between the depth of half-tooth groove X and the maximal comprehensive deformation Y are obtained and respectively shown as Eq.1 and Fig.4. Y ( X = 0.000018106 X -1.9889 X 3 6-0.0019263 X + 26.2370 X 2 5 + 0.084918X -186.2500X + 577.8600 It is obvious in Fig.5 that there is an optimal depth of half-tooth groove X m with which the maximal tooth deformation is minimal. This article analyzes Eq.1 is analyzed by Matlab and the optimal depth of half-tooth groove X m is obtained. The optimal depth Xm is equal to 16.713[mm]. 4 (1) Fig.4 Y&X for gear with module 3[mm] Fig.5 Relationship between X m and M 1282

Optimal Depth of Half-tooth Groove under Different Module. Maintaining the above parameters except module unchanged, the article analyzes the half-tooth master gaers of which module is respectively equal to 4,5,6,and 8[mm] and obtains the optimal half-tooth depths of the gaers. The optimal depths of gears with different module is shown in Table 2.. The Relationship Between Module and the Optimal Depth. In order to reveal the relationship between module M and the optimal depth of half-tooth groove X m, this article fits the optimal half-tooth groove depths X m related to modules 3, 4, 5, 6 and 8[mm] with the least square linear fitting. The fitted relationship between module and the optimal half-tooth groove depth is shown as Fig.5. The fitted equation is as following: X m = 2.7521M + 8.7711 (2) There is the good linear relationship between module and the optimal half-tooth groove depth as shown in Fig.5. Eq.2 has fitting degree up to 0.9959 and can be used as the empirical equation to determine the depth of half-tooth groove. Utilizing the equation, the approximate optimal depth of half-tooth groove X m, with which the half-tooth master gear will posess approximatively maximum stiffness, can be directly determined according to the gear module M. Application Example and Verification Design a half-tooth master gear with the objective of maximum tooth stiffness, the module of gear is 7[mm], other parameters are the same as the above. Design According to the Empirical Equation. Substitute M=7[mm] into Eq.2, and abtains the approximate optimal half-tooth groove depth X ma : X ma = 2.7521M + 8.7711 = 2.7521 7 + 8.7711= 28.0358[ mm]. Design According to above AnalysisMethod. With the half-tooth groove depth X being respectively equal to 20, 22, 24, 26, 28, 30, 32, 34 and 36[mm], the models are built and analyzed according to above analysis method, and the maximal comprehensive deformation Y under different half-tooth groove depth X are obtained as shown in Table 3. It can be seen from Table 3 that the gear deformation is minimal when the depth of half-tooth groove X is 28[mm], which is accordant to the approximate optimal half-tooth groove depth X ma obtained by Eq.2. Besides, fitting the data in Table 3 and evaluating its optimal value following above methods, it is obtained that the optimal depth of half-tooth groove X m equals 27.407[mm], which is very close to the optimal depth of half-tooth groove X ma obtained from Eq.2. Conclusion Table 2 The optimal depth X m M[mm] X m [mm] 4 19.821 5 23.098 6 25.138 8 30.641 Table 3 Y&X under module M=7[mm] X(mm) 20 22 24 26 28 30 32 34 36 Y(μm) 2.666 2.457 2.326 2.276 2.263 2.277 2.325 2.408 2.505 Through the finite element analysis of the gear with same module and different half-tooth groove depth, the variation of the maximal gear tooth deformation with the half-tooth groove depth is obtained. Moreover the optimal half-tooth groove depth under which the gear tooth deformation will be minimal is deduced. And then, following the above analysis methods, several optimal half-tooth groove depths of several gears with different module are also obtained. From this, an empirical equation is established through the least square method linear fitting, the optimal half-tooth groove depth can be determined according to gear module by above equation. At last, the usage of this empirical equation is given, and the accuracy and applicability of the equation are also verified by an example. 1283

References 1. A Type of Measuring Gear & Measuring Method, ZL201210255341.4, 2014-12-01 2. Xinmiao Yu, Zhiliang, Qian, et al. New Kind of Master Gear and Measurement Principle for Gear Composite Deviations[J], New Technology & New Process, 2013.7:20-22 3. Xiongxiong Lu, Zhiliang Qian, et al. Design and Stiffness Verification of a New Type of Measuring Gear[J], New Technology & New Process, 2013.7:53-56 4. Xiaolu Zhu. Gear Design Manual(second edition). Chemical Industry Press,2010 1284