Design Optimization in Rotary Tillage Tool System

Abstract—The design optimization of rotary tillage tool by the application of Computer Aided Engineering (CAE)-Techniques on the basis of finite eleme...

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International Journal of Environmental Science and Development, Vol. 3, No. 3, June 2012

Design Optimization in Rotary Tillage Tool System Components by Computer Aided Engineering Analysis Gopal U. Shinde and Shyam R. Kajale a solid (3-D) model is prepared in CAD-software such as Ansys, Catia, Pro-E, Hyper-mesh etc. by assembling individual parts with detail specifications.

Abstract—The design optimization of rotary tillage tool by the application of Computer Aided Engineering (CAE)-Techniques on the basis of finite element method and simulation method is done by using CAD-Analysis software for the structural analysis. The different tillage tool parts of rotary tillage tools are geometrically constrained by the preparation of solid model, Meshing and Simulation is done with actual field performance rating parameters along with boundary conditions .The energy constrained for the tillage tool applications with 35Hp and 45Hp power tractor and estimated forces acting at soil-tool interface. The resultant effect on tillage blade and whole rotavator assembly is obtained from stress distribution and deformations plots.The proposed work results in identifying sufficient tolerance in changing the dimensions of rotavator frame sections and side gear box for removing the excess weight in a solid section and also to raise the weight of blade for a reliable strength. The present working model with tillage blade is analysed to new design constraints with change of its geometry for the maximum weed removal efficiency by presenting its practical results from the field performance.

A. Rotavator Assembly Consists of Following Parts 1) Independent Top Mast 2) Single / Multi Speed Gear Box 3) Chain / Gear Cover Part Flange 4) Blades 5) Chain / Gear Cover Part 6) Frame and Cover 7) Adjustable depth skids 8) Offset adjustable frame B. CAD Model of Rotavator The CAD-Software is used for the preparation of solid geometry of rotavator according to specification see Fig.1.

Index Terms—Rotary tillage tool, weed removal efficiency, CAD-Analysis, simulation, structural analysis, von misses stress

I. INTRODUCTION Rotary tiller is a tillage machine designed for preparing land suitable for sowing seeds (without overturning of the soil), for eradicating weeds, mixing manure or fertilizer into soil, to break up and renovate pastures for crushing clods etc. It offers an advantage of rapid seedbed preparation and reduced draft compared to conventional tillage. It saved 30-35 % of time and 20-25 % in the cost of operation as compared to tillage by cultivator. It gave higher quality of work (25-30 %) than tillage by cultivator. The design optimization of tillage tool is obtained by reducing its weight, cost and by improving a field performance to high weed removal efficiency .The computer aided design analysis by preparing a three-dimensional solid modelling and finite elements method applications are getting so widespread in the industry. Thus due to undesired stress distributions on its components, it cannot compensate to the operating forces i.e. field environment and results in breakdown and failure due to higher stresses and deformation. The proposed work develops a computer aided experimental system for design testing and valuation of agricultural tools and equipments. The selected physical model of rotavator is measured with accurate dimensions and

Fig. 1. Solid Model as per physical specifications

C. Finite Element Method The following are the three basic features of the finite element method. a) Division of whole into parts; which allows representation of geometrically complex domains as collection of simple domains that enable a systematic derivation of the approximation functions. b) Derivation of approximations functions over each element; the approximation functions are often algebraic polynomials that are derived using interpolation theory. c) Assembly of elements, which is based on continuity of the solution and balance of internal fluxes

Manuscript received November 11, 2011, revised April 18, 2012. Gopal U. Shinde is with Marathwada Agricultural University, Parbhani (M.S.) India (e-mail: [email protected]). .Shyam R. Kajale is with S.G.G. I. E.& T. Nanded (M.S.)India (e-mail: [email protected]).

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International Journal of Environmental Science and Development, Vol. 3, No. 3, June 2012

4. To make an engineering analysis of rotavator blade and -modify it with significant changes

D. CAD-Modeling and Analysis The three important steps in ANSYS programming used for CAD-modeling and analysis are: a) Preprocessing b) Solution c) Post processing After preparing a solid geometry of rotavator the important steps are meshing and applying loading and boundary conditions in the preprocessor so that simulation can be run to get a solution and generate results in the post-processor.

II. MATERIALS AND METHODS A. Material The materials are taken from the manufacturing database of rotavator production system specification drawn by Industry. The Material properties and Soil properties are considered according to following data in the Table I and II as given below.

E. Mesh Generation (Meshing) After validation of the model next step is generation of Finite Element Mesh. For the Rotavator SOLID45 elements are used for meshing. A very fine mesh of freedom of the model increases Hence a designer has to model it optimally i.e. placing fine mesh only at critical area; and coarse mesh at other. So that the run time is less and also the accuracy is not much affected.[2]

Sr. No. 1

F. Element Description 1) Solid 45 The solid meshing using SOLID-45 8 NODE 45 element, DOF: UX, UY, UZ Surface meshing by triangular 6 node element 1. Element edge length – 1.5 mm for crankshaft. Because in this, crankshaft model chamfer width is 3 mm, so for better results, we can take two elements in this area. 2. Element edge length- 2 mm for flywheel and Pulley. 2) Beam 188 BEAM188 has six or seven degrees of freedom at each node using BEAM 188 element DOF: UX, UY, UZ and rotation RX,RY,RZ The proposed work is taken for complete finite element analysis of rotavator tillage tool which introduces the use of CAD analysis for the first time in the design and development of Agricultural machine, tools and equipment. a)

2

Software Tools

Design Services

Mild Steel

2.10 X e

Sr. No. 1 2 3 4 5

Types of Soil sandy Sandy loam Slit loam clay Heavy loam

0.30

7.2 x e-9 7.89 x e-9

TABLE II: SOIL PROPERTIES: Optimum Moisture content Soil resistance (%) (Kg/cm2) 0.2 3.5 0.3 5.8 0.35 – 0.5 0.4 – 0.56 7.18 0.5 – 0.7 13.30

D. Modal analysis The frequencies at which vibration naturally occurs, and the modal shapes which the vibrating system assumes are properties of the system, and can be determined analytically using Modal Analysis. The following table shows an idea about fundamental natural frequencies and higher natural frequencies in Hz. Section 4.1 contains the deformation plot for individual component and assembly for below mention 10 different natural frequency.

Engineering Analysis

Extencore offer engineering analysis and use of CAE based solutions to customers with product development initiatives, to develop word class and reliable products[5],[6]. d)

3

7.48 x e-9

C. Element and Node Count in FE-Model Following table shows the total number of 2d and 3d elements obtained in FE model of rotavator [7], [8].

Extencore provide top of the line CAD/CAM design services for aircraft components, industrial equipment, Agricultural Implement and machine tool [3]. c)

5

Density (tons / mm2)

B. Soil Parameters The soil properties relevant to the design of rotavator were identified as soil type, moisture, bulk density and cone index. The manners of measurement and characterization of these properties are discussed in the following sections. The type of soil was black soil were experiment was conducted. Moisture content of soil plays an important role for the growth of the crop hence following Soil resistance and Moisture content of soil are considered as given in Table II.

CAE: Ansys, Nastran, Abacus, Hypermesh, Cosmos CAD: Catia, Solid-work, Solid-edge AutoCAD, CFD: Fluent, Ansys CFX, ICEM-CFD, b)

TABLE I: MATERIAL PROPERTIES: Material Properties Poisso Material Name Elastic Modulus n 2 (N/mm ) Ratio High Carbon 11 0.29 1.97 X e Steel 5 Cast Iron 1.20 X e 0.28

Objectives

III. RESULT AND CONCLUSIONS

1. To prepare a geometric solid model of rotavator by using -CAD-software 2. To make the finite meshing by using meshing software. 3. To generate a CAD analysis report of rotary tillage tool -components.

A rotary tillage tool such as Rotavator is designed in computer aided design software. The rotary motion and soil surface interaction is considered with respect to the soil Vs. tillage tool dynamics [7]by considering the following factors effecting the tillage operation such as tractor power (hp), 280

International Journal of Environmental Science and Development, Vol. 3, No. 3, June 2012

safety coefficients, displacement and Von Misses hp and 45 hp tractor rotavator see Table IV

maximum peripheral force (N), rotavator tyne velocity (m/s), tractor transmission efficiency (0.9 for concurrent revolution and 0.8-0.9 for reversed rotary), soil resistance to 0.7-0.8, radius of rotary (mm) see Table IV The design analysis executed following results • Maximum Peripheral force on rotary blade 6031.08975 (for35 hp)N and 7041.17 N (for 45hp) • Torque= 270600 N-mm(for35 hp)N and 315920 N-mm (see appendix-I) The Design analysis of rotavator results with an output file generated by simulation with respect to yield stress and deformation obtained by using field conditions in the Post processor. The CAE-Analysis Cycle, see APPENDIX-I

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TABLE IV: WORKING SAFETY COEFF. FOR 35 HP AND 45 HP TRACTOR INDEPENDENT TOP MAST; II) ROTOR WITH BLADE; III) SIDE GEAR BOX PART IV) FRAME AND COVER; V) LEFT SIDE FRAME; VI) RIGHT SIDE FRAME Resultant Von Misses Safety Von Misses Displacement Part Stress (Mpa) Coefficient Stress (Mpa) (mm) No. 35hp 45hp 35hp 45 hp 35hp 45 hp 35hp 45hp I 404.29 471.46 2.19 3.39 404.29 471.46 01.24 1.06 II 417.03 503.20 6.75 7.89 417.0 503.20 01.65 1.37 III 015.63 018.28 5.65 6.61 015.63 018.28 11.51 9.84 IV 016.86 019.67 6.52 7.89 016.86 019.67 10.67 9.15 V 056.26 065.61 6.58 7.68 056.26 065.61 03.20 2.75 VI 055.38 064.73 6.68 7.60 055.38 064.73 03.25 2.78

A. Modal Analysis The modal analysis as per above stated condition is done and the results obtained from the table 1 in Appendix VI, it is observed that, the maximum and minimum deformation of 1.923mm and 0.252mm respectively was observed in blade section. See Table III. TABLE III: MODAL ANALYSIS Frequency Max Deformation

for

Remark

Sr. No. (Hz) -2

(mm)

(Rotavator component)

1.

3.50509e

2.119

Top

2.

0.12474

1.682

Front left

3.

0.13638

1.449

Top Front

4.

0.16626

1.767

Front left

5.

0.18940

2.012

Bottom front

6.

0.22161

1.693

Bottom Front

7.

16.645

4.313

Front

8.

40.799

5.994

Front Corner

9.

56.556

2.883

Top Front

10

66.299

4.242

Bottom Front

B. Structural Analysis The structural analysis as per above stated condition is done and the results obtained from simulation [10] & [11], it is observed that 1. The displacement Vector Sum and Von Misses Stress is maximum at blade-section such as 6.757 mm and 417.03 Mpa respectively for 35 hp tractor 2. The displacement Vector Sum and Von Misses Stress is maximum at blade- section such as 7.893 mm and 503.21 Mpa respectively for 45 hp tractor[4], See Fig 2.

Fig. 2. Principle stress &Von misses stress in blade section

The Rotary tillage blade modified and physically tested in the field operation which was satisfactorily resulted with high weed removal efficiency and excellent soil bed performance.

C. Blade Analysis 1. The maximum Displacement vector sum in: 6.757mm ( 35 hp) and 7.893 mm(45 hp ) 2. The maximum Von Misses Stress: 417.03 Mpa( 35 hp) and 503.20 Mpa (45 hp) 3. The maximum principle stress for 35 hp tractor is 490 Mpa was observed in blade section. This stress value is less than yield stress of blade material i.e. 690 Mpa 4. The maximum principle stress for 45 hp tractor is 577 Mpa was observed in blade section. This stress value is less than yield stress of blade material i.e. 690 MpaWorking

Fig.3. Saw tooth angular blade of rotavator

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The reverse engineering concept for redesigning and conceptual modifications in the Blade was found to be significant in cereal inter crop secondary tillage operation Fig 3.above mentioned.

REFERENCES [1]

Akinci, I., D. Yilmaz, and M. Canakci. Failure of a Rotary Tiller Spur Gear. Engineering failure analysis, 12(3): 400- 404. (2005). [2] Altair Engineering. Inc, “Hypermesh Users Guide”, 2003 [3] Anonymous, (1971). Design data book. PSG college of Tech. Kalaikathir Publications, Coimbatore. [4] Ansys Inc, “ANSYS 8.1 Documentation, Structural Analysis Guide”, Swansos Analysis System, United state, 2004 [5] Bechly, M. E., and P. D. Clausent. (1997). “Structural Design of a Composite wind turbine blade using Finite Element Analysis”. Computers & Structures Vol. 63. No. 3, pp. 639-616. [6] Beeny, J. M., and D. C. Khoo. (1970). “Preliminary investigations in to the performance of different shaped blades for the rotary tillage of wet rice soil”. J. Agric. Engg. Res, 15 (1):27-33. [7] Ben Yahia, Logue, and M. Khelifi. (1999). “Optimum settings for rotary tools used for on-the-row mechanical cultivation in corn”. Transactions of ASAE, 15(6): 615-619. [8] David Roylance (2001). “Finite Element Analysis Method”. Department of Materials Science and Engineering Massachusetts Institute of Technology Cambridge, MA 02139 February 28 [9] Fielke, J. M, T. W. Reiley; M. G. Slattery and R. W. Fitzpatt. (1993). “Comparision of tillage forces and wear rates of pressed and cast cultivator shares”. Soil and Tillage Research, 25; 317-328. [10] Ghosh, B.N. (1967). “The power requirement of a rotary cultivator”. J. Agric. Engg. Res., 12 (1): 5-12. [11] Gill, W. R., and G. E. Vanden Berg. (1996). “Design of tillage tool. In soil dynamics in tillage and traction”. 211-294. Washington, D.C.,U.S.GPO

Fig. 4. Frequency Vs deformation

Gopal U. Shinde was born on 1971 in Parbhani,India. He completed his bachelor of Engineering on Production Engineering in 1994 from Dr.Babasaheb Ambedkar Marathwada University (Dr.B.A.M.U.) and Master’s degree in Mechanical Engineering (Manufacturing Process Engg) from IIT Kharagpur (W.B.) India. Currently Working as a Assistant Professor of Mechanical engg., Department of Farm Machinery and Power, College of Agricultural Engineering & Technology, Marathwda Agricultural University Parbhani(M.S.)India. He is a Member of scientific societies ISAE, ASABE, APBEES, AAAE, and IEI. He is CAD/CAM/CAE-Lab in-charge. He is a member of APBEES. His area of research is in CAD/CAM/CAE-Applications in Agricultural Engg.and Food engg.,Farm machiney and power,Agricultural process Engg.,Mechanization in Agriculture.

APPENDIX-I Computer aided design and engineering analysis of rotavator components

Shyam R. Kajale was born on 1959 in Mharashtra State, India. He completed his bachelor of Engineering on Mechanical Engineering in 1983 from Nagpur University. He is Master’s degree in Mechanical Engineering and the Docterate degree in Mechanical Engg. from IIT Kharagpur (W.B.)India. He is Currently Working as a Director, Shri Guru Gobind Singhji Institute of Engineering and Technology, Vishnupuri, Nanded (M.S.). He published more than 40 research papers and his area of Research is in Micro and on-Conventional Manufacturing, CAD/CAM, Process Modelling and Optimisation.

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