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IRJET- Design and Analysis of Progressive Die for Industrial Component Tail Gate Stricker
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1.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 08 | Aug 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 117 Design and Analysis of Progressive Die for Industrial Component Tail Gate Stricker Jayshree M. Gadhe1, A. Yadao2 1,2Department of Mechanical Engineering, G. H. Raisoni College of Engineeing & Management, Pune, India. ---------------------------------------------------------------------------***--------------------------------------------------------------------------- Abstract: In sheet metal manufacturing, Design and development of different components is one of the important phase. This is a highly complex process and leads to various uncertainties. These uncertainties can induce heavy manufacturing losses through premature die failure, final part geometric distortion and production risk. Progressive die is a press tool of collective operations performed on the sheet metal. The various operations are carried out in a single stroke. The design of progressive die is largely depends on material of sheet metal, thickness of sheet metal and complexity of design and operations. This press tool has significance like high rate of production and minimum per unit cost of product. In progressive die the variety of operations are performed at common work station. In present project the intensions is given on quality improvement along with production rate and cost minimization. Progressive die components are modeled in CATIA with selected dimensions for sheet metal plate. Finite element analysis is conducted for Progressive die obtaining deformation and stresses on sheet metal component by using ANSYS software. Keywords- Sheet metal, Die, Catia, Ansys I. INTRODUCTION The design and manufacture of press tools, or punches and dies, is a branch of production technology that has extended into many lines of engineering manufacture over the past seventy years. There is no doubt that the accuracy achieved by new ideas in design and construction applied by the press tool designer, coupled with increased speed and rigidity of the presses etc. used have all contributed toward maintaining this form of metal tooling well to the force as a means of obtaining pleasing, yet strong, durable articles that can withstand severe day-today usage. Design of sheet metal dies is a large division of tool engineering, used in varying degree in manufacturing industries like automobile, electronic, house hold wares and in furniture. There is no doubt that accuracy achieved by the new ideas in design and construction applied by the press tool designer, coupled latest development made in related fields made more productive, durable and economical. Hardened and toughened new martial & heat treatment process made the design easy. Progressive die can perform many operation compared to other dies and also it can able to eliminate the loading & unloading time which results in faster production rate. It has become the practice more and more to produce from sheet metal by some form of pressing process, work pieces that would have been made from bar, forging or casting two or three decades ago. Also, the handling of both strip material and semi-finished components has assumed an importance simply because fast and efficient movement means cheap products from operators who do not suffer fatigue from the handling of awkward or heavy components. However, it should not be forgotten that press design has made many advances in recent years in common with, for example, the machine tool industry, and machines are now available that are capable of withstanding the heavy stresses set up in many modern production process. So development of a computer-aided progressive die design and machining is become beneficial because of the ability to build precision tooling in less time and at a lower cost. The component to be formed in this project is known as tailgate striker of an automobile vehicle head/backlight assembly. It is assembled with nut bolt to fit with other parts in assembly. This project is divided into following parts: 1) Design of a progressive die according to the dimensions of the component. 2) 2D & 3D modelling of a progressive die. 3) Static structural and modal analysis of a progressive die for evaluation of frequencies and stresses. 4) Manufacturing of progressive die and result interpretation. i) Design of a progressive die according to the dimensions of the component. Various design steps are followed for design of progressive die by using standard references. From the dimensions of given component the die is designed. ii) 2D & 3D modelling of progressive die- By using the design data, we develop a 2D & 3D models of progressive die. For 2D model we used AutoCad and for 3D Unigraphics NX is used. iii) Static structural and modal analysis of a progressive die for evaluation of
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International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 08 | Aug 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 118 frequencies and stresses. After developing the 2D & 3D models finite element analysis is done on the 3D model. Static structural and modal AutoCad and for 3D Unigraphics NX is used. iii) Static structural and modal analysis of a progressive die for evaluation of frequencies and stresses. After developing the 2D & 3D models finite element analysis is done on the 3D model. Static structural and modal analyis are carried out and frequencies and stresses are evaluated for further analysis of results. iv) Manufacturing of progressive die and result interpretation. After analysis is done the die is manufactured and experiments are carried out for result interpretation. Sufficient area to prevent undue wear. It has even expansion under thermal load should be free as possible from discontinuities II. METHODOLOGY Project started with collecting necessary information. Literature related to progressive die and also various research papers are gathered and studied. For execution of project which methods to be implemented are studied and discussed. The dimension of the product is given by the enterprisers. By calculating the dimensions required for required progressive die we will go for the 3D model of. By using 3D software we will develop a 3D model. We used AutoCad for 2D model and Uni-graphics NX for 3D model. After development of 3D model finite element analysis is done. In that we have performed static structural and nodal analysis for evaluation of various stresses and frequencies respectively. Later on the basis of results of FE analysis we manufactured a required progressive die. Then experiments are performed on it. After that we prepared the results. III. DESIGN AND CALCULATION Design Considerations of a component Material MS Thickness of Material = 1mm Shear Strength = 400 N/mm2 Length = 76mm Width = 45mm Pierce diameter d1 = 21mm Pierce diameter d2 = 7mm Fillet radius R1 = 20mm Fillet radius R2 = 3mm We will perform piercing and blanking operations for development of a component. Material HCHCr is selected for die as it is hardened material. Punch and Die Size for Piercing Holes: In piercing punch is made equal to component while die is made larger (component size+2C) Where, C is cutting clearance, C = 0.01×t× 3√τmax/10 = 0.06mm per side Thus, die size, Ø7.12mm and Ø21.12mm Punch and Die Size for Complete Blanking: Length = 76mm, Width = 45mm,
3.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 08 | Aug 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 119 R1 = 20mm, R2 = 3mm Here, size of die would be same as size of the original blank. Cutting Force Calculations: Cutting force, Fsh = L× t ×τmax Where, L= blanking periphery + piercing periphery = 376.665m Also area of cutting= 2000mm2 Thickness of material = 1mm Thus, cutting force, Fsh = 376.665×1×400 = 150666 N = 15.06Ton Actual Press Tonnage, Press tonnage = 1.3× Fsh = 1.3 × 15.06 = 19.578≈20 ton Die Plate Thickness Here, Td = √(3Fsh/τ) × [(B/A)2/1+(B/A)2] Where, B= width of blank A= length of blank = √(3×1500666/400)×[(45/76)2/(1+(45/76)2] = 17.12 = 17.12+3mm …(for standard size 3mm is added to Td ) = 20.12mm =22mm≈ 25mm …(25mm D2 material block standard size Considered for deflection, δ= FL3/192EI where, I=bh3/12 = 150666×3303/192×2.1×105×221833.34 = 0.6053 mm Top Plate Top plate= 2×die plate thickness = 2×22 = 44mm ≈45mm For deflection, δ= FL3/48EI = 150666×3303/354×2.1×105×1898437.5 = 0.2829mm Bottom Plate Bottom plate = 2×die plate thickness = 2×die plate thickness = 2×22 = 44mm≈45mm For deflection, δ= FL3/354EI = 150666×3303/354×2.1×105×1898437.5 = 0.03836mm Guide Pillar Calculations Shut Height=160mm Press tonnage= 20 tons So we will use 4 pillars here For single pillar force tonnage= 20/4 = 5 ton/per pillar Here the load that will act on pillar is the crippling load For crippling load, P= π2EI/L2 e 5000×9.81 = π2×2.1×105×I/320 I = 2423.37mm4 Crippling Stress for M.S. σcr = 250 MPa σcr = π2E/λ2 thus, λ= 91.05 λ = Le/K 91.05 = 320/K K= 3.514mm Now, I= AK2 242.37=A×(3.514)2 A = 196.25mm2 Where, A=(π/4)×d2 D= 15.08mm For safety it is taken as twice of calculated Thus, D=30mm A= 706.85mm2 Now again, I=AK2 2423.37= 706.85×K2 K= 1.851mm λ= Le/K = 320/1.851 = 172.82 σcr= π2E/λ2 = 69.39N/mm2 which is safe for M.S. Strip Layout Here, Area of Product= 3000mm2 Area of Sheet= 102.5×103 mm2 Total number of blank per sheet Total length of sheet= 1250mm Total length of single product=51mm Number of blank= 1250/5 = 24.5 Thus number of blank per sheet=24 Total area of single product= 3000mm2 Now for 24 product= 3000×24 =72000mm2 For utilization of sheet Utilization of sheet = (72000/102.5×103)×100 = 70.24%
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International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 08 | Aug 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 120 IV. FINITE ELEMENT ANALYSIS Cad Modelling Fig 01: Assembly of Progressive Die Solid Modelling NX is a multi-use, multi-platform CAD software suit. NX also called as Unigraphics is 3D model developing software. It is most user friendly software. Fig 2: 3D model of progressive die Spring Modelling Fig 3: Spring modelling using Ansys connection tool Model Meshing No. of Nodes = 3,67,437 No. of Elements = 2,26,883 Fig 4: Meshed model as whole assembly Modal Analysis of an assembly The boundary conditions applied to the assembly during modal analysis is frictionless support. X-direction displacement is fixed at supports. Fig 5: 1st frequency The 1st natural frequency is 12.38 Hz. When the operating frequency 12 Hz coincides with this frequency, resonance will occur and shaft may fail during twisting. Fig 6: Displacement of assembly
5.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 08 | Aug 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 121 Fig 7: Von Misses Stresses generated V. RESULTS AND DISCUSSIONS We have analyzed Von Misses stresses with help of ANSYS. After comparing results, it is concluded design is safe. Modes Natural Frequency(Hz) Result 1 12.38 No Resonance 2 119.6 No Resonance 3 143.91 No Resonance 4 404.59 No Resonance 5 497.07 No Resonance Table 01: Modal Analysis Results Table 02: Structural analysis results Here we calculated all permissible stresses which are in limit of standard stress of material used. Thus the design is safe. The observations taken for 1minute, from that it is observed that for 1 minute the parts produced are 6 in number and for 1 hour parts produced are 360 in number. VI. CONCLUSIONS • From the results obtained from modal analysis we concluded that the vibrations on the die are bearable and there is no formation of resonance • From the results obtained from structural analysis we concluded that the equivalent stresses acting on the assembly are within limit and thus design is safe for operations • From the experimental results we obtained that time required for operation is 50 % less than old time. Also production rate obtained is 50% increased than old • So the aim of designing progressive die with factors productivity, cost reduction, product quality is achieved. REFERENCES [1]. Prakash H. Joshi, Press tolos design And Construction, A. H. Wheeler and Co. Ltd., 411, Surya Kiran, K. G. Marg, New Delhi. [2]. Ivana Shcy, Handbook of Die Design, 2nd edition Mc Grawth-Hill, 2006. [3]. Gashaw Desie1 and Yonas Mitiku Degu2 1, 2, School of Mechanical and Industrial Engineering, Bahir Dar Institute of Technology Bahir Dar University, Bahir Dar, Ethiopia ,“ Progressive Die Design for Self Explosive Reactive Armor Holder (Case Study at Bishoftu Motorization-Industry- Ethiopia)”,The International Journal Of Engineering And Science (IJES) ISSN (e): 2319 – 1813 ISSN (p): 2319 – 1805. [4] Taylan Altan, Metal Forming Hand book, Schuler, Berlin Heidelberg, 1998. [5] Ch. Mastanamma1, K. Prasad Rao2, Dr. M.Venkateshwara Rao3, “Design and Analysis of Progressive die”, Vol.1, Issue 6, Aug. 2012 IJERA. [6] Jyothi Bhaskar1, G Sathya Prakash2, “Die design and analysis of progressive tool for can lid lever” International Journal of Research in Engineering & Advanced Technology, Volume 1, Issue 4, Aug-Sept, 2018. Sr. No Param eters Von Misses Stress (Mpa) Yield Stress (Mpa) Results 1 Die 162 827 Within Limit 2 107 370 3 55 370 4 Punch 140 827 Within Limit 5 13 370 6 14 370
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