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“FABRICATION AND ANALYSIS OF MECHANICAL PROPERTIES CELLULOSE JUTE FIBER AND GRAPHITE FIBER BASED HYBRID COMPOSITE MATERIAL”
1.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 07 | Jul 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 14 “FABRICATION AND ANALYSIS OF MECHANICAL PROPERTIES CELLULOSE JUTE FIBER AND GRAPHITE FIBER BASED HYBRID COMPOSITE MATERIAL” PRITI DWIVEDI1, ASHUTOSH SHUKLA2 1M.Tech Student, Department of Mechanical Engineering, Kanpur Institute of Technology, Kanpur AKTU, U.P India. 2Assistant Professor Department of Mechanical Engineering, Kanpur Institute of Technology, Kanpur AKTU, U.P India. ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract – Composite material is one of the most emerging materials of modern era as it provides light weight, high strength to weight ratio, electrical insulation etc. and Hybrid composites have vast area of application due to its better mechanical properties and economically point of view.Intoday’sscenariocompositematerial hascompetitionwithitsowncompatibilities. Aviation industries are most benefitted from composite materials. Hybrid composite materials such as carbon-glass fiber, agamid etc. are used in the fabrication of air craft wings, nose and some other parts that full fill their desired demands. Some other hybrid composites of baggage, cellulose fiber particles, cellulose jute fiber ash, cellulose jute fiber powder, barley husk etc. are most successfully used in automobile industry, furniture industry, and electronic device industry and in dentistry for filling. It is very difficult to fabricate a hybrid composite that provides superior properties over existing composites. Thus the measurement of mechanical properties of fabricated composite material is studiedto understandthebehaviorofcompositeof material. In the present work, a hybrid composite of cellulose jute fiber powder and graphite-fiber has been fabricated. For binding cellulose jute powder and graphite-fiber epoxy resin is used. For fabrication hand lay-up method was usedandtwo categories were decided one for 30gm CSP (cellulose jute powder) and another for 45gm CSP. The next step a number of samples were taken from these two categories. Then hardness testing, tensile testing, impact testing and bending test were performed on these selected samples and behavior of 30gm CSP and 45gm CSP were studied. Key Words: Then hardness testing, Tensile Testing, Impact Testing and Bending test were performed on these selected samples and behavior of 30gm CSP and 45gm CSP were studied. 1. INTRODUCTION In today’s industrialization composite materials are used in various applications likeinteriorsofvehicles,machine parts,aero- space industry, furniture industry, railways, building constructions,ceilingsandpanels,automobiles,medical industryetc. due there surprising property of light weight, cost effective, easy manufacturing, bio-degradable and environment eco- friendly materials. Composites have the continuous phase with one or more discontinuous phase. The reinforcementmaterial iscalled discontinuous phase and the continuous phase is known as matrix. Discontinuous phase is stronger than continuous phase. Composite displays the properties of their constituent materials.Thesize,shapeandmaterial reinforcementdistributionaffect the composite properties. The size, shape and material reinforcement distribution affect the composite properties. Fiber reinforced and natural fillers composite have high qualities and widearea ofapplicationinvariousfieldsoftechnical sector[1]. In the thermoplastic like armed and glass fiber conventional synthetic fibersarealsousedforreinforcement.Dueto properties like low density, high thermal insulation, better mechanical properties, environment friendly, disposable, minimal tool wear, easy availability and low price synthetics fibers are used. Synthetic fibers are available in different forms like threads, woven form, wool form, strands etc. 1.2 Definition of Composite Two or more natural or artificial materials are combined to make a composite. Thus their constituent’s useful properties are maximized and their weaknesses are minimized. Most widely used composite is graphite-fibers reinforced plastic (GRP) that combines with graphite fibers with plastic to make a composite material that is tough but not brittle. Composite are best alternatives of metals as they provide higher strength in lighter weight.
2.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 07 | Jul 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 15 Figure 1.2: Composite materials 1.3 Hybrid composites These composites are the composition of two or more different types of reinforcement material, combined in a single matrix form. Hybrid composite materials have the properties of both reinforcement materials in a single matrix. A wide variety of reinforcement material available, but well known commonreinforcementmaterial isgraphite-fiber. Theconstituentsofhybrid composite material are mixed at molecular level, due to this it forms the more homogenous material and mostly they are anisotropic in nature. 2. Fabrication methods 2.1 Hand lay-up method is the process when fiber reinforcements are placed with resin and allow air dry in room temperature. In this the wooden mold are prepared of required size and gel coatingisdonetopreventthestickingof resinover the surface. After that with the help of trowel the layers of resin and reinforcement material are formed. 2.2 Compression molding, in this method the heat and pressure is used to fabricate the material. The mold is filled with the plastic material and then the heat and pressure applied to the mold to form the composite material. Figure 2.1 Hand Lay-up Method Figure 2.2 Compression molding Method Fibers are categorized in two types one is natural fiber and second is synthetic fiber. Natural fibersareextractingfromorganic sources, where as synthetic fibers are made from inorganic sources. Natural fibers are the by-product of plants, fruits and crops. They are the waste of plants, fruits and crops after using these organic products. Natural fibers are renewable, cheap, recyclable and biodegradable. Plants like banana, pineapple, jute, bamboo etc. 2.3 Cellulose fiber Cellulose fiber is a natural crop and it comes from crops . Farming of cellulose fiber is mainly done in all Indian states near by the rives crops. It is also cropped in other countries like Sri Lanka, Indonesia, Thailand and Malaysia. After using the cellulose fiber water the waste is rest called cellulose fiber. Cellulose fiber is agro waste with hard lingo-cellulose content. Composite made from cellulose fiber are used in building material, furniture and fishnets. Cellulose fiber is prominent reinforcement
3.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 07 | Jul 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 16 material in fabrication of various types of polymer matrix composites. Cellulose fiber has low cost, easily and abundantly available, high strength, etc. 2.4 Cellulose jute Cellulose jute fiber was taken and then sieved to determine the hair sizes in by passing through different sieves. Cellulose jute fiber have no economic value because it is the waste by-product after using cellulose jute anditshairforms.Cellulosejutefiber is costly and the environment friendly. Cellulose jute fiber are can also used as absorbents in water purification system and to treat industrial and municipal waste. Figure. Cellulose fiber Figure Graphite fiber The graphite fiber is the very strong certain class of Carbone fiber the atomic structure is the both are seam is thecarbonfiber is the similar to graphite fiber it is the consisting of sheets of the carbon atoms arranged in a regular hexagonal pattern. 3. Experimental Set-Up and methodology Figure 3.1: Flow diagram of experimentation The present study is to fabricate a new type of composite and to measure its mechanical properties so that it can be used in different applications. The methodology as given in a flow chart (figure 3.1) followed in the experimental investigation: Cellulose jute fiber hair by crushing and taking samples of different weights Graphite fiber in woven form Slurry of cellulose jute fiber will be prepared by mixing the resin and hardener by hand lay-up method and graphite fiber will be placed in the slurry after that mixture with graphite fiber will be dried Mechanical testing of samples
4.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 07 | Jul 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 17 3.1 Material used Material that are used are given below in figure 3.2 Materials are use Figure 3.2: Materials used 3.2 Cellulose jute fiber Table 3.1.1: Grain size ratio for 30gm CSP S NO. Grain Size in microns Material weight in grams 1 600 0.56 2 425 3.33 3 300 2.78 4 150 5.00 5 90 2.22 6 75 1.11 7 Smaller particles below 75 microns 5.00 3.3 Graphite fiber Graphite fiber is an artificial fiber mostly used as reinforced material in preparing of composite. There several types’ graphite fiber is formed like wool, threads and in woven form. Graphite fiber is used in woven form in present work. Table 3.1.4: Materials Quantity S. No. Cellulose jute fiber hair Reinforced Graphite Fiber Epoxy solution Resin Hardener 1 30 gm Woven form 165gm 165gm 2 45 gm Woven 170gm 170gm 3.4 Mixing of Resin and Hardener The adhesive solution epoxy resin and hardener is mix in proportion, by weighing scale resin and hardener are taken 150gm each in beaker and both are mix well by stirring continuously until both the resin and hardener are mixes with each other. Mixture is cured in normal room temperature and pressure. Cured mixture has good thermal and physical stability. 3.5 Mixing of Cellulose jute fiber (CSP) and Epoxy solution CSP is taken in two weights 30gm and 45gm by weighing scale and these two weights are mixed with resin hardener mixture (160gm each) separately in separate beakers, stir the mixture of CSP and epoxy well until theCSPmixed within epoxysolution evenly. This mixture is also cured in normal room temperature and pressure. Epoxy solution (Resin + Hardener) Cellulose jute fiber Graphite fiber in woven form
5.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 07 | Jul 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 18 4. Sample Preparation Table 3.5Specimen size S.No. Test of Properties Specimen size in mm 1 Tensile Test 170 X 20 X 7 2 Bending Test 76 X 25 X 7 3 Impact Test 65 X15 X7 4.1 Tensile strength test: This digital and advance machine used for testing tensile strengthforvariouspolymer compositesplasticmaterial etc.Machine has a maximum capacity of 1000 kgf. A specimen of 170×20×7 mm is taken and fix it in between the grippers of UTM the span length is 90mm. 4.2 Bending strength test For this test UTM is used. For this test specimen size is 76 25 7 mm taken and specimen held in roller type bending set up. 4.3 Impact strength test A specimen size of 65 ×15×7 mm is taken and notch is prepared at the center of specimen then specimen is kept on the machine. In the next step pendulum is released towards the specimen to measure the impact energy of specimen. 5. RESULT AND DISCUSSION 5.1 Hardness A Sample piece of 30gm CSP and 45gm CSP is placed one by one over the flat surface, then the probe of hardness tester is pressed at 5 random points over the sample surfaces and readings are noted. Hardness value for both composite samples is taken as the average of 5 random values of hardness for selected sample For 30 gm CSP composite sample the average hardness value is 78.2 while for 45 gm CSP the average hardness value is 80.5 5.2 Tensile strength Table no. 5.2.1: Maximum load and tensile strength of samples for 30gm CSP: Specimen Maximum Load in (N) Tensile Strength in (Mpa) 1 2305.900 25.273 2 2028.600 22.354 3 1753.200 19.455 Table no. 5.2.2: Maximum load and tensile strength of samples for 45gm CSP Specimen Maximum Load in (N) Tensile Strength in (Mpa) 1 1570.000 17.516 2 1220.200 13.792 3 1435.700 16.092
6.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 07 | Jul 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 19 5.3 Bending Strength Table 5.3.1: Maximum load and bending strength of samples for 30gm CSP: Specimen Maximum Load in (N) Bending Strength in (Mpa) 1 132.400 24.571 2 182.400 33.467 3 123.600 24.589 Table no. 5.3.2: Maximum load and bending strength of samples for 45gm CSP Specimen Maximum Load in (N) Bending Strength in (Mpa) 1 280.300 48.586 2 210.000 37.264 3 175.600 32.157 5.4 Impact strength For impact strength test, four samples are taken, two of 30gm CSP and two of 45gm CSP. Table no. 5.4.1 Impact test showing Impact energy and Impact strength for 30gm CSP: Sample Izod Impact Energy Impact Strength 1 1.675 ASTM standards j/m Kg.cm/cm Kg.m/m 290.4 31.6327 30.6327 IS/ISO standards j/mm² j/cm² Kj/m² 0.055 2.4048 25.0476 2 1.05 ASTM standards j/m Kg.cm/cm Kg.m/m 185 20.8755 20.7755 IS/ISO standards j/mm² j/cm² Kj/m² 0.0246 1.7603 16.6032 Table no. 5.4.2 Impact test showing Impact energy and Impact strength for 45gm CSP Sample Izod Impact Energy Impact Strength 1 1.066 ASTM standards j/m Kg.cm/cm Kg.m/m 213.2 21.7551 21.7551 IS/ISO standards j/mm² j/cm² Kj/m² 0.0169 1.6921 16.9206 2 1.066 ASTM standards j/m Kg.cm/cm Kg.m/m 213.2 21.7551 21.7551 IS/ISO standards j/mm² j/cm² Kj/m² 0.0169 1.6921 16.9206
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International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 07 | Jul 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 20 6. CONCLUTION 45gm CSP sample was harder than 30 gm CSP. As the weight of CSP increases hardness of hybrid composite increases. 30 gm CSP hybrid composite sample result an improved tensile strength in UTM than 45 gm CSP hybrid composite sample. Load required to break 30 gm CSP hybrid composite sample is also higher than that of 45 gm CSP hybrid composite sample.45 gm CSP hybrid composite resulted an improved bending strength in UTM than30gmCSP. Maximumloadthata 45gmCSPsample can bear is higher than that of 30 gm CSP sample. Impact strength of 30 gm CSP hybrid composite is higher than that of 45 gm CSP hybrid composite. Impact energy of 30 gm CSP is 1.752 while for 45 gm CSP it is 1.095. 7. FUTURE SCOPE Many experiments have been performed to fabricate and to test hybridcompositebutlimitedstudyispresentforcelluloseJute fiber and graphite fiber hybrid composite. Graphite fiber can also be used in some other forms like wool form, thread formetc. In the current work Cellulose jute is used fiber by varying its weight. This hybrid composite can also be fabricated by varying particle size Cellulose jute fiber. In the current work the ratio of resin and hardener are same, this can also be varied tochange the properties of hybrid composite. SEM (Scanned Electron Microscopy) can also be used for detailed study of hybrid composite material. REFERENCES 1. S. Luo and A.N. Netravali “Mechanical and Thermal Properties of Environmentally Friendly “Green”compositesMade from Pineapple Leaf Fibers and Poly (hydroxybutyrate-co-valerate) Resin” Polymer Composites, 20 (3). (1999), pp. 367- 378. 2. M. azaurang P. Herrera I. Gonzalez and V.M. Aguilar “Physical and Mechanical Properties of Henequen Fibers”Journal of Applied Polymer Sciences, 43 (1991), pp. 749–756 3. E.M. Ahmed B. Sahari and P. Pedersen “Non Linear Behavior of Unidirectional Filament Wound OTFRP FRP andGFRP composites” Proceedings of World Engineering Congress 1999, Mechanical and Manufacturing Engineering, Kuala Lumpur, 19–22 July, 1999, pp. 537–543. 4. Salmah H., Koay SC., And Hakimah O. “Surface Modulation of Coconut Shell Powder Filled Polylactic” 5. Thwe, Moe Moe, and Kin Liao. "Effects of environmental aging on the mechanical properties of bamboo–glass fiber reinforced polymer matrix hybrid composites." CompositesPartA:AppliedScienceand Manufacturing 33.1(2002): 43- 52. 6. Bledzki, Andrzej K., Abdullah A. Mamun, and Jürgen Volk. "Barley husk and coconut shell Reinforced polypropylene composites: the effect of fibre physical, chemical and surface properties ." Composites Science and Technology 70.5 (2010): 840-846. 7. Pradhan, Siddhartha K., E. S. Dwarakadasa, and Philip J. Reucroft. "Processing and Characterization of coconut shell powder filled UHMWPE." Materials Science and Engineering: A 367.1-2 (2004): 57-62. 8. Agunsoye, J. Olumuyiwa, Talabi S. Isaac, and Sanni O. Samuel. "Study of mechanical behavior of coconut shell reinforced polymer matrix composite." Journal of minerals and materials characterization and Engineering 11.8 (2012): 774-779. 9. Gunasekaran, K., P. S. Kumar, and M. Lakshmipathy. "Mechanical and bond properties of coconut shell concrete." Construction and building materials 25.1 (2011): 92-98. 10. Agunsoye, J. Olumuyiwa, Talabi S. Isaac, and Sanni O. Samuel. "Study of mechanical behavior of coconut shell reinforced polymer matrix composite." Journal of minerals and materials characterization and Engineering 11.8 (2012): 774-779.
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International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 07 | Jul 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 21 11. Lassila, L. V. J., T. Nohrström, and P. K. Vallittu. "The influence of short-term water storageontheflexural propertiesof unidirectional glass fiber-reinforced composites." Biomaterials 23.10 (2002): 2221-2229. 12. Udhayasankar, R., and B. Karthikeyan. "A review on coconut shell reinforced composites." International Journal of Chem Tech Research 8.11 (2015): 624-637. 13. Gunasekaran, K., P. S. Kumar, and M. Lakshmipathy. "Mechanical and bond properties of coconut shell concrete." Construction and building materials 25.1 (2011): 92-98. 14. Jawaid M, Khalil A HPS, Bakar ABU A, “Mechanical performance of oil palmemptyfruit Cunches/jutefibersreinforced epoxy hybrid composites”. Material science and Engineering A527 (2010) 7944-7949. BIOGRAPHIES PRITI DWIVEDI (M.Tech.) Master of Technology Student, Department of Mechanical Engineering, Kanpur Institute of Technology, Kanpur AKTU, U.P India. Ashutosh Shukla Assistant Professor Department of Mechanical Engineering, Kanpur Institute of Technology, Kanpur AKTU, U.P India.
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