ANALYSIS OF DEFORMATION CHARACTERISTIC OF EPOXY COTTON PLASTIC LAYER BASED SYNTACTIC FOAM

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International Research Journal of Engineering and Technology (IRJET) e ISSN: 2395 0056

ANALYSIS OF DEFORMATION CHARACTERISTIC OF EPOXY COTTON PLASTIC LAYER BASED SYNTACTIC FOAM

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Abstract The current research focus is on the study and synthesis of the deformation characteristic of epoxy plastic syntactic foams. In the current investigation, important to achieve good reinforcement properties as we know polymer vary in their chemical structure and offer different properties there selection of polymer matrix made based on application and property requirement. thermoplastics can used to make composites The resin plastic mixture (putty like consistency) which have high viscosities beyond 4 layer stops filtering and depends on the reinforcement used in the layer it is found that if polymer matrix is filled with fibrous materials the resulting material that is process very high and excellent mechanical properties these materials can be used for load bearing and other high end application such as material are composite materials there are two component themaincomponent ofthe composite is the matrix and second is component is reinforcement which is more often called as filler. The overpriced of artificial thermoplastic fibers like glass and carbon, etc. results ineffective and products obtained from these stuff which has demanded substitute resources of stuff advancement. This is also include the usage of nearby obtainable waste thermoplastics for materials stuff advancement. In this research, the main motive is to develop, investigate and determine the mechanical properties of the reinforcement material using waste thermoplastics. The fabrication of the composite was carried out using epoxyresin as the matrix and the waste thermoplastics as reinforcement. Tests were carried out to determinethemechanicalproperties such as tensile, hardness, impact and compressive strengths. The results were studied and compared with the conventional materials and it process that the material developed can be used in structural applications with strong dependence on its mechanical properties.

1. INTRODUCTION

Syntacticfoamisacompositematerial [1] Itisclosedcell composite material mixed in an epoxy and hardener matrix.[2] It has good mechanical properties, very strong andinsulationproperties,lowexpansionandlowmoisture absorptioncapacity,etc.[3] Itisdevelopedfornewmaterial andstrengthishigh.Applicationbecauseitislightweights alsoitsapplicationinshipstructureandspacecraft.Syntactic

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foamisusedascorematerialasanynewproductstructure in composite.[4] first is matrix phase and reinforcement matrixofmaterialisbyweightiscompositeonefiberepoxy compositesareusedasstructuralmaterialsforthefuselage wings tail doors and much of the interior lightweight compositesenhanceanaircraft’sefficiency inloadcarrying capacityand hugeadvantageinfuelsavinginfactthevery firstlarge scaleseofcarbonfiberepoxycomposite isused thematrixenergysectorisalsoutilizingcompositeandthere are turbines with blades and application it is the storage tankisverylightnotasteelcylinderthisissolvedbyhaving FRPasthematerialforhydrogenstoragetankorcylinders when a polymer matrix material is mixed with a non polymermaterialsuchasametal,non metal,ametal,anoil ,aceramic,etc.toformanewmaterialthequalityofallthe othermaterialthatwegetisinthematerialalone,whichwe call polymer composite material[5][6][7]. There are two types of composite material .first is the main constitute formingthebodyofcompositematerialisthematrixphase andsecondisthematerialwhichprovidethestrengthtothe matrix material is the reinforcement matrix. Composite material are an what are constitute and what their propertiesarewhohavelearnthatcompositearelight,stiff, and strong material[8][9][10]. There are combination of two are more than two phases the very important fiber material isglass,carbon,boron,silica,andsyntheticfiber conventionalengineeringmaterialarenotabletoservethe specific need there is a requirement to develop formed material the need of material with better properties are increase thecombinationofbetter propertiescanonlybe achievedwithintroductionofnewmaterialtheprojectisan studyofnaturalfibresandparticularglassfibreandwood andfindthemechanicalstrengthandstiffnessisselectedas areinforcementbecauseofgoodproperties andalsoused 79:7.9 as the Wight ratio four epoxy and hardener and placed the one by one and applied the mixed epoxy and hardenerinbetweenthefibreslayerandusedsiliconspread and dry for 48 hours [11][18] Epoxy resin is important classesofthermosettingpolymersthatareusedinadvanced composites, because it has chemical resistance and high tensilealsohighcompressivestrength.[12][19] Ithaslow shrinkage properties during cure process, and has good adhesion,andalongwithgoodstructuralstrength[13][18].

Volume: 09 Issue: 06 | Jun 2022 www.irjet.net p ISSN: 2395 0072 © 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page520

Puneet Kumar Bhatia1 , Aditya Mall 2 , Anand Gopal Yadav3 ,Akash Singh4 ,Dhirendra Pratap Singh5 Assistant Professor, Dept. of Mechanical Engineering, Buddha Institute of Technology, Gorakhpur, Uttar Pradesh, India 2,3,4,5 Dept. of Mechanical Engineering, Buddha Institute of Technology, Uttar Pradesh, India

International Research Journal of Engineering and Technology (IRJET) e ISSN: 2395 0056

Volume: 09 Issue: 06 | Jun 2022 www.irjet.net p ISSN: 2395 0072

2. LITERATURE RIVIEW

•J.R.M ALMEDA et.al (2012)[14]Work on the effect of diameter of glass, wood on the mechanical behaviour of microspherecompositehefindthatmechanical behaviour of glass microsphere is achieve by varying diameter of microsphere.Wallthicknessofmicrosphereisindependent ofmeansize,soitisimportanttoachieveoptimumdiameter towallthicknessratioanditismostimportantprocessing parameter.

•AARE ARUNIIT et.al (2014)[15] Researchonthetopicof effect of wood microsphere on a mechanical and physical characteristicthefocusedstudyistofindminimumcostwith of composition of composite which is light in weight but havingdesirablemechanicalproperty.

•K.C. YUNG et.al (2014)[16] Researchondifferentproperty of hollow glass microsphere, they filled hollow glass microsphere in the epoxy matrix with varying volume% from0 50ofhollowglassmicrosphere.Inthisprocessthey gotimprovedpropertylikecoefficientofexpansionandglass transitiontemperature.

3. MATERIAL

Raw material choose for this experimental work are as follows

I EpoxyResinLY556 II Hardener HY951 III SiliconeSpray IV Plywood V. Polythene VI. CelloTape

4. SAMPLE PREPARATION

There are three types of sample has been prepared using Epoxyresin(LY556),hardener(HY951)[17], polytheneand Plywood.

I. By using only epoxy and Hardener

Fig 1 EpoxyResin(LY556)andHardener(HY951) [17]

Fig 2 Thisimageshowingthesampleofepoxyandhardener

II. By adding a layer of Polythene in the above sample(Reinforcement of polythene)

Fig 3 Thisimageshowingthereinforcementofpolythene.

© 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page521
International Research Journal of Engineering and Technology (IRJET) e ISSN: 2395 0056 Volume: 09 Issue: 06 | Jun 2022 www.irjet.net p ISSN: 2395 0072 © 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page522 III. By Adding Reinforcement of polythene and Plywood with epoxy and hardener Fig 4 Thisimageshowingthereinforcementof polytheneandPlywood 5. PREPARATION OF TESTING SPECIMEN After preparation of sample to analysis of deformation characteristic of epoxycotton plasticlayer basedsyntactic foamistomakeadifferenttypeofsample a.Forimpacttestspecimen b.ForTensileTestspecimen c.Forcompressivetestsample Fig 5 Impacttestspecimen Fig 6 TensileTestspecimen Fig 7 Compressivetestsample 6. METHODOLOGY Fig 7 ThisblockdiagramshowstheMethodologythatis used. 7. APPLICATION Theepoxyreinforcementisuseindifferentareas I. Intransportindustries Mixingof precursorEpoxy andHardener +Thermoplastic Mixingbystir casting Mixuntilsmall amountofheat willrelease Applysilicon sprayonmold Pourmixturein mold Placecrystal clearsheeton mold Implement some load on mold Dryatroom temperaturefor 24hrs. Removeweight andtakeout sample Testing

International Research Journal of Engineering and Technology (IRJET) e ISSN: 2395 0056

Volume: 09 Issue: 06 | Jun 2022 www.irjet.net

ISSN: 2395 0072

9. CONCLUSION

•Thestrengthofimpactandcompositematerialisdepends accordingtodifferentlayerofthermoplasticinimpacttest. Impact strength of different sample is grew with growing layer of Reinforcement up to 3 layer and then begin reducing.

8. RESULT

AfterperformingcompressiveTest,Thefollowingresultsare obtains

For without Reinforcement

FractureLoad=46.2kN

Cross sectionAreaofrectangularSpecimen

A=30*15=450mm2

So, Compressivestress=Fractureload/Area Compressivestress=(46.2×103)/450=102.66MPa

For Reinforcement uses

FractureLoad=56kN

Cross sectionAreaofrectangularSpecimen

A=30*15=450mm2

So, Compressivestress=Fractureload/Area Compressivestress=(56×103)/450=124.44MPa

Compressive Strength curve with different layer of reinforcementareshownbelow

•The Hardness of composite material is differing in accordance with different layer of thermoplastic in the hardnesstest.Hardnessofdifferentsampleisincreasedwith increasing layer of Reinforcement up to 3 layer and then startreducing.

•InTensiletrialthetensilestrengthofcompositematerialis differinginaccordancewithdifferentlayerofthermoplastic. Tensilestrengthof1layersampleisincreasedthenfurther decreaseat2and3layersofreinforcement&at4layerof reinforcementthetensilestrengthisincreased.Itmeansthat thecharacteristicsoftensilestrengthofcompositesmaterial arenotpoor.

•Thecompressivestrengthofcompositematerialisdiffering in accordance with different layer of thermoplastic in compressivetest.ofcompositescompressivestrengthofthe increasesandstrong withincreasinglayerofReinforcement up to 3 layer and then start decreasing. It means the propertiesofcompressivestrengthmaterialareverygoodas comparetotensilestrength.

10. ACKNOWLEDGEMENT

I would like to thank PhD Scholar and Former Assistant professorMr.DirendraKumar,whohavehelpedmeinthe understandingtheconceptof compositeandreinforcement.

11. REFERENCES

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© 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page523 II.Usedinracingboats IV. Inrocketcomponent V. Inmilitaryaircraft VI. Inenginecomponent VII.InSportindustries
Fig 4: ThisFigureshowingCompressivestrengthvaries withrespecttothelayerofreinforcement.

International Research Journal of Engineering and Technology (IRJET) e ISSN: 2395 0056

Volume: 09 Issue: 06 | Jun 2022 www.irjet.net p ISSN: 2395 0072

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