Research Article
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Year 2017, , 111 - 116, 23.11.2017
https://doi.org/10.26701/ems.357076

Abstract

References

  • [1] Zhang P. Q., Ruan J. H., Li W. Z., (2001) “Influence of Some Factors on the Damping Property of Fiber-einforced Epoxy Composites at Low Temperature”, Cryogenics, vol.41, pp.245-253.
  • [2] Bhatnagar T., Ramakrishnan N., Kaik N. K., Komanduri R., (1995) “On the Machining of Fiber Reinforced lastic (FRP) Composite Laminates”, International Journal Mach. Tools Manufacture, vol. 35(5), pp.701-708.
  • [3] Botelhoa C. E., Silvac A. R., Pardinia C. L., Rezendea C. M., (2006) “A Review on the Development and Properties of Continuous Fiber/epoxy/aluminum Hybrid Composites for Aircraft Structures”, Materials Research, Vol. 9, No. 3, pp. 247-256.
  • [4] Calik A. and Yilidirm S., (2017) “Effect of adherend recessing on bi-adhesively bonded single-lap joints with spew fillet”, Sādhanā, Vol. 42, No. 3, pp. 317–325.
  • [5] Cortes P. and Cantwell W.J., (2006) “The prediction of tensile failure in titanium-based thermoplastic fibre–metal laminates”, Composites Science and Technology, vol. 66, pp. 2306–2316.
  • [6] Vogelesang L.B. and Vlot A., (2000) “Development of fibre metal laminates for advanced aerospace structures”, Journal of Materials Processing Technology, vol. 103, pp. 1-5.
  • [7] Khalili S.M.R., Daghigh V. and Farsani R.E., (2011) “Mechanical behavior of basalt fiber-reinforced and basalt fiber metal laminate composites under tensile and bending loads”, Journal of Reinforced Plastics and Composite, vol.30(8), pp. 647–659. DOI: 10.1177/0731684411398535
  • [8] Gonzalez-Canche N.G., Flores-Johnson E.A., Carrillo J.G., (2017) “Mechanical characterization of fiber metal laminate based on aramid fiber reinforced polypropylene”, Composıte Structures, Vol. 172, pp. 259-266. DOI: 10.1016/j.compstruct.2017.02.100
  • [9] Carrillo J.G. and Cantwell W.J., (2009) “Mechanical properties of a novel fiber–metal laminate based on a polypropylene composite”, Mechanics of Materials, Vol.41, pp.828–838. doi:10.1016/j.mechmat.2009.03.002.
  • [10] Calik A., (2016) “EFFECT OF ADHEREND SHAPE ON STRESS CONCENTRATION REDUCTION OF ADHESIVELY BONDED SINGLE LAP JOINT”, Engineering Review, Vol. 36, Issue 1, pp. 29-34

Improving the Adhesion Bonding Strength for FML Composites by Using an Extremely Thin Mesh Steel

Year 2017, , 111 - 116, 23.11.2017
https://doi.org/10.26701/ems.357076

Abstract

Fiber
metal laminate (FML) is an advanced composite material that combine the
advantageous of both fiber reinforced composites and metal alloys without
sharing their individual disadvantages. When it is compared to commonly known
fiber reinforced polymer composites, the FML provide better impact resistance
and fatigue strength. But the production of a FML composite is a major problem
since the bonding at fiber-metal interface can be poor. For this reason, the
adhesion bonding capability at the fiber-metal interface was investigated in
this study. Carbon fiber and glass fiber fabrics having both  ±45° and 0°-90° orientation were used as
fiber layers. And extremely thin stainless steel materials in the mesh form
were used as metal layers. The mesh sizes of the layers are 100 and 500
respectively. The produced specimens having 12 different configurations were
subjected to  single lap shear tests
according to ASTM D 5868-01 Standard. The results showed that 500-mesh
stainless steel favorably affected the adhesion bonding strength.

References

  • [1] Zhang P. Q., Ruan J. H., Li W. Z., (2001) “Influence of Some Factors on the Damping Property of Fiber-einforced Epoxy Composites at Low Temperature”, Cryogenics, vol.41, pp.245-253.
  • [2] Bhatnagar T., Ramakrishnan N., Kaik N. K., Komanduri R., (1995) “On the Machining of Fiber Reinforced lastic (FRP) Composite Laminates”, International Journal Mach. Tools Manufacture, vol. 35(5), pp.701-708.
  • [3] Botelhoa C. E., Silvac A. R., Pardinia C. L., Rezendea C. M., (2006) “A Review on the Development and Properties of Continuous Fiber/epoxy/aluminum Hybrid Composites for Aircraft Structures”, Materials Research, Vol. 9, No. 3, pp. 247-256.
  • [4] Calik A. and Yilidirm S., (2017) “Effect of adherend recessing on bi-adhesively bonded single-lap joints with spew fillet”, Sādhanā, Vol. 42, No. 3, pp. 317–325.
  • [5] Cortes P. and Cantwell W.J., (2006) “The prediction of tensile failure in titanium-based thermoplastic fibre–metal laminates”, Composites Science and Technology, vol. 66, pp. 2306–2316.
  • [6] Vogelesang L.B. and Vlot A., (2000) “Development of fibre metal laminates for advanced aerospace structures”, Journal of Materials Processing Technology, vol. 103, pp. 1-5.
  • [7] Khalili S.M.R., Daghigh V. and Farsani R.E., (2011) “Mechanical behavior of basalt fiber-reinforced and basalt fiber metal laminate composites under tensile and bending loads”, Journal of Reinforced Plastics and Composite, vol.30(8), pp. 647–659. DOI: 10.1177/0731684411398535
  • [8] Gonzalez-Canche N.G., Flores-Johnson E.A., Carrillo J.G., (2017) “Mechanical characterization of fiber metal laminate based on aramid fiber reinforced polypropylene”, Composıte Structures, Vol. 172, pp. 259-266. DOI: 10.1016/j.compstruct.2017.02.100
  • [9] Carrillo J.G. and Cantwell W.J., (2009) “Mechanical properties of a novel fiber–metal laminate based on a polypropylene composite”, Mechanics of Materials, Vol.41, pp.828–838. doi:10.1016/j.mechmat.2009.03.002.
  • [10] Calik A., (2016) “EFFECT OF ADHEREND SHAPE ON STRESS CONCENTRATION REDUCTION OF ADHESIVELY BONDED SINGLE LAP JOINT”, Engineering Review, Vol. 36, Issue 1, pp. 29-34
There are 10 citations in total.

Details

Subjects Mechanical Engineering
Journal Section Research Article
Authors

Mete Han Boztepe

Melih Bayramoğlu

Çağrı Uzay

Necdet Geren

Publication Date November 23, 2017
Acceptance Date November 23, 2017
Published in Issue Year 2017

Cite

APA Boztepe, M. H., Bayramoğlu, M., Uzay, Ç., Geren, N. (2017). Improving the Adhesion Bonding Strength for FML Composites by Using an Extremely Thin Mesh Steel. European Mechanical Science, 1(4), 111-116. https://doi.org/10.26701/ems.357076

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