Detail publikace

Effect of Ply Orientation on the Mechanical Performance of Carbon Fibre Honeycomb Cores

KONDRATIEV, A. PÍŠTĚK, V. GAJDACHUK, V. KHARCHENKO, M. NABOKINA, T. KUČERA, P. KUČERA, O.

Originální název

Effect of Ply Orientation on the Mechanical Performance of Carbon Fibre Honeycomb Cores

Typ

článek v časopise ve Web of Science, Jimp

Jazyk

angličtina

Originální abstrakt

Carbon fibres used as a honeycomb core material (subject to a proper in-depth analysis of their reinforcement patterns) allows solving the thermo-dimensional stability problem of the units for space systems. Based on the results of numerical simulations with the support of finite element analysis, the paper provides an evaluation of the accuracy of analytical dependencies for the determination of the moduli of elasticity of a carbon fibre honeycomb core in tension/compression and shear. It is shown that a carbon fibre honeycomb reinforcement pattern has a significant impact on the mechanical performance of the carbon fibre honeycomb core. For example, for honeycombs measuring 10 mm in height, the maximum shear modulus values corresponding to the reinforcement pattern of +/- 45 degrees exceed the minimum values for a reinforcement pattern of 0 degrees and 90 degrees by more than 5 times in the XOZ plane and 4 times for the shear modulus in the YOZ plane. The maximum modulus of the elasticity of the honeycomb core in the transverse tension, corresponding to a reinforcement pattern of +/- 75 degrees, exceeds the minimum modulus for the reinforcement pattern of +/- 15 degrees more than 3 times. We observe a decrease in the values of the mechanical performance of the carbon fibre honeycomb core depending on its height. With a honeycomb reinforcement pattern of +/- 45 degrees, the decrease in the shear modulus is 10% in the XOZ plane and 15% in the YOZ plane. The reduction in the modulus of elasticity in the transverse tension for the reinforcement pattern does not exceed 5%. It is shown that in order to ensure high-level moduli of elasticity with respect to tension/compression and shear at the same time, it is necessary to focus on a reinforcement pattern of +/- 64 degrees. The paper covers the development of the experimental prototype technology that produces carbon fibre honeycomb cores and structures for aerospace applications. It is shown by experiments that the use of a larger number of thin layers of unidirectional carbon fibres provides more than a 2-time reduction in honeycomb density while maintaining high values of strength and stiffness. Our findings can permit a significant expansion of the area of application relative to this class of honeycomb cores in aerospace engineering.

Klíčová slova

thermo-dimensional stability; modulus of elasticity; finite element analysis; experimental prototype technology

Autoři

KONDRATIEV, A.; PÍŠTĚK, V.; GAJDACHUK, V.; KHARCHENKO, M.; NABOKINA, T.; KUČERA, P.; KUČERA, O.

Vydáno

29. 5. 2023

Nakladatel

MDPI

ISSN

2073-4360

Periodikum

Polymers

Ročník

15

Číslo

11

Stát

Švýcarská konfederace

Strany od

1

Strany do

17

Strany počet

17

URL

https://www.mdpi.com/2073-4360/15/11/2503

Plný text v Digitální knihovně

http://hdl.handle.net/11012/213612

BibTex

@article{BUT183613,
  author="Andrii {Kondratiev} and Václav {Píštěk} and Vitaliy {Gajdachuk} and Maksym {Kharchenko} and Tetyana {Nabokina} and Pavel {Kučera} and Ondřej {Kučera}",
  title="Effect of Ply Orientation on the Mechanical Performance of Carbon Fibre Honeycomb Cores",
  journal="Polymers",
  year="2023",
  volume="15",
  number="11",
  pages="1--17",
  doi="10.3390/polym15112503",
  issn="2073-4360",
  url="https://www.mdpi.com/2073-4360/15/11/2503"
}