Manufacturing technology honeycomb core from polymeric composite materals

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Resumo

The honeycomb core is an integral part of the spacecraft's sandwich panel. Currently, use of aluminum honeycomb core in sandwich constructions. The proposed technology makes it possible to replace the honeycomb filler material from aluminum with a polymer composite material (PCM). The main difference between the developed technology for the production of honeycomb filler by the RTM method is that corrugated tape is glued during the formation of the composite material. This is a separate process in the existing methods for the production of honeycomb cores from PCM. This paper presents the results of creating a prototype of a honeycomb filler by the RTM-method, a technological process has been developed.

Sobre autores

Mikhail Rudenko

Reshetnev Siberian State University of Science and Technology

Autor responsável pela correspondência
Email: mister.m.rudenko@gmail.com

Assistant

Rússia, 31, Krasnoyarskii rabochii prospekt, Krasnoyarsk, 660037

Anatoly Mikheev

Reshetnev Siberian State University of Science and Technology

Email: michla@mail.ru

Dr. Sc., Professor

Rússia, 31, Krasnoyarskii rabochii prospekt, Krasnoyarsk, 660037

Alexey Girn

Reshetnev Siberian State University of Science and Technology

Email: girn007@gmail.com

Cand. Sc., Associate Professor

Rússia, 31, Krasnoyarskii rabochii prospekt, Krasnoyarsk, 660037

Bibliografia

  1. Panin V. F., Gladkov Yu. A. Konstruktsii s zapolnitelem [Constructions with filler]. Moscow, Mashinostroenie Publ., 1991, 272 p.
  2. Khaliulin V. I., Shapaev I. I. Tekhnologiya proizvodstva kompozitnykh izdeliy [Technology of production of composite products]. Kazan', Izd-vo Kazan. gos. tekhn. un-ta Publ., 2003.
  3. Achilles Petras Design of Sandwich Structures : Doct. Diss. 1998. P. 5–7.
  4. Grabin B. V. Inzhenernye osnovy konstruirovaniya kosmicheskikh apparatov [Engineering bases of spacecraft design]. Moscow, MAI Publ., 2018, 255 p.
  5. Testoedov N. A., Nagovitskin V. N., Permyakov M. Yu. [The use of three-layer honeycomb structures in spacecraft]. Vestnik SibSAU. 2016, Vol. 17, No. 1, P. 200–211 (In Russ.).
  6. Endogur A. I., Vainberg M. V., Ierusalimsky K. M. Sotovye konstruktsii: Vybor parametrov i proektirovanie [Cellular structures: choice of parameters and design]. Moscow, Mashinostroenie Publ., 1986, 192 p.
  7. Melnikov D. A., Petrov A. P., Gromova A. A. et al. [Calculation of the ratio of the components of the prepreg brand VPS-53/120, determination of the physical-mechanical and operational characteristics of fiberglass]. TRUDY VIAM. 2019, No. 1 (73), P. 92–104 (In Russ.).
  8. Urakova A. S., Nagovitsin V. N. [Application of cellular panels in satellite technology]. Reshetnevskie chteniya [Reshetnev readings]. 2018, P. 179–180 (In Russ.).
  9. Minakov V. T., Postnov V. I., Shchvets N. I. et al. [Features of manufacturing three-layer honeycomb panels with a polymer filler of hot curing]. Aviatsionnye materialy i tekhnologii. 2009, No. 4 (12), P. 15–18 (In Russ.).
  10. Zlotenko V. V., Ishenina N. N. [Features of mechanical processing of aluminum honeycomb structures] Vestnik SibSAU. 2005, No. 6, P. 209–211 (In Russ.).
  11. Slivinsky, V. I., Tkachenko, G. V., Slivinsky M. V. [Efficacy of cell structures in aircraft].
  12. Vestnik SibSAU. 2005, No. 6, P. 169–173 (In Russ.).
  13. A. A. Ivanov, S. M. Kashin, V. I. Semenov Novoe pokolenie sotovykh zapolniteley dlya aviatsionno-kosmicheskoy tekhniki [New generation of cell aggregates for aerospace engineering]. Moscow, Energoatomizdat Publ., 2000, 584 p.
  14. Pershin A. M. [Computational study of static stability of cellular aggregates made of composite materials]. Vestnik Samarskogo gosudarstvennogo aerokosmicheskogo universiteta. 2014, No. 5 (47), chast' 1, P. 118–123 (In Russ.).
  15. Kryukov A. M., Volkova V. S., Murashkin Yu. G. et al. Sposob izgotovleniya sotovykh zapolniteley [Method of manufacturing honeycomb fillers]. Patent RF, No. 2651012, 2018.
  16. Kryukov A. M., Volkova V. S., Murashkin Yu. G. et al. Sposob izgotovleniya trekhsloynykh paneley slozhnoy krivizny [Method of manufacturing three-layer panels of complex curvature]. Patent RF, No. 2680571, 2018.

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Declaração de direitos autorais © Rudenko M.S., Mikheev A.Y., Girn A.V., 2021

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Este artigo é disponível sob a Licença Creative Commons Atribuição 4.0 Internacional.

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