67.02
Doi: 10.31772/2712-8970-2021-22-2-391-397
Rudenko M. S., Mikheev A. E., Girn A. V.
Reshetnev Siberian State University of Science and Technology,
31, Krasnoyarskii rabochii prospekt, Krasnoyarsk, 660037, Russian Federation
The honeycomb filler is an integral part of the spacecraft's sandwich panel. Currently, a honeycomb filler made of aluminum alloys is used. The proposed technology makes it possible to replace the honeycomb filler material from aluminum alloys with polymer composite materials (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.
Keywords: honeycomb filler, polymer composite material, RTM method.
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]. Vestnik SibSAU. 2005, No.
6, P. 169–173 (In Russ.).
12. 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.
13. 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.).
14.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.
15. 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.