Study of dynamic characteristics of samples from metal-polymeric materials and aluminium alloy D16ch-AT

Postnov V.I., Postnova M.V., Antipov V.V., Veshkin E.A
UDC
669.018.95
DOI
10.18577/2307-6046-2025-0-4-70-80
Article PDF (Russian) (457.69 KB)
How to cite
Postnov V.I., Postnova M.V., Antipov V.V., Veshkin E.A Study of dynamic characteristics of samples from metal-polymeric materials and aluminium alloy D16ch-AT // Proceedings of VIAM. 2025. No. 4. DOI: 10.18577/2307-6046-2025-0-4-70-80. URL: https://test.viam.ru/en/journal/2025/4/6
Keywords
metalpolymers, alloy, strength, deformation, loading, elasticity
Abstract

The experience of metal-polymeric composite materials (MPCM) application shows that these materials have a higher durability than traditional aluminum alloys. The article considers results of comparative tests for determination of the elastically damping properties of different types of MPCM and alloy D16. The studies show that the modulus of elasticity and Poinson’s coefficient of the tested MPCM panels are practically independent of the load level in the studied range of relative deformations and close to the values of alloy D16. The damping capacity is slightly dependent on the MPCM structure and logarithmic oscillation discretion is 5 %, while it does not exceed 0,6 % in the alloy D16.

Reference list
  1. Kablov E.N. New generation materials – the basis of innovations, technological leadership and national security of Russia. Intellekt & Tekhnologii, 2016, no. 2, pp. 41–46.
  2. Kablov E.N. Aerospace materials science. Vse materialy. Entsiklopedicheskiy spravochnik, 2008, no. 3, pp. 2–14.
  3. Duyunova V.A., Kutyrev A.E., Serebrennikova N.Yu., Vdovin A.I., Somov A.V. Examination of the impact of aggressive environmental factors on the development of corrosion damage on samples of laminated glass-reinforced plastic of SIAL class. Aviation materials and technologies, 2021, no. 4 (65), paper no. 09. Available at: http://www.journal.viam.ru (accessed: September 16, 2024). DOI: 10.18577/2713-0193-2021-0-4-81-90.
  4. Duyunova V.A., Serebrennikova N.Yu., Nefedova Yu.N., Sidelnikov V.V., Somov A.V. Methods of forming metal-polymer composite materials (review). Aviation materials and technologies, 2022, no. 1 (66), paper no. 06. Available at: http://www.journal.viam.ru (ассеssed: September 16, 2024). DOI: 10.18577/2713-0193-2022-0-1-65-77.
  5. Kablov E.N., Kulagina G.S., Zhelezina G.F., Lonskii S.L., Kurshev E.V. Microstructure research of the unidirectional organoplastic based on Rusar-NT aramid fibers and epoxy-polysulfone binder. Aviacionnye materialy i tehnologii, 2020, no. 4 (61), pp. 19–26. DOI: 10.18577/2071-9140-2020-0-4-19-26.
  6. Antipov V.V., Serebrennikova N.Yu., Konovalov A.N., Nefedova Yu.N. Perspectives of application of fiber metal laminate materials based on aluminum alloys in aircraft design. Aviacionnye materialy i tehnologii, 2020, no. 1 (58), pp. 45–53. DOI: 10.18577/2071-9140-2020-0-1-45-53.
  7. Grinevich A.V., Rumyancev Yu.S., Morozova L.V., Terehin A.L. Study of fatigue life of 1163-T and V95o.ch.-T2 aluminum alloys after surface hardening. Aviacionnye materialy i tehnologii, 2014, no. S4, pp. 93–102. DOI: 10.18577/2071-9140-2014-0-s4-93-102.
  8. Zhelezina G.F. Crack-resistant metal-organoplastics for aircraft structures: thesis abstract, Cand. Sc. (Tech.). Moscow: VIAM, 1996, 32 p.
  9. Lavro N.A., Barabash V.N., Efimov V.A. Forecasting the service life and resource of large-sized aircraft radar radomes made of polymer composite materials. VII Int. Scientific Conf. on Hydroaviation «Gidroaviasalon-2008»: in 2 parts. Gelendzhik, 2008, part 1, pp. 353–360.
  10. Lukina N.F., Dementeva L.A., Anikhovskaya L.I. Adhesive prepregs for laminated aluminum glass plastics (SIAL). Trudy VIAM, 2014, no. 1, paper no. 05. Available at: http://www.viam-works.ru (accessed: September 16, 2024). DOI: 10.18577/2307-6046-2014-0-1-5-5.
  11. Postnov A.V., Postnov V.I., Vyakin V.N. Elastic-damping properties of metal-polymer composites under high-frequency loading. Vestnik SGAU im. S.P. Koroleva, 2011, no. 3, pp. 80–87.
  12. Zagrebalov A.A., Kishkina S.I. Residual stresses and fatigue of composite materials. Issues of aviation science and technology. Ser.: Aviation materials. Moscow: VIAM, 1990, pp. 87–93.
  13. Grabilnikov A.S., Mashinskaya G.P., Zhelezina G.F., Zinevich O.M., Deev I.S. Interlayer crack resistance of the hybrid composite material Alor. Mekhanika kompozitsionnykh materialov, 1990, vol. 30, no. 2, pp. 196–206.
  14. Nesterenko G.I. Residual strength of reinforced structures with extensive and multi-focal fatigue damage. Strength, vibrations and resource of aircraft structures and constructions. Moscow: TsAGI, 2002, pp. 112–117.
  15. Senatorova O.G., Anikhovskaya L.I., Sidelnikov V.V. et al. Fatigue resistance and fracture features of sheet aluminum-glass plastics. Reports Int. Conf. «Layered Composite Materials – 98». Volgograd: VSTU, 1998, рp. 86–88.