Carbon fiber based on a volume-reinforcing braided preform for an element of a propeller blade

Donetskiy K.I., Karavaev R.Y., Bystrikova D.V., Gracheva A.D.
UDC
678.8
DOI
10.18577/2307-6046-2022-0-12-27-38
Article PDF (Russian) (887.78 KB)
How to cite
Donetskiy K.I., Karavaev R.Y., Bystrikova D.V., Gracheva A.D. Carbon fiber based on a volume-reinforcing braided preform for an element of a propeller blade // Proceedings of VIAM. 2022. No. 12. DOI: 10.18577/2307-6046-2022-0-12-27-38. URL: https://test.viam.ru/en/journal/2022/12/3
Keywords
propeller, polymer composite materials, carbon fiber, pressure impregnation, epoxy hot melt binder, woven preforms, physical properties, performance properties
Abstract

Currently, one of the global trends in the development of aircraft engines is the replacement of metal alloys with composite materials, which makes it possible to achieve a significant reduction in the weight of products and improve their performance. The use of modern methods of modeling the process of impregnation of carbon filler allows to reduce the development time of both the material itself and the product based on it. It is necessary to apply a multilevel approach when developing materials of a new generation – material modeling at nano-, micro-, meso- and macrolevels, behavior of elementary samples, structural elements and products.

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