Main Catalog Aviation and Rocket-Space Engineering Innovation Technologies of Aerospace Engineering

Creation of a defective CFRP panel for testing methods of its control and cutting

Authors: Tsypysheva S.N., Ternovskikh K.A., TSzia CHzheniuan
Published in issue: #5(58)/2021
DOI: 10.18698/2541-8009-2021-5-703
Category: Aviation and Rocket-Space Engineering \| Chapter: Innovation Technologies of Aerospace Engineering
Keywords: composite part defects, adhesion, delamination, contact molding, carbon prepreg, acoustic emission, non-destructive testing
Published: 17.06.2021

The process of creating a defective composite panel by the method of contact molding is described in detail for developing the method of non-destructive testing and analyzing the results of drilling artificially weakened sections of a carbon fiber reinforced panel. In the process of manufacturing a carbon fiber panel, defects are embedded in its structure in accordance with the template, leading to a violation of adhesion in the “fiber-binder” structure and most effectively controlled by non-destructive testing methods. Further directions of the study of the panel-sample are indicated for a detailed study of the results obtained using the method of acoustic emission.

References

[1] Komkov M.A., Bochkarev S.V., Galinovskiy A.L., et al. Tekhnologiya proizvodstva i diagnostika kachestva kompozitnykh konstruktsiy raketno-kosmicheskoy tekhniki [Production and quality diagnostics technology for rocket-spacecraft composite constructions]. Staryy Oskol, TNT Publ., 2020 (in Russ.).

[2] Galinovskiy A.L., Bochkarev S.V., Nelyub V.A. Tekhnologii proizvodstva i diagnostiki kompozitnykh konstruktsiy letatel’nykh apparatov [Production and quality diagnostics technology for aircraft composite constructions]. Staryy Oskol, TNT Publ., 2019 (in Russ.).

[3] Kovalev S.P., Nelyub V.A., Shelofast V.V. Multi-criteria analysis of aircraft structures fracture. Izvestiya vysshikh uchebnykh zavedeniy. Aviatsionnaya tekhnika, 2015, no. 4, pp. 9–14. (in Russ.). (Eng. version: Russ. Aeronaut., 2015, vol. 58, no. 4, pp. 370–375. DOI: https://doi.org/10.3103/S1068799815040029)

[4] Aleksandrov I.A., Malysheva G.V., Nelyub V.A., et al. Study of fracture surfaces of black-reinforced plastics made by melted and dissolved technologies. Entsiklopediya inzhenera-khimika [Encyclopaedia of Chemical Engineer], 2012, no. 4, pp. 24–30 (in Russ.).

[5] Nelyub V.A. Estimate of adhesion interaction between carbon fiber and epoxy binding agent. Klei. Germetiki. Tekhnologii [Adhesives. Sealants. Technologies], 2014, no. 7, pp. 20–22 (in Russ.).

[6] Abashin M.I., Barzov A.A., Galinovskiy A.L., et al. Ultrajet express diagnostics for machine building materials and products. Nauchno-tekhnicheskie vedomosti SPbGPU [St. Petersburg Polytechnic University Journal of Engineering Science and Technology], 2011, no. 2, pp. 141–147 (in Russ.).

[7] Galinovskiy A.L., Papich A., Erokhin S.A., et al. Possibility evaluation of potential extension of ultra-jet diagnosis method for composite materials. Vse materialy. Entsiklopedicheskiy spravochnik [All Materials. Encyclopaedic Reference Manual], 2021, no. 3, pp. 34–40 (in Russ.).

[8] Litvinov V.B., Toksanbaev M.S., Deev I.S., et al. Kinetics of curing the epoxy binders and microstructures of polymer particles in carbon reinforced plastics based on them. Materialovedenie [Material Science], 2011, no. 7, pp. 49 (in Russ.).

[9] Bochkarev S.V., Tsaplin A.I., Galinovskii A.L. et al. Ultra-jet diagnosis of heat treated material microstructure. Met. Sci. Heat Treat., 2017, vol. 59, no. 5-6, pp. 384–388. DOI: https://doi.org/10.1007/s11041-017-0160-7

[10] Tarasov V.A., Galinovskiy A.L. Problems and prospects of ultra-jet technology in rocket space engineering. Inzhenernyy zhurnal: nauka i innovatsii [Engineering Journal: Science and Innovation], 2013, no. 3. DOI: http://dx.doi.org/10.18698/2308-6033-2013-3-636 (in Russ.).

[11] Nelyub V.A., Aleksandrov I.A., Malysheva G.V., et al. Study of state parameters of carbon fiber surface. Entsiklopediya inzhenera-khimika [Encyclopaedia of Chemical Engineer], 2013, no. 5, pp. 34–38 (in Russ.).

[12] Abashin M.I Possibilities of express-estimate of product information-diagnostic parameters by ultra-jet method. Fundamental’nye i prikladnye problemy tekhniki i tekhnologii [Fundamental and applied problems of engineering and technology], 2011, no. 4-3, pp. 128–133 (in Russ.).