Modeling of Hybrid Shell Shaping Process in Carbon Fiber Tooling

Russian Aeronautics - Tập 60 - Trang 640-646 - 2018
L. P. Shabalin1, I. N. Sidorov1, R. N. Sungatullin1
1Tupolev Kazan National Research Technical University, Kazan, Russia

Tóm tắt

This paper covers an advanced technique of finite element analysis of co-curing shaping process at high temperature of hybrid metal-composite structures. The technique allows us to model a technological production process and to evaluate the influence of design parameters of tooling on the deflected mode and strength of elements taking into account the contact interaction.

Tài liệu tham khảo

Kurennov, S.S., Koshevoi, A.G., and Polyakov, A.G., Through-Thickness Stress Distribution in the Adhesive Joint for the Multilayer Composite Material, Izv. Vuz. Av. Tekhnika, 2015, vol. 58, no. 2, pp. 10–15 [Russian Aeronautics (Engl. Transl.), vol. 58, no. 2, pp. 145–151]. Shabalin, L.P., Khilov, P.A., and Sungatullin, R.N., A Technique of Finite Element Analysis for Co-Curing a Composite Shell with Integral Metal Part, Izv. Vuz. Av. Tekhnika, 2016, vol. 59, no. 4, pp. 143–148 [Russian Aeronautics (Engl. Transl.), vol. 59, no. 4, pp. 600–605]. Khilov, P.A., Khaliulin, V.I., and Shabalin, L.P., Special Features of Technological Process for Producing a Hybrid Titanium Structure, Trudy mezhdunarodnoi nauchni-tekhnicheskoi konferentsii “Problemy i perspektivy razvitiya aviatsii, nazemnogo transporta i energetiki” (Proc. Int. Sc.-Tech. Conf. “Problems and Perspectives of Aviation, Surface Transport and Energetics Development”), 2015, Kazan: Brig, pp. 254–256. Batrakov, V.V., Konstantinov, D.Yu., and Shabalin, L.P., Study of Technological Special Features of the Combined Shaping Process for Wedge-Shaped Sandwich Structures, Trudy mezhdunarodnoi nauchnotekhnicheskoi konferentsii “Problemy i perspektivy razvitiya aviatsii, nazemnogo transporta i energetiki” (Proc. Int. Sc.-Tech. Conf. “Problems and Perspectives of Aviation, Surface Transport and Energetics Development”), 2015, Kazan: Brig, pp. 144–150. Gureeva, N.A., Klochkov, Yu.V., and Nikolaev, A.P., Analysis of an Arbitrarily Loaded Shell of Revolution Based on the Finite Element Method in a Mixed Formulation, Izv. Vuz. Av. Tekhnika, 2010, vol. 53, no. 3, pp. 7–10 [Russian Aeronautics (Engl. Transl.), vol. 53, no. 3, pp. 250–256].