Problem of optimisation of the transport aircraft nacelle damper assembly
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Дата
2024-11-03
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CPN Publishing Group
Анотація
In connection with the development of aircraft construction, the problem of calculating the stress-strain state and solving the problem of weight optimisation of nacelle fasteners for single-engine transport aircraft is relevant. Today, various models, including computer models, are widely used in strength calculations. A computer model of a complex system should reflect as fully as possible all the main factors and interrelationships that characterise real loads. Today, computer modelling of mechanical systems is widely used in mechanical engineering, so it is advisable to use computer modelling methods to calculate the strength and reliability of important structural elements of an aircraft.
Опис
Today, computer modelling of mechanical systems is widely used in mechanical engineering, so it is advisable to use computer modelling methods to calculate the strength and reliability of important structural elements of an aircraft. Due to the development of aircraft construction, the problem of calculating the stress-strain state and optimising the damper assembly of an aircraft nacelle is of great importance.
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Бібліографічний опис
Trubachev, S. I. Problem of optimisation of the transport aircraft nacelle damper assembly / Trubachev S. I., Kryvova S. G. //Science and technology: challenges, prospects and innovations : Proceedings of III International Scientific and Practical Conference, [Osaka, Japan], 1-3 November 2024. - Osaka, 2024. - Pp. 168-170.