Study on Integrated Optimum Design System of Composite Aircraft Structures
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DOI: 10.25236/icceme.2019.010
Corresponding Author
Kong Lei
Abstract
With the development of aircraft manufacturing industry, transportation, national defense and other aspects, the requirement for the overall performance of aircraft is getting higher and higher, and the research of composite aircraft structural integrated optimization design has attracted more and more attention. In this paper, the application of composite materials in aircraft structure is described firstly. Secondly, the current research situation of composite aircraft structure comprehensive optimization design is analyzed. Finally, the existing problems are described. Thus, under the constant attempts and efforts of more experts and scholars, the comprehensive optimization design of aircraft composite structures in the aircraft manufacturing industry can be continuously innovated and reformed, so as to improve the overall performance of aircraft and create greater value for the country.
Keywords
Composite material; aircraft structure; optimization design