Abstract
Glass or carbon fiber reinforced composite frames are ideal lightweight and high-span structures in the field of aerospace. Fundamental frequency is a key performance indicator in the process of the composite frame structure design. Increasing the value of fundamental frequency of the frames could avoid the phenomenon of structural resonance. Based on the structure and material concurrent optimization concept, the concurrent multi-scale optimization design for the maximum fundamental frequency of fiber reinforced frame structure is proposed. An optimization model based on the maximum structural fundamental frequency and the specified fiber material volume constraint has been established. The objective function sensitivity information about the two geometrical scales design variables are deduced with semi-analytical method. Numerical example in the paper shows that the concurrent multi-scale optimization for the maximum fundamental frequency can further explore the coupling effect between the macro-structure and micro-material to increase the fundamental frequency. The new two geometrical scales optimization model provides a choice for the design of composite frame structure in aerospace and other industries.
Original language | English |
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Publication date | 2017 |
Publication status | Published - 2017 |
Event | 21st International Conference on Composite Materials, ICCM 2017 - Xi'an, China Duration: 20 Aug 2017 → 25 Aug 2017 |
Conference
Conference | 21st International Conference on Composite Materials, ICCM 2017 |
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Country/Territory | China |
City | Xi'an |
Period | 20/08/2017 → 25/08/2017 |
Bibliographical note
Publisher Copyright:© 2017 International Committee on Composite Materials. All rights reserved.
Keywords
- Composite frame
- Fiber winding angle
- Fundamental frequency maximization
- Multi-scale optimization
- Semi-analytical sensitivity analysis