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Coiling and deploying dynamic optimization of a C-cross section thin-walled composite deployable boom

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Abstract

A C-cross section thin-walled composite deployable boom (C boom) can be flattened and coiled elastically. Furthermore, C boom can be deployed by releasing stored strain energy. Finite element (FE) models of C booms are constructed based on a nonlinear explicit dynamics analysis. The full simulation is divided into six consecutive steps: flattening, end-compacting, releasing, coiling, holding, and deploying around a hub. An optimal design method for the coiling and deploying of the C boom is presented based on the response surface method (RSM). Twenty-seven sample points are obtained by using a full-factorial design of experiment method. Surrogate models of the maximum moment and stress during the fully simulated process, including the mass of the C boom, are created by the RSM. The maximum moment and mass are set as objectives, and the maximum stress is set as a constraint to increase deploying statue stiffness and enhance use times. A multi-objective optimization design of the C boom is performed by sequential quadratic programming algorithm. Lastly, FE models for the optimal design are built to validate the accuracy of the optimization and the response surface results.

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Funding

This study was supported by Key Funds of the National Natural Science Foundation of China (Grant No. 51835002), National Natural Science Foundation of China (Grant No. 51975001 and 51605001), in part by the Joint Funds of the National Natural Science Foundation of China (No. U1637207), and the Key Research and Development Plan of Anhui Province, China (No. 201904A05020034).

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Correspondence to Hongwei Guo.

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The authors declare that they have no conflict of interest.

Replication of results

All FE models of the present paper used the following parameters: radius and thickness of the radial and circumferential rollers are 20 mm and 1 mm, the distance between the two axes of the radial rollers is 60 mm, radius of the hub is 80 mm, all the parts have the same length of 60 mm, and the radius and longitudinal length of the dabber are 58 mm and 100 mm, respectively.

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Responsible Editor: Palaniappan Ramu

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Yang, H., Guo, H., Liu, R. et al. Coiling and deploying dynamic optimization of a C-cross section thin-walled composite deployable boom. Struct Multidisc Optim 61, 1731–1738 (2020). https://doi.org/10.1007/s00158-019-02429-x

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  • DOI: https://doi.org/10.1007/s00158-019-02429-x

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