Abstract
Variants of constructive solutions for transformable frameworks of spacecrafts are offered. The folded structures with four-ray elementary modules are used as the basis of the kinematic configurations. It is shown that the transformation patterns of folded structures ensure compactness of the framework in a transport position and make it possible to get placed in a packaged state onto a planar or cylindrical surface of the load-carrying structure, to deploy simultaneously biaxially, and to exert a minimal impact on dynamic stabilization of a spacecraft. A mathematical model for transformation of the frameworks with four-ray folded structures is developed. The model is based on vector coupling between the nodal points of the folded structure at each stage of transformation.
This is a preview of subscription content, log in via an institution to check access.
Similar content being viewed by others
REFERENCES
US Patent 8813455, 2014.
RU Patent 2380798, 2010.
Maji, A.K., Harris, M., Garcia, D., and Deblonk, B.J., Feasibility assessment of deployable composite telescope, J. Aerosp. Eng., 2011, vol. 24, no. 1, p. 12.
Brinkmeyer, A., Pellegrino, S., and Weaver, P.M., Effects of long-term stowage on the deployment of bistable tape springs, J. Appl. Mech., Trans. ASME, 2016, vol. 83, no. 1.
RU Patent 2247683, 2005.
US Patent 5487791, 1996.
Zirbel, S.A., Lang, R.J., et al., Accommodating thickness in origami-based deployable arrays, J. Mech. Des., 2013, vol. 135.
Khaliulin, V.I., On the classification of regular ordinary folded structures I, Izv. Vyssh. Uchebn. Zaved., Aviats. Tekh., 2003, no. 2, p. 7.
Wan, Z., Zhou, H., Khaliulin, V.I., and Shabalov, A.V., Six-ray folded configurations as the geometric basis of thin-walled elements in engineering structures, Thin-Walled Struct., 2018, no. 130, p. 435.
Khaliulin, V.I., On the method of synthesis of the structure of folded fillers of multilayer panels, Izv. Vuzov, Aviats. Tekh., 2005, no. 1, p. 7.
Zakirov, I.M. and Alekseev, K.A., Determination of parameters of a four-beam spiral-shaped folded structure, Izv. Vyssh. Uchebn. Zaved., Aviats. Tekh., 2005, no. 4, p. 57.
Khaliulin, V.I., Razdaibedin, A.A., and Menyashkin, D.V., Estimating the effect of instability of technological parameters on the accuracy of the folded filler, Izv. Vyssh. Uchebn. Zaved., Aviats. Tekh., 2005, no. 3, p. 63.
Krylov, A.V. and Churilin, S.A., Modeling the deployment of solar batteries of various configurations, Vestn. Mosk. Gos. Tekh. Univ. im. N. E. Baumana, Ser. Mashinostr., 2011, no. 1, p. 106.
Zimin, V.N., On the issue of modeling and calculating the dynamics of opening of transformable structures, Oboronnaya Tekh., 2006, nos. 1–2, p. 123.
Khaliulin, V.I., Geometric modeling in the synthesis of structures of folded aggregates of multilayer panels, Vestn. Kazan. Gos. Tekh. Univ., 1995, no. 1.
Razdaibedin, A.A. and Khaliulin, V.I., Determination of technological parameters of forming a folded filler with an enveloping curved surface, Izv. Vyssh. Uchebn. Zaved., Aviats. Tekh., 2015, no. 1, p. 69.
Funding
This work was supported by the Ministry of Science and Higher Education of the Russian Federation under the project with the unique identifier RFMEFI61620X0126.
Author information
Authors and Affiliations
Corresponding author
Ethics declarations
The authors declare no conflict of interest.
Additional information
Translated by L. Mukhortova
About this article
Cite this article
Khaliulin, V.I., Savitskii, V.V. A Transformed Framework with a Folded Configuration. J. Mach. Manuf. Reliab. 49, 948–957 (2020). https://doi.org/10.3103/S1052618820110072
Received:
Accepted:
Published:
Issue Date:
DOI: https://doi.org/10.3103/S1052618820110072