DOAJ Open Access 2014

A location optimization method for aircraft weakly-rigid structures

Wang Zhong-Qi Yang Yuan Kang Yong-Gang Chang Zheng-Ping

Abstrak

Since aircraft weakly-rigid structure has large size and weak stiffness, there has serious deformation during assembly process. The current deformation analysis theory of rigid assembly is not applicable. Based on the N-2-1 (N > 3) locating principle, this paper presents a methodology for weakly-rigid parts. An optimization algorithm combines finite element analysis and nonlinear programming methods to find the optimal number and position of the locating points in order to minimize the assembly deformation. An example application study is presented to demonstrate the optimization procedure and its effectiveness by using the software of ABAQUS.

Topik & Kata Kunci

Industrial engineering. Management engineering Industrial directories

Penulis (4)

Wang Zhong-Qi

Yang Yuan

Kang Yong-Gang

Chang Zheng-Ping

Format Sitasi

APA MLA BibTeX

Zhong-Qi, W., Yuan, Y., Yong-Gang, K., Zheng-Ping, C. (2014). A location optimization method for aircraft weakly-rigid structures. https://doi.org/10.1051/smdo/2013014

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Informasi Jurnal

Tahun Terbit: 2014
Sumber Database: DOAJ
DOI: 10.1051/smdo/2013014
Akses: Open Access ✓