| 2016 2nd International Conference on Mechanical and Aeronautical Engineering (ICMAE 2016) | |
| Study of Fuze Structure and Reliability Design Based on the Direct Search Method | |
| 机械制造;航空航天工程 | |
| Lin, Zhang^1 ; Ning, Wang^1 | |
| Air Force Engineering University, Xi'an, Shaanxi, China^1 | |
| 关键词: Critical systems; Design optimization; Direct search methods; Multiple factors; Redundancy configuration; Redundant design; Reliability design; Structural weight; | |
| Others : https://iopscience.iop.org/article/10.1088/1757-899X/187/1/012038/pdf DOI : 10.1088/1757-899X/187/1/012038 |
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| 学科分类:航空航天科学 | |
| 来源: IOP | |
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【 摘 要 】
Redundant design is one of the important methods to improve the reliability of the system, but mutual coupling of multiple factors is often involved in the design. In my study, Direct Search Method is introduced into the optimum redundancy configuration for design optimization, in which, the reliability, cost, structural weight and other factors can be taken into account simultaneously, and the redundant allocation and reliability design of aircraft critical system are computed. The results show that this method is convenient and workable, and applicable to the redundancy configurations and optimization of various designs upon appropriate modifications. And this method has a good practical value.
【 预 览 】
| Files | Size | Format | View |
|---|---|---|---|
| Study of Fuze Structure and Reliability Design Based on the Direct Search Method | 575KB |
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