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Sensitivity analysis for probabilistic anti-resonance design of aeronautical hydraulic pipelines 被引量:13
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作者 Changcong ZHOU Zheng ZHANG +1 位作者 Fuchao LIU Wenxuan WANG 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2019年第4期948-953,共6页
In an uncertainty scheme, reliability and global sensitivity analysis is studied in this work, to provide helpful information for probabilistic anti-resonance design of vibration systems.Discussions show that the reso... In an uncertainty scheme, reliability and global sensitivity analysis is studied in this work, to provide helpful information for probabilistic anti-resonance design of vibration systems.Discussions show that the resonance failure problem can be viewed as a series system, in which input uncertainties are modeled by random variables. In order to quantitatively measure the contributions of input variables to the system reliability, a global sensitivity index is proposed, the properties of which are also discussed. Then the proposed index is tested with an aeronautical hydraulic pipeline system, which is under the excitation of pump vibration and at a risk of resonance failure. Sensitivity results under different failure criteria and variation coefficients are obtained and studied, from which significant and insignificant input variables can be identified.The proposed method provides a relatively new insight for anti-resonance design of engineering structures. 展开更多
关键词 Global sensitivity HYDRAULIC PIPELINE Reliability RESONANCE Uncertainty
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Reliability and global sensitivity analysis for an airplane slat mechanism considering wear degradation 被引量:2
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作者 Changcong ZHOU Haodong ZHAO +2 位作者 Qi CHANG Mengyao JI Chen LI 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2021年第1期163-170,共8页
This paper focuses on the issue of reliability and global sensitivity analysis for an airplane slat mechanism considering the uncertainties in the wear process of mechanical components.First,the multi-body kinematic m... This paper focuses on the issue of reliability and global sensitivity analysis for an airplane slat mechanism considering the uncertainties in the wear process of mechanical components.First,the multi-body kinematic model of the slat mechanism is built in the ADAMS software.The geometrical sizes of the roller wheels after wear degradation are considered as input variables and the angle the slat should turn is considered as the output response.To accurately identify the influential roller wheels to the reliability and robustness of the slat mechanism,the failure probability based sensitivity and variance-based sensitivity indices are introduced.Comprehensive analysis of the results have shown that the reliability analysis and global sensitivity theory can help engineers find significant parts by their contributions,thus provide guidance for mechanical design and maintenance. 展开更多
关键词 Slat mechanism Roller wheel Wear degradation RELIABILITY Sensitivity
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