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An accelerated life test model for harmonic drives under a segmental stress history and its parameter optimization
  • ISSN号:1000-9361
  • 期刊名称:《中国航空学报:英文版》
  • 分类:TU431[建筑科学—岩土工程;建筑科学—土工工程] O213.2[理学—概率论与数理统计;理学—数学]
  • 作者机构:[1]School of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, China, [2]Science and Technology on Aircraft Control Laboratory, Beihang University, Beo'ing 100191, China
  • 相关基金:co-supported by National Natural Science Foundation of China(Grant No.51505015,51575019);the National Basic Research Program of China(No.2014CB046402);CAST-BISEE Innovation Foundation of China
中文摘要:

Harmonic drives have various distinctive advantages and are widely used in space drive mechanisms. Accelerated life test(ALT) is commonly conducted to shorten test time and reduce associated costs. An appropriate ALT model is needed to predict the lifetime of harmonic drives with ALT data. However, harmonic drives which are used in space usually work under a segmental stress history, and traditional ALT models can hardly be used in this situation. This paper proposes a dedicated ALT model for harmonic drives applied in space systems. A comprehensive ALT model is established and genetic algorithm(GA) is adopted to obtain optimal parameters in the model using the Manson fatigue damage rule to describe the fatigue failure process and a cumulative damage method to calculate and accumulate the damage caused by each segment in the stress history.An ALT of harmonic drives was carried out and experimental results show that this model is acceptable and effective.

英文摘要:

Harmonic drives have various distinctive advantages and are widely used in space drive mechanisms. Accelerated life test (ALT) is commonly conducted to shorten test time and reduce associated costs. An appropriate ALT modet is needed to predict the lifetime of harmonic drives with ALT data. However, harmonic drives which are used in space usually work under a segmental stress history, and traditional ALT models can hardly be used in this situation. This paper proposes a dedicated ALT model for harmonic drives applied in space systems. A comprehensive ALT model is established and genetic algorithm (GA) is adopted to obtain optimal parameters in the model using the Manson fatigue damage rule to describe the fatigue failure process and a cumulative dam- age method to calculate and accumulate the damage caused by each segment in the stress history. An ALT of harmonic drives was carried out and experimental results show that this model is acceptable and effective.

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期刊信息
  • 《中国航空学报:英文版》
  • 中国科技核心期刊
  • 主管单位:中国航空工业第一集团公司
  • 主办单位:中国航空学会
  • 主编:朱自强
  • 地址:北京学院路37号中国航空学报:英文版编辑部
  • 邮编:100083
  • 邮箱:caifei@buaa.edu.cn
  • 电话:010-82317058 82318016
  • 国际标准刊号:ISSN:1000-9361
  • 国内统一刊号:ISSN:11-1732/V
  • 邮发代号:
  • 获奖情况:
  • 国内外数据库收录:
  • 被引量:393