某型飞机气压控制系统电驱动设计可靠性指标的提高

2021 28th International Workshop on Electric Drives: Improving Reliability of Electric Drives (IWED) Pub Date : 2021-01-27 DOI:10.1109/IWED52055.2021.9376392

F. Ismagilov, V. Vavilov, R. Karimov, O. Yushkova, A. Timofeev

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引用次数: 0

摘要

本文通过对设计开发过程中电驱动元件的失效模式及影响分析，探讨了提高座舱气压控制系统电驱动可靠性设计的方法。根据可靠性指标，对系统的电力驱动实施方案进行了研究。选用对电传动设计可靠性影响最大的部件。提出了电驱动的改进设计。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Design Reliability Indicators Enhancement on the Example of an Aircraft Air Pressure Control System Electric Drive

The paper discusses a way to improve the reliability design of the air pressure control system electric drive in the cockpit by electric drive components failure mode and effects analysis in the design development process. Possible options for the system's electric drive implementation have been investigated in terms of their reliability indicators. Components are selected, the failures of which have the greatest impact on the electric drive design reliability. The electric drive improved design is proposed.

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2021 28th International Workshop on Electric Drives: Improving Reliability of Electric Drives (IWED)

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