Multi-modal safety analysis of the more electric aircraft starter generator system

Z. Zeng, Y. Hu, Y. Xiong, Q. Gong, X. Xu, H. Ge
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Abstract

Aiming at the characteristics of complex structure, strong coupling and different multi-modal safety levels of more electric aircraft starter generator system, a safety analysis method based on the operating process and a multi-modal failure rate calculation method are proposed. This paper analyses the architecture, operating process and modals of more electric aircraft starter generator system and decomposes the system into eight operating modals. Based on the construction of SafetyLab, a domestic safety analysis platform, the structural models and failure rate calculation models of eight modals of starter generator system are established, and the top event failure rate of each modal, the highest transient failure rate and the steady state failure rate of the system are calculated for a complete safety analysis, taking a typical starter generator system as an example. The method proposed in this paper helps to solve the problem of multi-modal failure rate analysis of complex systems with different equipment involved in the operating process. The multi-modal failure rate calculation method proposed in this paper is also applicable to the safety analysis of other multi-modal complex systems.
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更多电动飞机起动发电机系统的多模式安全分析
针对多电机飞机起动发电机系统结构复杂、耦合性强、多模态安全等级不同的特点,提出了基于运行过程的安全分析方法和多模态故障率计算方法。本文分析了多电机飞机起动发电机系统的结构、运行过程和模态,并将系统分解为八个运行模态。在构建国内安全分析平台 SafetyLab 的基础上,建立了起动发电机系统八个模态的结构模型和故障率计算模型,并以典型的起动发电机系统为例,计算了各模态的最高事件故障率、最高瞬态故障率和系统稳态故障率,进行了完整的安全分析。本文提出的方法有助于解决运行过程中涉及不同设备的复杂系统的多模态失效率分析问题。本文提出的多模式故障率计算方法也适用于其他多模式复杂系统的安全分析。
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