CESSNA M2飞机液压系统失效模式与可靠性分析OA
该文通过失效模式与影响分析(Failure Modes and Effects Analysis,FMEA)对 CESSNA M2 飞机液压系统进行深入的可靠性与风险评估.其液压系统在起落架收放、襟翼操作以及减速板关键功能中扮演着核心角色.研究通过系统性地识别潜在故障模式、分析其对飞机运行的影响、确定故障根本原因,并结合严重度(S)、发生度(O)和探测度(D)3 项指标进行量化评分,计算出风险优先数(Risk Priority Number,RPN),从而对风险进行排序和优先级划分.负载活门无法关闭、液压软管爆裂以及发动机驱动泵的灾难性损坏是该系统中最具风险的失效模式.针对这些高风险模式,该报告提出具体的维护改进建议,例如加强油液清洁度管理、实施定期油液分析,旨在从根本上降低风险,提升系统的整体可靠性和飞行安全性.
This paper conducts an in-depth reliability and risk assessment of the CESSNA M2 aircraft hydraulic system using Failure Modes and Effects Analysis(FMEA).The hydraulic system plays a central role in critical functions such as landing gear retraction and extension,flap operation,and speedbrake operation.This study systematically identifies potential failure modes,analyzes their impact on aircraft operations,and determines the root causes.These failures are then quantitatively scored using severity(S),occurrence(O),and detection(D)metrics,and a Risk Priority Number(RPN)is calculated to rank and prioritize risks.The highest-risk failure modes in the system are failure to close the load valve,hydraulic hose rupture,and catastrophic damage to the engine-driven pump.For these high-risk modes,this report proposes specific maintenance improvement recommendations,such as strengthening oil cleanliness management and implementing regular oil analysis,to fundamentally reduce risk and enhance overall system reliability and flight safety.
唐冬冬
中国民用航空飞行学院遂宁分院,四川 遂宁 629000
航空航天
液压系统失效模式故障分析风险评估可靠性分析
hydraulic systemfailure modefault analysisrisk assessmentreliability analysis
《科技创新与应用》 2026 (15)
13-16,21,5
中国民用航空飞行学院面上项目(25CAFUC03114)
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