摘要
航空发动机燃油管主要用于提供燃油,属于复杂3维管路系统。为了更好地分析管路系统的振动特性,以双路总管燃油管路系统为例,结合其管路繁多、连接结构多样、支撑结构特殊、管内充液等特点,系统研究了各部件的有限元模拟方法。考虑到支撑刚度对管路系统振动特性有较大影响,采用有限元静力分析对其进行了求解。结合以上不同部件的分析方法,建立起系统的振动有限元模型。对该管路系统进行模态分析,得到系统固有频率变化规律及具有分簇特点的振动模态;对系统进行共振评估,认为副燃油分管最有可能发生共振,提出了振动优化的合理建议。
Aircraft engine fuel pipe is a three-dimensional pipeline system, mainly used for fuel supply. In order to analyze the vibration characteristics, taking dual fuel line system as an example, combining clustered lines, diversified connection structures, specific bracing structures and pipe with injecting liquids, the finite element simulation method has been systematically studied. Bracing stiffness of pipeline system, which has great influence on vibration characteristics, was analyzed by the finite element static method. Combining the above analysis methods of different components, the finite element model of vibration system was established. After modal analyzed the pipeline system, natural frequency change rule of the vibration system was obtained. The analysis results show that the mode of vibration has cluster characteristics. After the resonance evaluation of the system, vice fuel line branch was considered most possibly to resonate, and some reasonable optimization suggestions were proposed.
出处
《航空发动机》
2016年第1期42-47,共6页
Aeroengine
关键词
燃油管路
振动特性
支撑刚度
有限元
航空发动机
fuel pipe
vibration characteristics
bracing stiffness
finite element method
aeroengine