Modeling of aero-engine afterburning fuel metering module with natural frequency studies
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摘要:
针对某型航空发动机加力燃油计量模块结构复杂、试验分析困难等问题,基于力平衡和流量平衡方程在AMESim中进行了模块数字化建模和仿真,并采用流场仿真分析软件得到了稳态液动力相关模型参数,对加力各区等压差活门和计量活门性能进行了研究;利用AMESim的线性分析工具对加力各区关键活门的固有频率及相关影响因素进行了专门研究。仿真结果表明:建立的模型与试验数据相比误差小于5%,具有较高的精度和可靠性;同时固有频率的研究成果可为该型燃油计量模块的改进和工程排故提供理论支持和实践基础。
Abstract:Considering the complexities of the structure and the difficulties in experimental analysis of a certain type of aircraft engine’s afterburner fuel metering module, digital modeling and simulation were conducted in AMESim based on force balance and flow balance equations. Additionally, steady-state hydrodynamic model parameters were obtained using flow field simulation analysis software. Studies on the performance of pressure-equalizing valves and metering valves in different zones of the afterburner were carried out. Utilizing AMESim’s linear analysis tool, special research was conducted on the natural frequencies of critical valves in various zones of the afterburner, along with their influencing factors. The simulation results showed that the established model had an error of less than 5% compared with experimental data, demonstrating high accuracy and reliability. Moreover, the research on natural frequencies could provide a theoretical support and practical foundation for improvements and engineering troubleshooting of this type of fuel metering module.
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表 1 0区计量模块固有频率影响因素分析结果
Table 1. Analysis results of factors contributing to natural frequencies of the zone 0 metrological module version
活门类型 影响因素 固有频率/Hz 等压差
活门中腔开口
直径/mm3.6 133.86 3.8 135.78 4 137.57 4.2 139.19 计量活门 弹簧刚度/
(N/mm)3.52174 19.42 4.02174 20.67 4.52174 21.78 5.02174 22.97 5.52174 24.04 阀芯等效
质量/kg0.15225 28.13 0.20225 24.41 0.25225 21.78 0.30225 19.96 0.35225 18.49 表 2 1区计量模块固有频率影响因素分析结果
Table 2. Analysis results of natural frequency influence factors of zone 1 metering module
影响因素 固有频率/Hz 弹簧刚度/(N/mm) 8.9524 24.53 9.9524 25.32 10.9524 26.09 11.9524 26.84 12.9524 27.56 阀芯等效质量/kg 0.5413 28.4 0.5913 27.17 0.6413 26.09 0.6913 25.13 0.7413 24.27 -
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