航空柱塞泵周向振动多尺度建模与参数敏感性驱动的异常振动机理研究

Aerospace piston pump circumferential vibration multiscale modeling and parameter sensitivity-driven anomalous vibration mechanism study

  • 摘要: 针对某型航空柱塞液压泵在高压工况下出现的压力脉动异常与壳体周向振动超限问题,提出一种基于参数敏感性驱动的多尺度振动特性分析方法。构建包含转子、主轴、斜盘、柱塞等核心部件的参数化模型,该模型在周向上与实验数据幅值平均差值最大仅有17.4%,系统地揭示流量脉动激励下结构参数对系统响应特性的影响规律;建立包含安装座螺栓、分油盖螺栓及滑靴球铰等关键连接结构的外壳部分的有限元数值仿真模型,将部件的相互作用效应根据传力路径简化为激励作用于壳体,该模型的周向加速度结果与实验数据比对误差最大仅有0.5%。进一步地分析了关键结构参数对周向振动的影响:定子侧安装座螺栓预紧力提升可使测点加速度稳定在3.17g附近,分油盖螺栓刚度增加可抑制共振响应使加速度迅速稳定在1.94g附近;而动子侧滑靴球铰间隙增大将导致加速度在1倍至6倍时无显著变化,超过6倍时失稳。通过参数敏感性量化指标,阐明定子连接结构参数变化通过等效刚度调整实现振动收敛,而动子运动副参数则通过接触非线性诱发响应失稳,此为壳体振动超限的核心诱因。本研究首次将多尺度参数化模型与敏感性分析结合,提出的参数敏感性量化指标可为结构优化设计与故障诊断提供理论依据。

     

    Abstract: To address the abnormal pressure pulsation and excessive circumferential vibration observed in a certain type of aviation hydraulic piston pump under high-pressure conditions, a parameter-sensitivity-driven multi-scale vibration analysis method is proposed. A parameterized model incorporating the rotor, main shaft, swashplate, and plungers is established. This model achieves high accuracy, with a maximum average percentage deviation of 17.4% in circumferential vibration amplitude compared to experimental data. The study systematically reveals the influence laws of structural parameters on the response characteristics of the system under flow pulsation excitation. A finite element model of the pump casing is also developed, which includes critical connection structures such as mounting bolts, valve plate cover bolts, and slipper ball joints. The mutual interactions of internal components are simplified into equivalent excitations acting on the housing along the force transmission path. The simulated circumferential acceleration shows excellent agreement with experimental measurements, with a maximum deviation of only 0.5%. Further analysis investigates the influence of key structural parameters on circumferential vibration. Increasing the preload of the stator-side mounting bolts stabilizes the measured acceleration around 3.17g, while enhancing the stiffness of the valve plate cover bolts effectively suppresses resonance, reducing the acceleration to approximately 1.94g. In contrast, enlarging the slipper ball joint clearance on the rotor side causes minimal change in acceleration at low multiples (1× to 6×), but leads to instability beyond that threshold. By introducing a quantitative parameter sensitivity index, the study demonstrates that variations in stator-side connection parameters reduce vibration via equivalent stiffness modulation, whereas rotor-side kinematic joint parameters trigger instability through contact nonlinearity. This mechanism is identified as the primary cause of the casing’s vibration limit exceedance. This research, for the first time, integrates multi-scale parametric modeling with sensitivity analysis in the context of hydraulic pump dynamics. The proposed sensitivity-based evaluation method provides a theoretical foundation for structural optimization and fault diagnosis of high-performance hydraulic components.

     

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