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35 MPa压力体制民机液压能源系统故障工况热平衡分析
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国家自然科学基金面上项目(51775477)


Thermal Balance Analysis of 35 MPa Pressure System Civil Aircraft Hydraulic Energy System Fault Operating Condition
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    摘要:

    针对我国正在自主研发的35 MPa压力体制压力体制的2H/2E民机能源系统中的一套液压能源系统,分析其液压元件和液压能源系统热产生及热散失机制,建立其热平衡分析仿真模型。进一步分析液压泵斜盘卡死、安全阀卡滞在最大流量位置2个故障工况下的热产生机制,建立其热产生模型,开展系统级热平衡分析。结果表明:故障工况会导致液压油箱、液压泵、燃油箱等液压元件内的液压管路温度上升,但是燃油箱内液压管路最高温度低于燃油箱点燃温度,故燃油箱不存在点燃的风险。

    Abstract:

    For the 2H/2E civil aircraft hydraulic energy system with a 5000 psi pressure system that is being independently researched and developed in China, the thermal generation and thermal dissipation mechanism of hydraulic components and hydraulic energy system were analyzed, and the thermal balance analysis simulation model was established. The thermal generation mechanism of hydraulic pump under the two fault conditions of swash plate stuck and safety valve stuck at the maximum flow position was further analyzed, and the thermal generation model was established to carry out systemlevel heat balance analysis.The results show that the temperature of the hydraulic pipelines in the hydraulic components such as hydraulic tank, hydraulic pump and fuel tank will rise under fault condition, but the maximum temperature of the hydraulic pipelines in the fuel tank is lower than the ignition temperature of the fuel tank, so there is no ignition risk of the fuel tank.

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权凌霄,赵国庆,许孝林,郭长虹,黄自立.35 MPa压力体制民机液压能源系统故障工况热平衡分析[J].机床与液压,2021,49(19):114-118.
QUAN Lingxiao, ZHAO Guoqing, XU Xiaolin, GUO Changhong, HUANG Zili. Thermal Balance Analysis of 35 MPa Pressure System Civil Aircraft Hydraulic Energy System Fault Operating Condition[J]. Machine Tool & Hydraulics,2021,49(19):114-118

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  • 在线发布日期: 2023-03-21
  • 出版日期: 2021-10-15