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直升机液压系统温度特性建模与仿真研究
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Research on Modeling and Simulation of Temprature Characteristics of Helicopter Hydraulic System
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    摘要:

    针对直升机液压系统分布广泛、结构复杂、功能需求多,导致其难以通过试验进行温度特性验证的难题,建立了直升机液压系统典型液压元件的发热及散热模型。以直升机执行某飞行任务为例,对液压系统的温度变化进行仿真分析。仿真结果与试飞数据对比证明:采用的分析方法及建立的模型正确可信,可为直升机液压系统的设计及优化提供依据

    Abstract:

    The helicopter hydraulic system has characteristics such as wide spreading,complicated structure and multifunction requirements,which make difficult to verity the hydraulic fluid temperature by experiment.The thermal model of typical helicopter hydraulic components was built.Aimed at a specific flight mission,the temperature variation of hydraulic system was simulated and analyzed.Comparisons between results with the flight data prove that the analysis method and the established models are correct and reliable,which can provide basis for design and optimization of helicopter hydraulic system.

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引用本文

张学雷,王晓欣,谭伦.直升机液压系统温度特性建模与仿真研究[J].机床与液压,2018,46(22):37-40.
. Research on Modeling and Simulation of Temprature Characteristics of Helicopter Hydraulic System[J]. Machine Tool & Hydraulics,2018,46(22):37-40

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  • 在线发布日期: 2019-07-09
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