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静压节流器微孔气膜参数测量装置设计与试验
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国家自然科学基金项目(51775529)


Design and Test of Gas Film Field Parameter Measurement Device for Micropore Aerostatic Throttler
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    摘要:

    研制一种节流器气膜场多路热工参数同时测量的自动化装置,阐述机械装置、硬件电路和软件程序的设计原理与实现。采用气膜厚度调节和气膜压力承载分离设计原理的机械结构以及基于Cortex-M4F内核的STM32F407主控芯片的电控系统和上下位机共同操作的软件程序组合的测量装置,具有自动化程度大、测量精度高等优点。在气膜厚度为6和10 μm以及供气压力为0.3、0.5和0.8 MPa的实验条件下进行测试,得到双U形平面静压节流器的气膜场温度和压力参数分布。分析得出:在供气压力和气膜厚度增大过程中,双U形节流器气膜场温度值均呈现减小趋势,气膜场压力值分别呈现增加和减小趋势;在供气压力和气膜厚度保持不变的情况下,双U形节流器气膜场在节流槽处产生温度骤降现象,在越过节流槽处产生压力骤降现象。

    Abstract:

    An automatic device for simultaneously measuring gas film field multi thermal parameters was developed and the design pinciple of mechanical shell,circuit and program were described.The measurement system consisted of mechanical shell with principle of gas film thickness adjustment module and pressure bearing module designed separately,control system with STM32F407 MCU based on Cortex-M4F kernel and program with PC and single chip,having advantages such as high automation level and high measuring accuracy.With the experimental conditions of 6 and 10 μm gas film thickness and 0.3,0.5 and 0.8 MPa supply pressure,the temperature and pressure parameters of gas film from double U type plane aerostatic throttle were measured and analyzed.Experimental results show not only with the increase of supply pressure and gas film thickness,the temperature of gas film from double U type plane aerostatic throttler is decreased,and the pressures are increased and decreased respectively,but also the gas film temperature from double U type plane aerostatic throttler appears drop phenomenon at the notches of aerostatic throttler and the pressure drops between notches and edge of aerostatic throttler but closer to notches when supply pressure and gas film thickness remains unchanged.

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引用本文

何勇强,陈爱军,李东升.静压节流器微孔气膜参数测量装置设计与试验[J].机床与液压,2020,48(2):7-12.
. Design and Test of Gas Film Field Parameter Measurement Device for Micropore Aerostatic Throttler[J]. Machine Tool & Hydraulics,2020,48(2):7-12

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  • 在线发布日期: 2020-04-23
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