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直升机空运医疗后送加热输液复温装置应用研究

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目的 收集加热输液复温装置实验数据,分析影响输液管末端液体温度的因素及规律,指导直升机空运后送加热复温护理操作.方法 采用控制变量法,分别在地面舱段和飞行环境下监测加热输液复温装置的加热温度、输液流量、输液管长度和隔热层等对输液管末端液体温度的影响,分析总结影响规律.采用插值计算方法计算输液管各点的温度值,并针对输液常用参数设置进行拟合计算.结果 设置加热输液复温装置的加热温度为42 ℃,输液流量分别设置为50、100、160、240、320、400、500 ml/h和600 ml/h,结果显示输液管始端温度随着输液流量增大而逐渐降低,末端温度随着输液流量增大先升高后降低,输液流量在240~320 ml/h时,输液管末端液体温度最高;飞行环境与地面状态下的输液管液体温度随流量变化的规律相同.对测试点以外的数据进行定量计算,获得各点位温度曲面图,且不同插值方法计算结果一致性较好.拟合计算结果显示,液体流量在240~320 ml/h时,线性度较好,计算结果与实验数据误差<0.5 ℃.结论 实验数据及总结的输液液体温度变化规律对直升机空运后送加热复温护理操作具有一定的参考价值和指导作用.
Applications of heating infusion rewarming device for helicopter aeromedical evacuation
Objective To analyze how the liquid temperatures at the end of the infusion tube are affected in order to facilitate the evacuation and rewarming by helicopters.Methods Using the control variable method,the effects of heating temperatures of the heating infusion rewarming device,infusion flow rate,infusion tube length and insulation layer on liquid temperatures at the end of the infusion tube were monitored in the ground cabin and flight environment respectively before the influencing factors were analyzed.The temperature values at each point of the infusion tube were calculated via interpolation,and fitting calculation was carried out for the common parameters of infusion.Results The heating temperature of the heating infusion rewarming device was set at 42 ℃,and the infusion flow at 50,100,160,240,320,400,500 ml/h and 600 ml/h respectively.The results showed that the temperatures at the beginning and the end of the infusion tube gradually decreased with the increase of infusion flow.When the infusion flow rate is 240~320 ml/h,the liquid temperature at the end of the infusion tube is the highest.The liquid temperatures of the infusion tube changed with the flow rate in the flight environment and on the ground.The data other than the test points was calculated quantitatively,and the surface map temperatures at each point was obtained.The results calculated using different interpolation methods were consistent.The results of fitting calculation showed that linearity was good when the liquid flow rate ranged from 240 to 320 ml/h,and the error between the calculated results and the experimental data was below 0.5 ℃.Conclusion The experimental data on and patterns of temperature change of infusion liquid are of referential value for nursing operations related to evacuation and rewarming by helicopters.

Medical evacuationHeating infusionControl variable method

崔小燕、薛兵杰、徐心怡、李俊娜、江琅、陈璐、王静、杜海波、郭磊、孔祥静

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东部战区空军医院健康管理中心,南京 210002

空军军医大学空军特色医学中心航空救生研究室,北京 100142

医疗后送 加热输液 控制变量法

2024

空军航空医学
空军总医院

空军航空医学

CSTPCD
影响因子:0.586
ISSN:2097-1753
年,卷(期):2024.41(3)