CAJ | 학술논문

以神舟载人飞船流体回路为物理模型，分析了各个部件的工作原理、流动和传热特性，建立起辐射器、泵、阀门、补偿器、冷板和换热器的部件模型。在此基础上建立了流体回路模型，并引入实际控制策略。模型的仿真数据与航天器热平衡试验数据进行对比，结果表明，模型对流体回路各点的温度、压力、系统的流量分配和液体体积变化的补偿都能较好的进行动态模拟，并能够模拟系统控制策略的动态执行情况，可用于流体回路系统控制算法和策略的优化分析。
이신주재인비선류체회로위물리모형，분석료각개부건적공작원리、류동화전열특성，건립기복사기、빙、벌문、보상기、랭판화환열기적부건모형。재차기출상건립료류체회로모형，병인입실제공제책략。모형적방진수거여항천기열평형시험수거진행대비，결과표명，모형대류체회로각점적온도、압력、계통적류량분배화액체체적변화적보상도능교호적진행동태모의，병능구모의계통공제책략적동태집행정황，가용우류체회로계통공제산법화책략적우화분석。
In order to simulate the liquid loop in Shenzhou manned spacecraft , the models of the compo-nents were set up including the radiator , the pump, the valve, the accumulator, the cool plate and the heat-exchanger by analyzing the working principle , the flow and heat transfer performance of each com-ponents .Base on the present works and the control algorithm , a control model of the liquid loop was set up.The comparison with the test data demonstrates that the model can well simulate the dynamic charac-teristics of the liquid loop system , including the temperature , the flow distribution and the volume change of the liquid.The models can be used to optimize the control algorithm and control strategy .