斯特林发动机热力循环的分析方法

An analysis method of thermodynamic cycle for Stirling engine

基于机械损失以及加热器和冷却器的温度校核,对斯特林发动机循环的二阶分析法进行修正。以斯特林发动机为模拟对象,数值模拟了GPU-3斯特林发动机内部的交变流动和换热过程,得出其内部压力、温度、速度、功率和效率等参数的变化规律。数值模拟结果与NASA给出的测试结果进行比较,两者结果符合。运用修正后的二阶分析方法,分析了发动机转速、工质以及平均压强对发动机输出性能的影响。该修正后的二阶分析方法功率误差均小于20%。该分析方法为斯特林发动机的优化设计和工作特性分析提供一个有用的工具。

The second-order analysis approach for the cycle of Stirling engine is amended on the basis of mechanical loss and the temperature check of heater and radiator. Stirling engine is taken as the object, the alternating flow and heat exchange process of GPU 3 Stirling engine is simulated, and the changing rules of its internal pressure, temperature, velocity, power and efficiency are obtained. The simulation results are identical to the test results of NASA. The amended second-order analysis approach is used to analyze the effect of engine＇s rotating speed, working substance and average pressure on the engine＇ s output performance. The error of the amended approach is less than 20%. The approach may he useful for the optimization design and the characteristic analysis of Stirling engine.