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本文采用基于燃料室和靶室独立控温的温度梯度法实现了燃料可控注入,验证了通过内径5μm充气微管注入燃料的充气技术路线可行性,并研究了初始充气压力、靶室温度和燃料室温度对充气过程的影响。结果表明,初始充气压力为86kPa、靶室温度恒温至19.5K时,控制燃料室温度即可控制燃料注入量。
In this paper, the controllable injection of fuel was achieved by the temperature gradient method based on the independent temperature control of the fuel chamber and the target chamber. The feasibility of charging the fuel through the 5 μm inner diameter aerated microtubules was verified. The effects of initial inflation pressure, Effect of Fuel Room Temperature on Aeration Process. The results show that when the initial inflation pressure is 86 kPa and the temperature of the target chamber is constant to 19.5 K, the fuel injection amount can be controlled by controlling the temperature of the fuel chamber.