空间核动力装置控制鼓系统试验样机热态性能试验

Hot Performance Test of Control Drum System Experimental Prototype of Space Nuclear Power Plant

  • 摘要: 控制鼓系统是空间核动力装置上执行功率调节、紧急停堆的重要安全设备,其能否正常运行直接关系到核动力装置的安全性。为验证控制鼓系统能否满足设计要求,必须进行热态下的性能试验。本文采用1∶1全尺寸控制鼓系统试验样机,通过设计建立专用的热态性能试验装置,对试验样机寿期内全行程往复、电机切换和快速复位功能进行了试验验证和研究分析。试验过程显示,试验样机运行基本平稳,无异响和卡顿,快速复位时间满足设计指标,但传动链终端存在角度滞后、旋转过程位置重复精度低和小角度快速复位乏力等现象。该控制鼓系统试验样机机构设计基本满足机械运转功能,为下一阶段控制鼓系统结构的优化与定型奠定了基础。

     

    Abstract: The control drum system is important for power regulation and emergency shutdown of the space nuclear power plant. The safety of the reactor directly depends on whether the control drum system can operate well or not. In order to check whether the control drum system can meet the design requirements, it is necessary to carry out the performance test of the system under high temperature. The full-scale model of the control drum system was selected as the target of the hot performance test. The specific hot performance test facility was designed and installed. On the basis of the facility, series of testing, research and analysis were carried out, such as whole route reciprocating motion testing, motor switch testing and scram testing, etc. The results show that the full-scale model of the control drum system operates normally and has no abnormal sound and stuck or stagnation, and scram time meets the design target. However, there are some phenomena such as angle stagnation, low position accuracy during the restoration and lacking strength during small angle scram in the termination of the transmission chain. The mechanical design of the control drum system basically meets the functional requirements, which lays the foundation of the optimization and finalization of the control drum system in the next stage.

     

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