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Analysis of Pressure Relief Valve Dynamics During Opening

机译:开启期间泄压阀动力学分析

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In nuclear power plants power actuated pressure relief valves serve several purposes. They act as safety valves and open automatically in response to unusually high pressures in the primary system. They also act as power operated valves and are used to relieve steam in response to automatic or manually initiated control signals. These valves are required to lift completely over a short duration from the time that they receive an actuation signal, or the system pressure exceeds the set point. This short lift time results in the valve disk moving at high velocities, and can result in high impact forces on the piston and stem when the valve fully opens. To quantitatively evaluate the dynamic performance of the Target Rocket Pressure Relief Valve, an analysis effort was undertaken which would accommodate both the fluid dynamic features of the valve operation, as well as the kinematic characteristics of the valve, during pressure relief valve operation. To execute the analysis, the Generalized Fluid System Simulation Program (GFSSP) was used. GFSSP is a network flow solver CFD code developed by NASA that has the ability to analyze transient, multi-phase flows, and conjugate heat transfer, along with the inclusion of custom user subroutines developed by the user which can accommodate other simulation requirements. In this paper we present the GFSSP model developed, and the computed results that could be compared with corresponding parameters as measured from experimental testing for the pressure relief valve. Adjustments to GFSSP input parameters allow the anchoring of the GFSSP valve model to test data. This makes it possible to use the GFSSP model as a predictive tool for understanding valve dynamics, as well as evaluating proposed pressure relief valve modifications for performance improvements.
机译:在核电厂中,动力驱动的泄压阀具有多种用途。它们充当安全阀并响应主系统中异常高的压力而自动打开。它们还充当电动阀,用于根据自动或手动启动的控制信号释放蒸汽。从接收到驱动信号或系统压力超过设定点开始,这些阀需要在短时间内完全提升。较短的升程时间会导致阀盘高速运动,并在阀完全打开时对活塞和阀杆产生较大的冲击力。为了定量评估目标火箭泄压阀的动态性能,进行了一项分析工作,该分析工作既要适应泄压阀运行过程中阀门运行的流体动力学特征,又要适应阀门的运动特性。为了执行分析,使用了通用流体系统仿真程序(GFSSP)。 GFSSP是由NASA开发的网络流量求解器CFD代码,具有分析瞬态,多相流和共轭传热的能力,并包含由用户开发的可满足其他模拟要求的自定义用户子例程。在本文中,我们介绍了所开发的GFSSP模型,并将计算结果与压力释放阀的实验测试所测得的相应参数进行比较。通过调整GFSSP输入参数,可以将GFSSP阀门模型锚定到测试数据。这样就可以将GFSSP模型用作预测阀,以了解阀的动态特性,并评估建议的泄压阀修改形式以提高性能。

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