在压水堆LOCA(Loss of Coolant Accident)事故之后,高能管道流体喷射冲击导致破口附近的保温层等材料破裂为碎片。这些碎片随流体在安全壳内传输并在地坑滤网沉积形成碎片床,阻碍应急堆芯冷却系统的正常运行。部分碎片可能旁通滤网进入...在压水堆LOCA(Loss of Coolant Accident)事故之后,高能管道流体喷射冲击导致破口附近的保温层等材料破裂为碎片。这些碎片随流体在安全壳内传输并在地坑滤网沉积形成碎片床,阻碍应急堆芯冷却系统的正常运行。部分碎片可能旁通滤网进入反应堆压力容器,从而引起一系列的效应。该问题被称之为GSI-191(Generic Safety Issue-191)问题。为解决GSI-191问题,首先需要确定破口附近产生的碎片量。当前研究基于ANSI/ANS58.2-1988标准和等效体积球体模型,自主开发了喷射冲击影响区域计算工具JETZOI。采用该工具计算获得的NEI(Nuclear Energy Institute)算例的喷射轮廓和等压线与美国核管会(United States Nuclear Regulatory Commission,U.S NRC)的结果符合很好,从而实现了对NEI算例的成功复现。进一步进行了不同滞止工况的敏感性分析。分析结果表明,在相同的滞止压力下,流体温度的升高将导致影响区域破坏半径的减小和碎片量的减少。因此在开展喷射冲击试验获得影响区域的破坏半径时,应当保守选取冷段双端断裂作为极限工况以使喷射冲击产生的碎片量最大。展开更多
Green manufacturing （GM） and high efficiency machining technology are inevitable trends in the field of advanced manufacturing of the 21st century. To ensure green and high-efficiency machining, a new high efficienc...Green manufacturing （GM） and high efficiency machining technology are inevitable trends in the field of advanced manufacturing of the 21st century. To ensure green and high-efficiency machining, a new high efficiency cooling technology-cryogenic pneumatic mist jet impinging cooling （CPMJI） technology is presented. For obtaining the best cooling effect, a little quantity of coolant is carried by high speed cryogenic air （-20 C ） and reaches the machining zone in the form of mist jet to enhance heat transfer. Experimental results indicate that under the conditions of 40 m/s in the jet impinging speed and 10 mm in the jet impinging distance, the critical heat flux（CHF） nearly reaches 6× 10^7 W/m^2, more than six times of the CHF of the grinding burn with a value of （8～10）×10^6 W/m^2.展开更多
The rainbow schlieren deflectometry has been combined with the computed tomography to obtain three-dimensional density fields of shock containing free jets and we call the method the schlieren CT. Experiments on the s...The rainbow schlieren deflectometry has been combined with the computed tomography to obtain three-dimensional density fields of shock containing free jets and we call the method the schlieren CT. Experiments on the schlieren CT have been performed at a nozzle pressure ratio of 4.0 by using an axisymmetric convergent nozzle with an inner diameter of 10 mm at the exit where the nozzle was operated at an underexpanded condition. Multidirectional rainbow schlieren pictures of an underexpanded sonic jet can be acquired by rotating the nozzle about its longitudinal axis in equal angular intervals and the three-dimensional density fields are reconstructed by the schlieren CT. The validity of the schlieren CT is verified by a comparison with the density fields reconstructed by the Abel inversion method. As a result, it is found that excellent quantitative agreement is reached between the three-dimensional jet density fields reconstructed from both methods.展开更多
In the present study,a computational fluid dynamics work was performed to investigate the occurrence of the shock wave by condensation in supersonic moist air jet.The unsteady,compressible axisymmetric Navier-Stokes e...In the present study,a computational fluid dynamics work was performed to investigate the occurrence of the shock wave by condensation in supersonic moist air jet.The unsteady,compressible axisymmetric Navier-Stokes equation is solved by TVD(Total Variation Diminishing) scheme in this study.The numerical simulations have been performed for low pressure ratio and various humidities.The results show the occurrence of the shock wave in supersonic moist air jet for a low pressure ratio when Mach disk does not occur,depending on humidity of the air.展开更多
文摘在压水堆LOCA(Loss of Coolant Accident)事故之后,高能管道流体喷射冲击导致破口附近的保温层等材料破裂为碎片。这些碎片随流体在安全壳内传输并在地坑滤网沉积形成碎片床,阻碍应急堆芯冷却系统的正常运行。部分碎片可能旁通滤网进入反应堆压力容器,从而引起一系列的效应。该问题被称之为GSI-191(Generic Safety Issue-191)问题。为解决GSI-191问题,首先需要确定破口附近产生的碎片量。当前研究基于ANSI/ANS58.2-1988标准和等效体积球体模型,自主开发了喷射冲击影响区域计算工具JETZOI。采用该工具计算获得的NEI(Nuclear Energy Institute)算例的喷射轮廓和等压线与美国核管会(United States Nuclear Regulatory Commission,U.S NRC)的结果符合很好,从而实现了对NEI算例的成功复现。进一步进行了不同滞止工况的敏感性分析。分析结果表明,在相同的滞止压力下,流体温度的升高将导致影响区域破坏半径的减小和碎片量的减少。因此在开展喷射冲击试验获得影响区域的破坏半径时,应当保守选取冷段双端断裂作为极限工况以使喷射冲击产生的碎片量最大。
文摘Green manufacturing （GM） and high efficiency machining technology are inevitable trends in the field of advanced manufacturing of the 21st century. To ensure green and high-efficiency machining, a new high efficiency cooling technology-cryogenic pneumatic mist jet impinging cooling （CPMJI） technology is presented. For obtaining the best cooling effect, a little quantity of coolant is carried by high speed cryogenic air （-20 C ） and reaches the machining zone in the form of mist jet to enhance heat transfer. Experimental results indicate that under the conditions of 40 m/s in the jet impinging speed and 10 mm in the jet impinging distance, the critical heat flux（CHF） nearly reaches 6× 10^7 W/m^2, more than six times of the CHF of the grinding burn with a value of （8～10）×10^6 W/m^2.
基金funded by Grant-in-Aid for Scientic Research(C)No.15K05804 of Japan Society for the Promotion of Science and supported in part by the 2014 Grant for Specially Promoted Research of the Institute of Environmental Science and Technology,The University of Kitakyushu
文摘The rainbow schlieren deflectometry has been combined with the computed tomography to obtain three-dimensional density fields of shock containing free jets and we call the method the schlieren CT. Experiments on the schlieren CT have been performed at a nozzle pressure ratio of 4.0 by using an axisymmetric convergent nozzle with an inner diameter of 10 mm at the exit where the nozzle was operated at an underexpanded condition. Multidirectional rainbow schlieren pictures of an underexpanded sonic jet can be acquired by rotating the nozzle about its longitudinal axis in equal angular intervals and the three-dimensional density fields are reconstructed by the schlieren CT. The validity of the schlieren CT is verified by a comparison with the density fields reconstructed by the Abel inversion method. As a result, it is found that excellent quantitative agreement is reached between the three-dimensional jet density fields reconstructed from both methods.
文摘In the present study,a computational fluid dynamics work was performed to investigate the occurrence of the shock wave by condensation in supersonic moist air jet.The unsteady,compressible axisymmetric Navier-Stokes equation is solved by TVD(Total Variation Diminishing) scheme in this study.The numerical simulations have been performed for low pressure ratio and various humidities.The results show the occurrence of the shock wave in supersonic moist air jet for a low pressure ratio when Mach disk does not occur,depending on humidity of the air.
