The performance tests were conducted on oil–water heat transfer in circumferential overlap trisection helical baffle heat exchangers with incline angles of 12°, 16°, 20°, 24° and 28°, and com...The performance tests were conducted on oil–water heat transfer in circumferential overlap trisection helical baffle heat exchangers with incline angles of 12°, 16°, 20°, 24° and 28°, and compared with a segmental baffle heat exchanger. The results show that the shell side heat transfer coefficient h_o and pressure drop Δp_o both increase while the comprehensive index h_o/Δp_o decreases with the increase of the mass flow rate of all schemes. And the shell side heat transfer coefficient, pressure drop and the comprehensive index ho/Δpo decrease with the increase of the baffle incline angle at a certain mass flow rate. The average values of shell side heat transfer coefficient and the comprehensive index h_o/Δp_o of the 12° helical baffled scheme are above 50% higher than those of the segmental one correspondingly, while the pressure drop value is very close and the ratios of the average values are about 1.664 and 1.596, respectively. The shell-side Nusselt number Nu_o and the comprehensive index Nu_o·Eu_(zo)^(-1) increase with the increase of Reynolds number of the shell side axial in all schemes, and the results also demonstrate that the small incline angled helical scheme has better comprehensive performance.展开更多
The failure mechanism of a cylindrical shell cut into fragments by circumferential detonation collision was experimentally and numerically investigated.A self-designed detonation wave regulator was used to control the...The failure mechanism of a cylindrical shell cut into fragments by circumferential detonation collision was experimentally and numerically investigated.A self-designed detonation wave regulator was used to control the detonation and cut the shell.It was found that the self-designed regulator controlled the fragment shape.The macrostructure and micro-characteristics of fragments revealed that shear fracture was a prior mechanism,the shell fractured not only at the position of detonation collision,but the crack also penetrated the shell at the first contact position of the Chapmen-Jouguet(C-J)wave.The effects of groove number and outer layer thickness on the fracture behavior were tested by simulations.When the thickness of the outer layer was 5e18 mm,it has little effect on fragmentation of the shell,and shells all fractured at similar positions.The increase of the groove number reduced the fracture possibility of the first contact position of the C-J wave.When the groove number reached 7 with a 10 mm outer layer(1/4 model),the fracture only occurred at the position of detonation collision and the fragment width rebounded.展开更多
为探究X80管线钢半自动焊环焊缝强度匹配特性,采用压痕试验、微剪切试验及数字图像相关法(Digital image correlation,DIC)进行研究。试验结果表明,焊缝根焊层与热影响区呈现显著强度软化现象,其强度值低于母材,构成环焊缝系统的强度薄...为探究X80管线钢半自动焊环焊缝强度匹配特性,采用压痕试验、微剪切试验及数字图像相关法(Digital image correlation,DIC)进行研究。试验结果表明,焊缝根焊层与热影响区呈现显著强度软化现象,其强度值低于母材,构成环焊缝系统的强度薄弱区域。基于DIC试验结果,在低强匹配工况下,初始塑性变形集中于根焊与盖面焊趾的应力集中区,随后沿最大剪应力方向(45°)形成贯通壁厚的应变带扩展路径,与PRCI(Pipeline research council international)提出的环焊缝软化模型预测结果高度吻合,验证了该模型在工程失效分析中的适用性。研究建议环焊缝设计应遵循等强或高强匹配原则,并在现有焊接工艺评定体系中增补压痕硬度测试、微剪切强度评估及DIC等先进表征方法,以提升高钢级管道环焊缝的强度控制精度。展开更多
失速工况下,气液两相流离心泵的内部流动极为复杂。为探究不同进口含气率对离心泵失速工况流动特性的影响,该研究基于欧拉-欧拉非均相流模型和SST k-ω湍流模型,分析了进口含气率对离心泵性能的影响规律。纯水条件下,基于性能曲线和内...失速工况下,气液两相流离心泵的内部流动极为复杂。为探究不同进口含气率对离心泵失速工况流动特性的影响,该研究基于欧拉-欧拉非均相流模型和SST k-ω湍流模型,分析了进口含气率对离心泵性能的影响规律。纯水条件下,基于性能曲线和内部流动特性分析可知,0.70倍设计流量(0.70Q_(d))和0.65Q_(d)是失速发展阶段的典型工况,流场的周向均匀性存在不同程度的破坏。2个典型失速工况下,随着进口含气率的增加,泵的性能下降但下降幅度相比设计工况和深度失速工况小,气相主要附着在叶片压力侧前缘附近且附着面积逐渐增大,失速流道压力侧前缘的相对速度角增大,流动方向整体向吸力侧偏移,使得吸力侧前缘冲角减小,抑制了吸力侧前缘分离涡和中间位置漩涡的融合,进而抑制了失速的发生。引入流量变异系数(coefficient of variance,CV)定量分析流场的周向均匀性,随着流场改善,CV值逐渐减小,当模型泵处于失速初生点时,CV值位于1.38%~3.69%。少量气体加入使得失速发展阶段离心泵性能下降幅度减小且抑制失速发生。研究结果可为拓宽离心泵的高效区和提高安全稳定运行提供参考。展开更多
基金Project(50976035)supported by the National Natural Science Foundation of ChinaProject(4521ZK120064004)supported by the Science and Technology Commission Green Energy and Power Engineering of Special Fund Project of Shanghai,China
文摘The performance tests were conducted on oil–water heat transfer in circumferential overlap trisection helical baffle heat exchangers with incline angles of 12°, 16°, 20°, 24° and 28°, and compared with a segmental baffle heat exchanger. The results show that the shell side heat transfer coefficient h_o and pressure drop Δp_o both increase while the comprehensive index h_o/Δp_o decreases with the increase of the mass flow rate of all schemes. And the shell side heat transfer coefficient, pressure drop and the comprehensive index ho/Δpo decrease with the increase of the baffle incline angle at a certain mass flow rate. The average values of shell side heat transfer coefficient and the comprehensive index h_o/Δp_o of the 12° helical baffled scheme are above 50% higher than those of the segmental one correspondingly, while the pressure drop value is very close and the ratios of the average values are about 1.664 and 1.596, respectively. The shell-side Nusselt number Nu_o and the comprehensive index Nu_o·Eu_(zo)^(-1) increase with the increase of Reynolds number of the shell side axial in all schemes, and the results also demonstrate that the small incline angled helical scheme has better comprehensive performance.
基金the National Natural Science Foundation of China No.11972018the Defense Pre-Research Joint Foundation of Chinese Ordnance Industry No.6141B012858.
文摘The failure mechanism of a cylindrical shell cut into fragments by circumferential detonation collision was experimentally and numerically investigated.A self-designed detonation wave regulator was used to control the detonation and cut the shell.It was found that the self-designed regulator controlled the fragment shape.The macrostructure and micro-characteristics of fragments revealed that shear fracture was a prior mechanism,the shell fractured not only at the position of detonation collision,but the crack also penetrated the shell at the first contact position of the Chapmen-Jouguet(C-J)wave.The effects of groove number and outer layer thickness on the fracture behavior were tested by simulations.When the thickness of the outer layer was 5e18 mm,it has little effect on fragmentation of the shell,and shells all fractured at similar positions.The increase of the groove number reduced the fracture possibility of the first contact position of the C-J wave.When the groove number reached 7 with a 10 mm outer layer(1/4 model),the fracture only occurred at the position of detonation collision and the fragment width rebounded.
文摘为探究X80管线钢半自动焊环焊缝强度匹配特性,采用压痕试验、微剪切试验及数字图像相关法(Digital image correlation,DIC)进行研究。试验结果表明,焊缝根焊层与热影响区呈现显著强度软化现象,其强度值低于母材,构成环焊缝系统的强度薄弱区域。基于DIC试验结果,在低强匹配工况下,初始塑性变形集中于根焊与盖面焊趾的应力集中区,随后沿最大剪应力方向(45°)形成贯通壁厚的应变带扩展路径,与PRCI(Pipeline research council international)提出的环焊缝软化模型预测结果高度吻合,验证了该模型在工程失效分析中的适用性。研究建议环焊缝设计应遵循等强或高强匹配原则,并在现有焊接工艺评定体系中增补压痕硬度测试、微剪切强度评估及DIC等先进表征方法,以提升高钢级管道环焊缝的强度控制精度。
文摘失速工况下,气液两相流离心泵的内部流动极为复杂。为探究不同进口含气率对离心泵失速工况流动特性的影响,该研究基于欧拉-欧拉非均相流模型和SST k-ω湍流模型,分析了进口含气率对离心泵性能的影响规律。纯水条件下,基于性能曲线和内部流动特性分析可知,0.70倍设计流量(0.70Q_(d))和0.65Q_(d)是失速发展阶段的典型工况,流场的周向均匀性存在不同程度的破坏。2个典型失速工况下,随着进口含气率的增加,泵的性能下降但下降幅度相比设计工况和深度失速工况小,气相主要附着在叶片压力侧前缘附近且附着面积逐渐增大,失速流道压力侧前缘的相对速度角增大,流动方向整体向吸力侧偏移,使得吸力侧前缘冲角减小,抑制了吸力侧前缘分离涡和中间位置漩涡的融合,进而抑制了失速的发生。引入流量变异系数(coefficient of variance,CV)定量分析流场的周向均匀性,随着流场改善,CV值逐渐减小,当模型泵处于失速初生点时,CV值位于1.38%~3.69%。少量气体加入使得失速发展阶段离心泵性能下降幅度减小且抑制失速发生。研究结果可为拓宽离心泵的高效区和提高安全稳定运行提供参考。
