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191.
为了科学地指导DN150承插管线的使用与管理,采用非线性有限元法对带内腐蚀缺陷的DN150承插管线进行了剩余强度的评估。通过分析和计算,研究了腐蚀缺陷宽度、长度和深度对管线极限承载能力的影响。结果表明:腐蚀缺陷宽度对DN150承插管线的承载能力影响很小,可忽略不计;随着腐蚀缺陷长度的增加,管线的承载能力略微减小,当缺陷长度达到150mm,管道失效压力基本不变;随着腐蚀缺陷深度的增加,管道失效压力呈线性递减,其对管道失效压力的影响程度远远大于腐蚀缺陷长度。 相似文献
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谢佳 《中国人民武装警察部队学院学报》2013,(12):74-76
对沸点低于45℃的甲B类液体全压力储罐消防设计、审查过程中存在的问题进行了较为全面的分析,并针对这些问题提出了解决的方法,为进一步完善相关工程设计规范和有效地执行这些规范提供了实例,以期给同类工程提供有益借鉴. 相似文献
195.
The properties of Sn–Zn–Al–La fusible alloy for mitigation devices of solid propellant rocket motors
《防务技术》2022,18(9):1688-1696
The Al and La elements are added to the Sn9Zn alloy to obtain the fusible alloy for the mitigation devices of solid propellant rocket motors. Differential scanning calorimetry (DSC), metallographic analysis, scanning electron microscopy (SEM), energy dispersive spectroscopy (EDS), tensile testing and fracture analysis were used to study the effect of Al and La elements on the microstructure, melting characteristics, and mechanical properties of the Sn9Zn alloy. Whether the fusible diaphragm can effectively relieve pressure was investigated by the hydrostatic pressure at high-temperature test. Experimental results show that the melting point of the Sn9Zn-0.8Al0·2La and Sn9Zn–3Al0·2La fusible alloys can meet the predetermined working temperature of ventilation. The mechanical properties of those are more than 35% higher than that of the Sn9Zn alloy at −50 °C–70 °C, and the mechanical strength is reduced by 80% at 175 °C. It is proven by the hydrostatic pressure at high-temperature test that the fusible diaphragm can relieve pressure effectively and can be used for the design of the mitigation devices of solid propellant rocket motors. 相似文献
196.
《防务技术》2022,18(11):2008-2022
In research of the characteristics of the cavity evolution, the pressure, and the liquid spurt in hydrodynamic ram, the experiment of the high-velocity fragment impacting the water-filled container had been conducted. The relationships between the above three characteristics have been researched. The evolution of the cavity can be divided into three processes according to its shape characteristics. The first liquid spurt occurred in Process Ⅱ and the rest of it occurred in Process Ⅲ. The duration of the second liquid spurt is longer than the first liquid spurt. When the impact velocity of the fragment is less than 996 m/s, the velocity of the second liquid spurt is the highest. When the velocity of the fragment is greater than 996 m/s, the velocity of the first liquid spurt is the highest. The maximum velocities of the first and second liquid spurt are 111 m/s and 94 m/s respectively. The pressure fluctuated sharply in Processes Ⅰ and Ⅲ. The maximum peak pressures in the shock and the cavity oscillation phases are 15.51 MPa and 7.96 MPa respectively. The time interval of the two adjacent pressure pulses increases with the increase of the fragment velocity. 相似文献
197.
通过解析公式计算得到面源和面偶的诱导速度,在面偶附近区域,用涡环代替面偶,计算得到螺旋桨的速度场,根据尾涡面必须和当地流体流速相切的原则,修正原来尾涡面的形状,逐步迭代直至尾涡形状收敛,用这种方法预报了三维水翼和螺旋桨的尾涡面的形状和梢涡卷起,与试验结果有较好的一致性。 相似文献
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A cycle time‐throughput (CT‐TH) curve, which quantifies the relationship of long‐run average cycle time to throughput rate, plays an important role in strategic planning for manufacturing systems. In this paper, a nonlinear regression metamodel supported by queueing theory is developed to represent the underlying CT‐TH curve implied by a manufacturing simulation model. To estimate the model efficiently, simulation experiments are built up sequentially using a multistage procedure. Extensive numerical experiments are presented to demonstrate the effectiveness of the proposed procedure. © 2006 Wiley Periodicals, Inc. Naval Research Logistics, 2007 相似文献
200.
为了探索跨声速来流条件时,不同安装位置、不同宽度的叶尖小翼对压气机叶栅气动特性的影响,对Ma=0.8时包括原型叶栅在内的7种扩压叶栅的流场进行了数值研究.结果表明:在多种因素的共同影响下,不同来流冲角的吸力面叶尖小翼在流场中都为负效果,增加了流场复杂性;压力面叶尖小翼则改善了泄漏流动,减小了流动损失.两种安装位置的叶尖... 相似文献