This paper deals with the determination of the static deflections, shaft stress distribution, and bearing reaction forces for a 1150 MW 11-bearing nuclear turbine-generator system.
首次尝试确定具有１１个液膜动力轴承的１１５万ｋＷ超大型核电站透平发电机转子系统的静挠度、轴应力和支承反力的分布。
Based on elasticity theory, the triaxial stress formulas of casing exposed to thermal steam under thermal stress and non-uniform in-situ stress were derived.
以暴露于热蒸汽中的目的层套管为研究对象,根据弹性力学理论,首先给出了套管在热应力和非均匀地应力作用下的三轴应力表达式,然后利用对套管施加预应力来降低套管的轴向热应力,以使得套管的有效应力控制在相应温度下套管的最小屈服极限内为原则,得到了热采井套管三轴预应力设计方法,并对辽河油田常用的N80钢级套管进行了预应力设计分析,给出了该套管在不同注汽温度和井深条件下所应使用的径厚比及相应的预应力值。
Based on the elastic theory,this paper derived the triaxial stress formulas of casing exposed to heating steam under thermal stress and non-uniform geologic stress,and established a new method to design the prestress of casing.
以暴露于热蒸汽中的目的层套管为研究对象,根据弹性力学理论,首先给出了套管在热应力和非均匀地应力作用下的三轴应力表达式,然后利用对套管施加预应力来降低套管的轴向热应力,使得套管的有效应力控制在相应温度下套管的最小屈服极限内为原则,得到了热采井套管三轴预应力设计方法,并对辽河油田常用的N80钢级套管进行了预应力设计分析,给出了该套管在不同注汽温度和井深条件下所应使用的径厚比及相应的预应力值。
The results of study is as follows: During the tensile test,the notch root produces relative high triaxial stress state.
研究结果表明:缺口拉伸试验中,缺口根部产生相对较高的三轴应力,随着应力的不断升高,微孔洞的体积分数不断增大。
In order to study the damage mechanism under different stress states of aluminum alloy component, two kinds of representative triaxial stress states have been adopted, namely notch tensile and pure shear.
为了研究铝合金构件在不同应力状态下损伤机理,采取了两种代表性的三轴应力状态,即缺口拉伸与纯剪切所产生的应力状态。
Several important factors influencing casing design and strength checkout were discussed in this paper, such as temperature and biaxial stress.
从温度对套管柱强度的影响、下部套管柱双轴应力计算等几个方面讨论了高温高压对套管柱设计和强度校核的影响 ,提出了一套适用于高温高压井套管柱设计和强度校核的理论方法 ,并给出了该方法的计算步骤 ,编制了相应的计算软件。
The damage evolution characteristics of concrete under biaxial stress are studied in this paper.
利用作者提出的混凝土各向异性损伤模型研究了混凝土材料双轴应力下的损伤演变规律在双轴应力比小于4。
Research on Numerical Simulation and Lifetime of High-temperature Components Creep Damage under Multiaxial Stress State;
多轴应力状态下高温部件蠕变损伤的数值模拟及寿命研究
The main factors influencing creep-fatigue failure under multiaxial stress and high tempera ture were investigated,and the simple model calculating method to predict the fa tigue life was worked out.
分析了高温多轴应力状态下不同应变保持时间和不同拉、扭应变比的实验结果，揭示了高温多轴应力下蠕变─疲劳失效行为的主要因素，进而提出了简捷有效的寿命计算模型和计算方法，即有交互作用系数的延性耗竭法。
Based on experiments of low-cycle tension-compression, torsion and tension-torsion fatigue with holding time, the interactional law of creep and fatigue under multiaxial stress is proposed.
通过对不同应变保持时间下的拉压、扭转和拉扭组合高温疲劳试验，得到了多轴应力下蠕变疲劳交互作用的特性及断口的微观相图，并且提出了多轴应力状态下疲劳寿命的统一方程。