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Effects of Hemispherical End-caps Geometric Optimization on Fatigue Life of Ceramic External Pressure Housing

机译:半球末端盖几何优化对陶瓷外压外壳疲劳寿命的影响

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摘要

At present, underwater gliders are not yet able to form effective observations throughout the hadal zones due to the limitations of traditional metal properties. Ceramic materials have excellent compressive strength, modulus of elasticity and low density, which can provide new solutions. However, pressure housing made of ceramic materials also has problems such as a short fatigue life. The material and geometric discontinuities between the end-cap and ceramic housing produce tensile stress on the bearing surface and cause fatigue failure under cyclic pressure. Based on this, the optimization of hemispherical TC4 end-cap geometry was focused. Utilizing the response surface method (RSM) of ANSYS workbench optimization module, and three optimization variables of mid-radius $R_{m}$ of the hemisphere end-cap, $B$ and $H$ of rigid support were analyzed to obtain the minimum tensile stress $T_{stress}$ of silicon carbide ceramic pressure housing. The radial and axial deformation curves of the pressure housing, as well as the variable sensitivity curve were obtained. Optimization results showed that $T_{stress}$ was reduced by 17.4%, and the $S_{f}$ is increased from 2.49 to 3.01. All three parameters had effects on the fatigue life of the ceramic pressure housing, the $R_{m}$ was most obvious. This method provides a methodological guide for designing the end-cap of a ceramic pressure housing.
机译:目前,由于传统金属特性的局限性,水下滑翔机尚未能够在整个牵引区内形成有效的观察。陶瓷材料具有优异的抗压强度,弹性模量和低密度,可以提供新的溶液。然而,由陶瓷材料制成的压力壳体也存在短暂的疲劳寿命等问题。端盖和陶瓷壳体之间的材料和几何不连续性在轴承表面上产生拉伸应力并在循环压力下引起疲劳失效。基于此,聚焦半球形TC4终盖几何的优化。利用ANSYS Workbench优化模块的响应曲面方法(RSM),以及中半径的三个优化变量 $ r_ {m} $ < / tex> 半球终点, $ b $ $ h $ 分析刚性载体以获得最小拉伸应力 $ t_ {crought} $ < / tex> 碳化硅陶瓷压力壳体。得到压力壳体的径向和轴向变形曲线,以及可变敏感曲线。优化结果表明 $ t_ {crought} $ < / tex> 减少了17.4%,而且 $ s_ {f} $ < / tex> 从2.49增加到3.01。所有三个参数对陶瓷压力壳体的疲劳寿命有影响, $ r_ {m} $ < / tex> 最明显。该方法提供了一种用于设计陶瓷压力壳体的端盖的方法导轨。

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