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Simulation of airbag impact on eyes after trabeculectomy by finite element analysis method

机译:小梁切除术后气囊对眼睛的影响的有限元分析

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PURPOSE: A finite element computer model of the human eye after trabeculectomy was used in an experiment of simulated airbag ocular injury. METHODS: A half-layer-incised scleral flap was created on the limbus and the strength of its adhesion to the outer sclera was set at 30%, 50% and 100%. The simulations were performed at a workstation using the finite element analysis program PAM CRASH (Nihon ESI, Tokyo, Japan), and the airbag was set to hit the surface of the post-trabeculectomy eye at various velocities in two directions, straight to the corneal center or straight to the scleral flap. RESULTS: In the case of airbag impact on the corneal center, the scleral flap was unlikely to rupture except when the airbag impact velocity was 40 m/sec. In the case of airbag impact on the scleral flap, at the lowest impact velocity of 20 m/sec, partial scleral flap rupture was likely to occur only at the lower adhesion strength, and scleral laceration extending to the posterior sclera was observed at impact velocities of over 30 m/sec. CONCLUSIONS: These simulation results suggest that current airbags may induce globe rupture in eyes after trabeculectomy treatment.
机译:目的:小梁切除术后人眼的有限元计算机模型用于模拟气囊眼损伤的实验中。方法:在角膜缘上形成半层切开的巩膜瓣,将其与外巩膜的粘附强度设置为30%,50%和100%。模拟是在工作站上使用有限元分析程序PAM CRASH(日本东京,日本,ESI)进行的,安全气囊设置为沿两个方向以不同的速度撞击小梁切除术后眼的表面,直达角膜中心或笔直至巩膜瓣。结果:在气囊撞击角膜中心的情况下,巩膜瓣不可能破裂,除非气囊撞击速度为40 m / sec。在气囊撞击巩膜瓣的情况下,最低撞击速度为20 m / sec,仅在较低的粘附强度下才可能发生部分巩膜瓣破裂,并且在撞击速度下观察到巩膜撕裂延伸至后巩膜超过30 m / sec。结论:这些模拟结果表明,小梁切除术治疗后,当前的安全气囊可能会引起眼球破裂。

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