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FINITE ELEMENT SIMULATIONS AND CHARACTERIZATION OF AIRBAGS USING DOE

机译:使用DOE进行气囊的有限元模拟和表征

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In the present study Low velocity impact tests have been carried out to study the energy absorption capabilities of airbags, the main objective is to increase the energy absorption capabilities by minimizing the acceleration levels and the number of bounces after the airbag impacts ground. In the present work, the effect of various parameters on the energy absorbing capabilities of airbag are studied. The three parameters chosen for the present study are Airbag Shape, Initial Pressure and the drop height. Finite Element Method (FEM) and Design of Experiments (DOE) approach are used in order to achieve the intended model objectives. The combination of both techniques is proposed to result in a reduction of the necessary experimental cost and effort in addition to getting a higher level of verification. It can be stated that the Finite Element Method coupled with Design of Experiments approach provides a good contribution in characterizing the airbag. The present work is divided into four phases, in the first phase Selection and testing of Airbag material is carried out, where the material required for the airbag is chosen and tested according to ASTM standards to find out the properties of the material The second phase includes fabrication and testing of Airbags, Where three different kinds of airbags (circular, cylindrical and rectangular) having same surface area are fabricated and tested according to the Taguchi's L9 Orthogonal Array experimental plan. In the third phase a Finite Element Model (FEM) which represents the drop tests on the airbags (carried out in the Low Velocity Impact Test Rig) is developed in order to evaluate the quality of the process parameters. In the fourth phase results are analyzed using Taguchi's Signal to Noise ratio technique, for both experimental testing and simulation of airbags to analyze the data and for the prediction of optimum results. Finally the two methods are compared (FEM and Experimental) using DOE and the results are analyzed to get the optimal set of process parameters.
机译:在本研究中,已经进行了低速冲击试验以研究安全气囊的能量吸收能力,其主要目的是通过最小化安全气囊撞击地面后的加速度和弹跳次数来提高能量吸收能力。在目前的工作中,研究了各种参数对安全气囊的能量吸收能力的影响。本研究选择的三个参数是安全气囊形状,初始压力和下落高度。为了实现预期的模型目标,使用了有限元方法(FEM)和实验设计(DOE)方法。建议将这两种技术结合使用,以降低所需的实验成本和工作量,并获得更高级别的验证。可以说,有限元方法与实验设计方法相结合,在表征安全气囊方面做出了很好的贡献。当前的工作分为四个阶段,在第一阶段中,进行安全气囊材料的选择和测试,其中选择安全气囊所需的材料并根据ASTM标准进行测试,以查明材料的特性。第二阶段包括气囊的制造和测试,其中根据田口L9正交阵列实验计划,制造并测试了三种具有相同表面积的不同类型的气囊(圆形,圆柱形和矩形)。在第三阶段,开发了代表安全气囊跌落试验的有限元模型(FEM)(在低速冲击试验装置中进行),以评估过程参数的质量。在第四阶段,使用Taguchi的信噪比技术分析结果,用于安全气囊的实验测试和仿真,以分析数据并预测最佳结果。最后,使用DOE比较这两种方法(有限元法和实验法),并对结果进行分析,以获得最佳的工艺参数集。

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