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VALIDATION METHODOLOGY ON AIRBAG DEPLOYMENT PROCESS OF DRIVER SIDE AIRBAG

机译:驾驶员安全气囊安全气囊部署过程的验证方法

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Recent years the numerical method of the simulation for the airbag deployment process has been improved with new material model and thermodynamic model, and has become a standard application of finite element codes. With such simulation tools, it is possible to attempt supporting the airbag module design and evaluating the injuries of dummy in airbag hazard area or out-of-position. Although the simulation model for the airbag's deployment process is usually correlated with the static airbag deployments and reaction force results, up-to-date the numerical approach to represent the fluid flow within the airbag is both costly and time consuming. This paper will provide an overview of the correlation process for reducing the resource to be invested. The following two tests are conducted for acquiring the reference data. 1. Static deployment test for acquiring the airbag internal pressure during the deployment process and 2. Drop tower test for acquiring the fully deployed airbag's reaction force. The drop tower test is simulated to determine the parameter related to the leakage of fabric and vent holes with the airbag model using the uniform pressure method offering the relatively short solving time. And then Static deployment test is simulated for determining the parameter related to the unfolding phase with the airbag model using the corpuscular (particle) method. These two simulations are compared to the test results and satisfactory correlation is found in both the cases. The drop tower simulation using the uniform pressure method leads to reduce the total correlation time and to easily extend the application for protection of the driver occupant while in-position. This airbag model can be used in parametric studies to investigate the effects of airbag module design changes and to study the out-of-position (OOP) load case.
机译:近年来,新材料模型和热力学模型得到了改进了气囊部署过程的模拟的数值方法,并成为有限元码的标准应用。利用这种仿真工具,可以尝试支持安全气囊模块的设计,并评估安全气囊危险区域的假人的伤害或备忘。虽然安全气囊的部署过程的仿真模型通常与静态安全气囊展开和反作用力结果相关,但是最新的数值方法来表示安全气囊内的流体流量的昂贵且耗时。本文将概述减少资源的相关过程。进行以下两个测试以获取参考数据。 1.静态部署试验,用于在展开过程中获取安全气囊内部压力和2.跌落塔测试,以获取完全展开的安全气囊的反作用力。模拟滴塔测试以确定与使用均匀的压力方法提供相对短的求解时间的安全气囊模型与织物和通气孔泄漏相关的参数。然后模拟静态部署测试,用于使用Corpuscular(粒子)方法确定与安全气囊模型有关的参数。将这两种模拟与测试结果进行比较,并且在这种情况下发现了令人满意的相关性。使用均匀压力法的滴塔仿真导致缩短总相关时间,并且可以轻松地延长驾驶员占用者的应用,而在位置。该安全气囊模型可用于参数研究,以研究安全气囊模块设计变化的影响,并研究备用型(OOP)负载壳体。

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