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Simulation and Physical Measurement of Seamless Passenger Airbag Door Deployment

机译:无缝乘客安全气囊门部署的仿真与物理测量

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Seamless Passenger Airbag Door, which means the seam of the passenger airbag door is not visible to the passenger, is being frequently implemented in the instrument panel because of its good surface appearance. But it is always a challenge to design a robust passenger airbag door with an invisible seam because many kinds of failures are possible during the design, such as cracks of the substrate of instrument panel, hinge failure of airbag door, windshield breakage, etc. Besides the engineering difficulties, the simulation of seamless passenger airbag door deployment is challenging due to three aspects: 1. the simulation method of the early stage airbag deployment (0~20 msec after trigger), 2. the material model of the airbag door pre-weakening line (the invisible seam); and 3. the physical measurement of the reaction load between cushion and door. In this paper, the FPM (Finite Point Method) method in PAM-CRASH? was used to simulate the early stage airbag deployment and the fabric material model was validated by a material sample tensile test. An airbag deployment test was designed to push a mass upwards and the acceleration of the mass was measured. The measured acceleration shows FPM method with the validated fabric material model is capable to give a good prediction of the early stage airbag deployment. The material model of door seam is also presented and validated with a physical test. To measure the reaction load between airbag cushion and door, Flexi-Force sensors, film-like pressure sensors, were used. To deal with the nonlinear signal output of the sensor in different pressure ranges, a calibration device was developed exclusively for this sensor. After the calibration, 32 Flexi-Force sensors were put into a seamless passenger airbag door on the IP structure, and then the reaction load between the airbag door and the cushion was measured in its deployment. The action point position of the resultant reaction load, its peak value and duration correlate with the physical tests. Finally, the limitations and future developments are discussed.
机译:无缝乘客安全气囊门,这意味着乘客安全气囊门的缝是不可见的乘客,在仪表板被频繁实施,因为其良好的表面外观。但它始终是设计一种健壮乘客安全气囊门具有一个不可见的接缝,因为许多种故障的设计期间是可能的,如仪表板,安全气囊门的铰链失效,挡风玻璃破损等的基板除了裂缝一个挑战工程困难,无缝乘客安全气囊门展开的仿真是具有挑战性由于三个方面:1.早期气囊展开的模拟方法(触发后0〜20毫秒),2.气囊门预的材料模型弱化线(不可见的接缝);以及3.坐垫和门之间的反应负载的物理测量。在本文中,在FPM PAM-CRASH(有限点法)的方法?被用来模拟初期气囊展开和织物材料模型是由一个材料样品拉伸试验验证。气囊展开试验设计用来向上推动的质量,测定质量的加速度。与验证织物材料模型所测得的加速度显示FPM方法能够得到早期的安全气囊展开的良好预测。门接缝的材料模型也呈现和与物理测试验证。为了测量气囊垫和门之间的反应负载,的Flexi-力传感器,薄膜状压力传感器,被使用。为了处理在不同的压力范围的传感器的信号输出的非线性,校准设备被此传感器专门开发。在校准后,32的Flexi-力传感器放入无缝乘客安全气囊门上的IP结构,然后将气囊门和座垫之间的反应负载在其部署进行测定。将得到的反应载荷的作用点位置,其峰值和持续时间相关成分与物理测试。最后,局限性和未来发展进行了讨论。

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