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Evaluation of the Second Transport Rotorcraft Airframe Crash Testbed (TRACT 2) Full Scale Crash Test

机译:评估第二次运输旋翼飞机机身崩溃试验用(道2)全规模碰撞试验

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Two Transport Rotorcraft Airframe Crash Testbed (TRACT) full-scale tests were performed at NASA Langley Research Center's Landing and Impact Research Facility in 2013 and 2014. Two CH-46E airframes were impacted at 33-ft/s forward and 25-ft/s vertical combined velocities onto soft soil, which represents a severe, but potentially survivable impact scenario. TRACT 1 provided a baseline set of responses, while TRACT 2 included retrofits with composite subfloors and other crash system improvements based on TRACT 1. For TRACT 2, a total of 18 unique experiments were conducted to evaluate ATD responses, seat and restraint performance, cargo restraint effectiveness, patient litter behavior, and activation of emergency locator transmitters and crash sensors. Combinations of Hybrid Ⅱ, Hybrid Ⅲ, and ES-2 Anthropomorphic Test Devices (ATDs) were placed in forward and side facing seats and occupant results were compared against injury criteria. The structural response of the airframe was assessed based on accelerometers located throughout the airframe and using three-dimensional photogrammetric techniques. Analysis of the photogrammetric data indicated regions of maximum deflection and permanent deformation. The response of TRACT 2 was noticeably different in the longitudinal direction due to changes in the cabin configuration and soil surface, with higher acceleration and damage occurring in the cabin. Loads from ATDs in energy absorbing seats and restraints were within injury limits. Severe injury was likely for ATDs in forward facing passenger seats.
机译:两次运输旋翼机机身崩溃试验用(道)全面测试在2013年和2014年在NASA Langley研究中心的着陆和影响研究机构进行了.2 CH-46E机构受到33-FT / S Firent和25-FT / s的影响。垂直组合速度在软土地上,这代表严重但潜在可生存的影响情景。道路1提供了一种基线的反应组,而道路2包括基于散乱的复合亚级和其他碰撞系统改进的改造。对于散乱2,进行了18个独特的实验,以评估ATD响应,座位和克制性能,货物克制有效性,患者凋落物行为和紧急定位器发射器的激活和碰撞传感器。将杂交Ⅱ,杂交Ⅲ和ES-2拟方针试验装置(ATDS)的组合放置在前面,侧面座椅和乘员结果与损伤标准进行比较。基于位于整个机身的加速度计和使用三维摄影测量技术来评估机身的结构响应。摄影测量数据的分析表明最大偏转和永久变形的区域。由于机舱配置和土壤表面的变化,在纵向方向上显着不同,在机舱内发生较高的加速度和损坏,在纵向方向上显着不同。从能量吸收座椅和束缚中的ATDS负载在伤害限制范围内。前瞻性乘客席位的ATDS可能会严重伤害。

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