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Modeling and Simulation Environment for Lightweight Helicopter Wire Strike Protection System Analysis

机译:轻量级直升机线罢工保护系统分析建模与仿真环境

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Wire strike accidents are a category of aviation accidents which entail an aircraft or rotor-craft colliding with power lines, communication wires, and any other mounted wires. Currently, there are a limited amount of helicopter equipment options available to protect helicopters from collision with a wire. In particular, there is no commercially available protection system for most lightweight rotorcraft against wire strike events. Indeed, the Wire Strike Protection System (WSPS) developed by Magellan Aerospace is mainly available for medium to heavy weight helicopters. The currently available passive protection system consists of a windshield deflector and sets of two angled blades mounted on the top and under the belly of the helicopter, as well as on the skids when applicable. The system relies on the momentum of the helicopter to successfully sever the wire. Lightweight helicopters may have more difficulty using these protection systems due to having less momentum, but the efficacy of passive protection systems on lightweight helicopters has not been fully defined thus far. The goal of the present study is to develop a modeling and simulation environment enabling the analysis of wire strike events by integrating simulations of helicopter dynamics, wire behavior upon a dynamic impact, and mechanics of wire cutting with shear. The main output of the modeling and simulation environment is the prediction of whether a given type of wire will be severed by a wire cutter mounted on a specified helicopter type. A model combining techniques in cutting mechanics and wire dynamics was implemented, and the results show accordance with experimental studies of the WSPS and accident reports involving the WSPS. The estimated benefits of the tool that was created are both the quantification of the limitations that lightweight helicopters face in using current passive wire strike protection systems, as well the creation of an environment to model and simulate future mechanically enhanced protection system designs.
机译:电线罢工事故是一类航空事故,其需要与电源线,通信线和任何其他安装的电线碰撞的飞机或转子。目前,有有限的直升机设备选项可用于保护直升机与电线的碰撞。特别是,对于大多数轻质旋翼飞行器,没有商业上可获得的保护系统。实际上,由Magellan航空航天开发的线攻击保护系统(WSP)主要可用于中型至重型重量直升机。目前可用的被动保护系统由挡风玻璃偏转器和安装在直升机顶部和腹部下方的两个成角度的刀片组,以及在适用时的滑块。该系统依赖于直升机的动量来成功切割电线。由于具有较少的动力,轻质直升机可能更难以使用这些保护系统,但是迄今为止,轻质直升机上的被动保护系统的功效尚未完全定义。本研究的目的是开发建模和仿真环境,通过将直升机动力学的模拟,在动态冲击时与剪切线切割的机械切割的机械,通过集成直升机动力学,电线行为的仿真来开发建模和仿真环境。建模和仿真环境的主要输出是预测给定类型的电线将由安装在指定的直升机类型上的钢丝切割器切断。实施了切削力学和线控动力学中的模型组合技术,结果表明了涉及WSP的WSP和事故报告的实验研究。创建的工具的估计效益既有规定的局限性,轻质直升机在使用当前无源线攻击保护系统时面临的局限性,也是模拟环境的创建和模拟未来机械增强的保护系统设计。

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