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Deck Motion Interface for MQ-8C Fire Scout Embarked Aviation

机译:MQ-8C火力侦察员登上航空的甲板运动接口

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This paper provides a discussion of the challenges associated with embarking the MQ-8C Fire Scout (converted Bell 407) system onboard ships, focusing on the launch and recovery (L&R) process and equipment. The baseline version of Fire Scout, MQ-8C, along with all its improved derivatives is required to undergo ship suitability assessments in the form of dynamic interface (DI) testing, also known as helicopter-ship qualification analysis, aboard ship. DI testing evaluates all aspects of shipboard helicopter compatibility such as adequacy, effectiveness and safety of shipboard aviation support facilities and procedures for all ship-based helicopter types. To facilitate the upcoming at-sea ship-suitability assessment, a parallel effort was initiated to apply motion simulation defining deck interface experimentation ahead of sea trials. Analysis is made of various system component responses to the encountered motions and forces from a generic mono-hull vessel. Improvements in deck limits are estimated from the motion characterization of a platform in terms of, and as a function of, oleo compression and deflection, torque monitor along with indications of precise weight on wheels. At-sea preliminary validation study results are discussed and compared with simulated scenarios. This computational method employs sufficient performance criteria and correlates well with forecasted quiescent windows of deck motion. Results are presented in relation to deck energy problems normally confronted by a helicopter during recovery in progressively difficult conditions.
机译:本文讨论了与在船上安装MQ-8C Fire Scout(转换后的Bell 407)系统相关的挑战,重点是发射和恢复(L&R)过程和设备。要求将Fire Scout的基本版本MQ-8C及其所有改进的衍生版本以动态接口(DI)测试的形式进行船适用性评估,也称为船上直升机直升机资格分析。 DI测试会评估船上直升机兼容性的所有方面,例如船上航空支持设施的充分性,有效性和安全性以及适用于所有舰载直升机类型的程序。为了促进即将进行的海上船舶适应性评估,在海上试验之前,人们发起了一项平行的工作来应用运动模拟来定义甲板界面试验。分析各种系统组件对遇到的来自普通单体船的运动和力的响应。甲板极限的改进是根据平台的运动特性来估算的,该特性取决于油压,挠度,扭矩监控器以及车轮精确重量的指示,并随其变化。讨论了海上初步验证研究结果,并将其与模拟方案进行了比较。这种计算方法采用了足够的性能标准,并且与甲板运动的预测静态窗口具有良好的相关性。提出的结果与直升机在逐渐困难的条件下恢复期间通常面对的甲板能量问题有关。

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