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Aerial refueling coupling for in-flight operation parameter measuring

机译:空中加油接头,用于测量飞行中的运行参数

摘要

The present disclosure refers an aerial refueling coupling for in-flight parameter measuring, including a body configured to receive and support a probe and a removable shell that covers at least part of the body. The aerial refueling coupling includes a sensor system for detecting at least one parameter related to in-flight refueling operation, a data processing device configured to provide a measure at least relative to parameters detected by the sensor system, a portable storage system, and a power supply system comprising at least on battery for supplying energy, and a ram air turbine for their activation when the aerial refueling coupling is in-flight. The data processing device, the storage system and the power supply system are mounted onto the body covered by the shell.
机译:本公开涉及一种用于飞行中参数测量的空中加油接头,其包括构造成接收并支撑探针的主体以及覆盖该主体的至少一部分的可移除壳体。空中加油联接器包括用于检测至少一个与飞行中加油操作有关的参数的传感器系统,配置为至少相对于由传感器系统检测到的参数提供度量的数据处理设备,便携式存储系统以及电源供给系统,其至少包括用于提供能量的电池,以及用于在空中加油联接器处于飞行中时对其进行激活的冲压空气涡轮机。数据处理设备,存储系统和电源系统被安装在被外壳覆盖的主体上。

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