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Aerial refueling coupling for in-flight operating parameter measurement

机译:空中加油接头,用于飞行中的运行参数测量

摘要

The present invention refers an aerial refueling coupling (1) for in-flight parameter measuring, comprising a body (13) configured to receive and support a probe (18) and a removable shell (14) that covers at least part of the body (13). The aerial refueling coupling (1) comprises a sensor system for detecting at least one parameter related to in-flight refueling operation, a data processing device (4) configured to provide a measure at least relative to parameters detected by the sensor system, a portable data storage system (5), and a power supply system (2) comprising at least one battery (20) for supplying energy, and a ram air turbine (12) for their activation when the aerial refueling coupling (1) is in-flight. The data processing device (4), the data storage system (5) and the power supply system (2) are mounted onto the body (13) covered by the shell (14).
机译:本发明涉及一种用于飞行中参数测量的空中加油接头(1),其包括构造成接收并支撑探针(18)的主体(13)和覆盖该主体至少一部分的可移动壳体(14)( 13)。空中加油联接器(1)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测量的数据处理设备(4),便携式数据存储系统(5)和电源系统(2),包括至少一个用于提供能量的电池(20),以及冲压空中涡轮(12),用于在空中加油接头(1)飞行中激活。数据处理装置(4),数据存储系统(5)和电源系统(2)安装在被外壳(14)覆盖的主体(13)上。

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