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Aerial refueling coupling for in-flight operating parameter measurement
Aerial refueling coupling for in-flight operating parameter measurement
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机译:空中加油接头,用于飞行中的运行参数测量
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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).
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