Systems and Methods for Aircraft Refueling

In an example, an indication system includes a plurality of light sources communicatively coupled with a control system. The indication system can be used with a refueling system, including a hose for supplying fuel to a receiver aircraft. Each light source is configured to simultaneously emit visib...

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Bibliographische Detailangaben
Hauptverfasser: Walsh, Timothy J, Chang, Kevin Julian
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:In an example, an indication system includes a plurality of light sources communicatively coupled with a control system. The indication system can be used with a refueling system, including a hose for supplying fuel to a receiver aircraft. Each light source is configured to simultaneously emit visible light and infrared light, and is operable at a dim setting and a bright setting. The control system receives refueling data from the refueling system. The refueling data includes position data indicating a position of the receiver aircraft relative to the refueling system. The control system is configured to, when the refueling data indicates that the position of the receiver aircraft is in a refueling range, activate at least one refueling light source of the plurality of refueling light sources at the bright setting and activate a remainder of the refueling light sources at the dim setting.