In-flight refueling system, damping device and method for...

Aeronautics and astronautics – Aircraft structure – Fuel supply

Reexamination Certificate

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C141S382000, C188S266700, C114S230210, C114S213000, C138S026000, C138S127000

Reexamination Certificate

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07007894

ABSTRACT:
An in-flight refueling system, damping device and method are provided for enhancing the stability of an elongate hose extending from a tanker aircraft during an in-flight refueling operation. The various embodiments of the system, device, and method provide a passive, integrated damping device that may generate electrical energy from changes in disposition of the elongate hose and then using the electrical energy generated to impart mechanical damping forces to a portion of the elongate hose. Thus, the embodiments may minimize the occurrence of oscillations in the elongate hose as it extends from the tanker aircraft during an in-flight refueling operation.

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patent: 2005/0045768 (2005-03-01), Saggio et al.

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