发明名称 IN-FLIGHT REFUELING SYSTEM, DAMPING DEVICE AND METHOD FOR PREVENTING OSCILLATIONS IN IN-FLIGHT REFUELING SYSTEM COMPONENTS
摘要 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.
申请公布号 US2006060710(A1) 申请公布日期 2006.03.23
申请号 US20040945602 申请日期 2004.09.21
申请人 THE BOEING COMPANY 发明人 TAKACS JOHN F.;STECKO STEPHEN M.
分类号 B64D39/00 主分类号 B64D39/00
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