发明名称 Integral propulsion and power radiant cavity receiver
摘要 A solar thermal engine for propelling and powering a craft. The solar thermal engine includes a housing, a propellant annulus, a plurality of static power converters and an electrical energy storage device. The housing has an optical cavity for receiving a beam of concentrated sunlight and converting the beam into ambient thermal energy. The propellant annulus is coupled to the housing and is selectively operable in a heating mode wherein the propellant annulus transmits at least a first portion of the ambient thermal energy to heat a flow of propellant. The plurality of static power converters are coupled to the housing and receive the first portion of the ambient thermal energy when the propellant annulus is not operated in the heating mode. The plurality of static power converters employ the first portion of the ambient thermal energy to generate electrical energy. The electrical energy storage device is coupled to the plurality of static power converters and receives and stores the electrical energy generated by the plurality of static power converters. A method for propelling and powering a craft is also provided.
申请公布号 US6311476(B1) 申请公布日期 2001.11.06
申请号 US20000590624 申请日期 2000.06.08
申请人 THE BOEING COMPANY 发明人 FRYE PATRICK EDWARD;KUDIJA, JR. CHARLES T.
分类号 B64G1/40;B64G1/44;F24J2/07;(IPC1-7):G21D1/00 主分类号 B64G1/40
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