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    • 6. 发明申请
    • THERMALLY-ENHANCED AND DEPLOYABLE STRUCTURES
    • WO2019204322A1
    • 2019-10-24
    • PCT/US2019/027700
    • 2019-04-16
    • RAYTHEON COMPANY
    • DUONG, Tuan L.LEEDS, Adam D.BENEDICT, James E.
    • B64G1/50
    • A system includes a flight vehicle (502, 602, 700) and one or more deployable radiators (504, 604, 702). Each deployable radiator includes a structure (100, 300) configured to receive thermal energy and to reject the thermal energy into an external environment. The structure includes (i) multiple inline and interconnected thermomechanical regions (102-108, 306-312) and (ii) one or more thermal energy transfer devices (202, 314a-314b) embedded in at least some of the thermomechanical regions. The one or more thermal energy transfer devices are configured to transfer the thermal energy between different ones of the thermomechanical regions. At least one of the thermomechanical regions includes one or more shape-memory materials configured to cause a shape of the structure to change. The thermomechanical regions may include one or more heat input regions (102, 306) configured to receive the thermal energy, one or more heat rejection regions (108, 312) configured to reject the thermal energy into the external environment, and one or more morphable regions (104, 308) including the one or more shape-memory materials and configured to change shape.