发明名称 HOLLOW COMPOSITE STRUCTURE USED AS WAVEGUIDE
摘要 Embodiments of the invention include a system including a spar of a wing having an outer body defining a hollow cavity in the outer body, a first communication assembly including a receiver and a first antenna connected to the receiver for receiving one or both of electrical signals and power, the first antenna located in the hollow cavity, and a second communication assembly. The second communication assembly includes a second antenna located in the hollow cavity and an electrical device. The second communication assembly is configured to transmit, by the second antenna, one or both of electrical signals and power through the hollow cavity to the first antenna.
申请公布号 WO2014168682(A1) 申请公布日期 2014.10.16
申请号 WO2014US16040 申请日期 2014.02.12
申请人 SIKORSKY AIRCRAFT CORPORATION 发明人 TOKGOZ, CAGATAY;SOLDNER, NICHOLAS CHARLES;ZACCHIO, JOSEPH
分类号 H01Q1/28 主分类号 H01Q1/28
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